ARMY DATA SHEETS FOR CARTRIDGES, CARTRIDGE ACTUATED...

TM 43-0001-39

TECHNICAL MANUAL

ARMY DATA SHEETS

FOR

CARTRIDGES,

CARTRIDGE ACTUATED DEVICES

AND

PROPELLANT ACTUATED DEVICES

FSC 1377

Approved for public release: distribution is unlimited.

HEADQUARTERS, DEPARTMENT OF THE ARMY

DECEMBER 1991

THE SQUIB SHALL NOT BE EXPOSED TO SOLVENTS ORACIDS. THEY SHALL NOT BE SUBJECTED TO SEVERESHOCK OR JAR WHICH MIGHT BREAK THE BRIDGE WIRERENDERING THE SQUIB INOPERATIVE.

TO PREVENT DISCONNECTED SQUIBS FROM FIRINGBARE ENDS OF LEAD WIRES SHALL BE TWISTEDTOGETHER SO THAT THEY ARE IN FIRM CONTACT WITHONE ANOTHER.

THIS ELECTRIC SQUIB SHALL NOT BE RESISTANCECHECKED EITHER PRIOR TO OR AFTER INSTALLATIONIN THE DEVICE OF INTENDED APPLICATION.

TM 43-0001-39C2

C h a n g e ))

No. 2 )

HEADQUARTERSDEPARTMENT OF THE ARMYWashington, DC, 30 June 1994

TECHNICAL MANUAL

ARMY DATA SHEETSFOR

CARTRIDGES, CARTRIDGE ACTUATED DEVICESAND

PROPELLANT ACTUATED DEVICES(FSC 1377)

TM 43-0001-39, 20 December 1991, is changed as follows:

1. Remove old pages and insert new pages as indicated below. New or changed material is indicatedby a vertical bar in the margin of the page. Added or revised illustrations are indicated by a verticalbar adjacent to the identification number.

Remove pages Insert pages

A and B A and Bi thru iv i thru iv5-99 thru 5-102 5-99 thru 5-102

2. File this change sheet in front of the publication for reference purposes,

By Order of the Secretary of the Army:

Official:

MILTON H. HAMILTONAdministrative Assistant to the

Secretary of the Army06338

DISTRIBUTION:

GORDON R. SULLIVANGeneral, United States Army

Chief of Staff

To be distributed in accordance with DA Form 12-34-E, Block 0933, Requirements for TM 43-0001-39.

TM 43-0001-39C1

Change ))

No. 1 )

HEADQUARTERSDEPARTMENT OF THE ARMYWashington, DC, 1 March 1994

TECHNICAL MANUAL

ARMY DATA SHEETSFOR

CARTRIDGES, CARTRIDGE ACTUATED DEVICESAND

PROPELLANT ACTUATED DEVICES(FSC 1377)

TM 43-0001-39, 20 December 1991, is changed as follows:

1. Remove old pages and insert new pages as indicated below, New or changed material is indicatedby a vertical bar in the margin of the page. Added or revised illustrations are indicated by a verticalbar adjacent to the identification number.

Remove pages Insert pages

A A and Bi and ii i and ii3-3 and 3-4 3-3 and 3-4none 3-4.1 and 3-4.2

2. File this change sheet in front of the publication for reference purposes.


Official:



DISTRIBUTION:


Chief of Staff

To be distributed in accordance with DA Form 12-34-E, Block 0933, Requirements for TM 43-0001-39.

TM 43-0001-39

When applicable, insert latest change pages and dispose ofsuperseded pages in accordance with applicable regulations.

TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 231CONSISTING OF THE FOLLOWING:

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CoverInside coverABiii. . .111iv1-1 and 1-22-12-2 blank2-3 thru 2-123-13-2 blank3-3 and 3-43-4.1 and 3-4.23-5 thru 3-124-14-2 blank4-3 thru 4-85-1 thru 5-985-99 thru 5-1025-103 thru 5-1095-110 blank6-16-2 blank

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Technical Manual

No. 43-0001-39

TM 43-0001-39

) HEADQUARTERS) DEPARTMENT OF THE ARMY) Washington, DC, 20 December 1991

ARMY DATA SHEETSFOR

CARTRIDGES,CARTRIDGE ACTUATED DEVICES

ANDPROPELLANT ACTUATED DEVICES

REPORTING OF ERRORS

You can help improve this manual. If you find any mistakes or if you know of away to improve the procedures, please let us know, Mail your letter, DA Form2028 (Recommended Changes to Publications and Blank Forms) to Commander,US. Army Armament Research, Development and Engineering Center, ATTN:SMCAR-LSB, Picatinny Arsenal, NJ 07806-5000. A reply will be furnisheddirectly to you. Comment or questions concerning individual items must beaddressed to the cognizant field activity at Naval Ordnance Station, ATTN:Code 5320C, Indian Head, MD, 20640-5000. Also see Chapter 1, para 1-1.d.

CHAPTER 1 INTRODUCTIONPurpose . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Scope . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . .DOT Shipping Class and Designation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Disposal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Reference Publications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

CHAPTER 2 CARTRIDGES, AIRCRAFT FIRE EXTINGUISHERGeneral. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cartridge, Aircraft Fire Extinguisher: (M182) . . . . . . . . . . . . . . . . . . . . . . . . .Cartridge, Aircraft Fire Extinguisher: (M193) . . . . . . . . . . . . . . . . . . . . . . . . . .Cartridge, Aircraft Fire Extinguisher: (M232) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cartridge, Aircraft Fire Extinguisher, CCU-90/A: (MH92) . . . . . . . . . . . . . . . . . . . . . .Cartridge, Aircraft Fire Extinguisher: (MT20) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

CHAPTER 3 CUTTERSGeneral . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cutter, Cartridge Actuated: M21 (M500) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cutter, Cartridge Actuated: M22 (M504) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cutter, Cartridge Actuated: (M554) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Cutter, Cartridge Actuated: P/N 3031-4-1 (MU02) . . . . . . . . . . . . . . . . . . . . .Cutter, Assembly P/N FTL3648-2 (MU03) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cutter, Delay, Propellant Actuated: (MU11) . . . . . . . . . . . . . . . . . . . . . . . .

CHAPTER 4 TIME DELAY CARTRIDGESGeneral . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cartridge, Delay: CCU-57/B, (MF35) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cartridge, Delay: CCU-89/B, (MH88) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cartridge, Delay: (M308) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

*This manual supersedes TM 43-0001-39, 28 November 1985, including all changes.

Page

1-11-11-21-21-2

2-12-32-52-72-92-11

3-13-33-4.13-53-73-93-11

4-14-34-54-7

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TM 43-0001-39

PageCHAPTER 5 SECTION I - EMERGENCY ESCAPE SYSTEMS FOR HELICOPTER;

AH-1 SERIES (COBRA)General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cord, Detonating, Assembly Flexible Confined (FCDC) (Gunner):

(MD15) . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cord, Detonating, Assembly Flexible Confined (FCDC) (Pilot):

(MD16) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cord Detonating, Assembly Shielded Mild (SMDC): (MD17) . . . . . . . . . . . . .Cord Assembly Detonating, Shielded Mile (SMDC): (MD18) . . . . . . . . . . . . . . . . .Cutting Assembly Window (WCA): (MD33) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cutting Assembly Window (WCA): (MD34) . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cutting Assembly Window (WCA): (MD35) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Cutting Assembly Window (WCA): (MD36) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS47) . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS48) . . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS49) . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS50) . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS51) . . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS52) . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS53) . . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS54) . . . . . . . . . . . . . .Cord, Detonating, Assembly, Shielded, Mild (SMCD): (MS55) . . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS56) . . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS57) . . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS58) . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS59). . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS60) . . . . . . . . . . . . . . . .Cord, Detonating, Assembly, Shielded, Mild (SMCD): (MS61) . . . . . . . . . . . . . . .Cord, Detonating, Assembly, Shielded, Mild (SMCD): (MS62) . . . . . . . . . . . . . . . .Linear Explosive Assembly (LEA): (MS76) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Linear Explosive Assembly (LEA): (MS77) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Linear Explosive Assembly Window (WCA): (MS78) . . . . . . . . . . . . . . . . . . . .Linear Explosive Assembly Window (WCA): (MS79) . . . . . . . . . . . . . . . . . .Inert Connectors. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

5-1

5-9

5-115-135-155-175-195-215-235-255-275-295-315-335-355-375-395-415-435-455-475-495-515-535-555-575-595-615-635-65

SECTION II - EMERGENCY ESCAPE SYSTEMS FOR HELICOPTER;AH-64 SERIES (APACHE)

General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Cord, Detonating, Assembly, Shielded, Mild (SMCD): (MS80) . . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS81) . . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS82) . . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS83) . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS84) . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS85) . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS86) . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS87) . . . . . . . . . . . . . . . .Cord, Detonating, Assembly Shielded, Mild (SMCD): (MS88) . . . . . . . . . . . . . . . .Cord, Detonating, Assembly, Flexible Confined (FCDC): (MS89) . . . . . . . . . .Cord, Detonating, Assembly Flexible Confined (FCDC): (MS90) . . . . . . . . . . .Cord, Detonating, Assembly, Flexible Confined (FCDC): (MS91) . . . . . . . . . . .Cord, Detonating, Assembly, Flexible Confined (FCDC): (MS92) . . . . . . . . . . .Cord, Detonating, Assembly, Flexible Confined (FCDC): (MS93) . . . . . . . . . .

5-675-715-735-755-775-795-815-835-855-875-895-915-935-955-97

ii

TM 43-0001-39

CHAPTER 5

CHAPTER 6

CHAPTER 7

CHAPTER 8

CHAPTER 9

CHAPTER 10

APPENDIX A

APPENDIX B

APPENDIX C

APPENDIX D

PageSECTION II - Continued

Canopy Severance Assembly, Forward Panel: (MS94) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-99Canopy Severance Assembly Rear (Aft) Panel: (MS95) . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-101Canopy Severance Assembly Rear (Aft) Panel: (MS96) . . . . . . . . . . . . . . . . . . . . . . . . . . 5-103Canopy Severance Assembly Forward Panel: (MS97) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-105Arming/Firing Initiator, JUA-59: (MT06) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-107Inert Connectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-109

IMPULSE CARTRIDGESGeneral . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-1Cartridge, Impulse, Mk 19 Mod 0: (MO12) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-3Cartridge, Impulse: (M162) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6-5Cartridge, Impulse: ARD 863-1 (M189) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-7Cartridge, Impulse: (M253) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-9Cartridge, Impulse, Mk 104 Mod 0: (M291) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-11Cartridge, Set, Impulse, Reduced Charge Primary: (M397) . . . . . . . . . . . . . . . . . . . . 6-13Cartridge, Impulse, Drogue: (M507) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-17Cartridge, Impulse, Guillotine: (M520) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-19Cartridge, Impulse: (M657) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-21Cartridge, Impulse, CCU-92/A: (MJ21) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-23Cartridge, Impulse: (MD73) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-25Cartridge, Impulse, CCU-44/B: (MD66) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-27

INITIATORS/DETECTORSGeneral . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-1Arming/Firing Mechanism: P/N 813633-4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-3Arming/Firing Mechanism: P/N 814033-101 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-5

ROCKET MOTORS/CATAPULTSGeneral . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8-1Rocket Motor: M447 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8-3

THRUSTERSGeneral . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9-1Thruster, Cartridge Actuated, TCU-1/B: (MF24) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9-3Thruster, Cartridge Actuated, TCU-3/A: (MJ20) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9-5Thruster, Explosive Actuated: P/N 209-033-007 -3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9-7

MISCELLANEOUS ITEMSGeneral . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10-1Refire Kit: 073-3831 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10-3Pin Puller, Explosive Actuated: P/N 816984 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10-5Cartridge Assembly, Cargo Hook: PY58 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10-7

REFERENCE PUBLICATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A-1

CAD/PAD AIRCRAFT/HELICOPTER/EQUIPMENT CROSS-REFERENCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B-1

AIRCRAFT/HELICOPTER/EQUIPMENT CAD/PAD CROSS-REFERENCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C-1

CAD/PAD INDEX BY DODIC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . D-1

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APPENDIX E CAD/PAD INDEX BY NSN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E-1

APPENDIX F CAD/PAD INDEX BY GOVERNMENT SOURCE DRAWING NUMBER . . . . F-1

APPENDIX G CAD/PAD INDEX BY MANUFACTURER’S PART NUMBER . . . . . . . . . . . . . . . . . . . . . G-1

APPENDIX H CAD/PAD INDEX BY NOMENCLATURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . H-1

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iv

TM 43-0001-39

CHAPTER 1

INTRODUCTION

1-1. Purpose

a. This manual is a reference handbookpublished as an aid in planning, training, andidentification of Cartridges/Cartridge ActuatedDevices (CADS) and Propellant ActuatedDevices (PADs). It is not to be used as authori-zation for requisitioning, stockage, mainte-nance, or issue of this materiel.

b. The CADs/PADs data sheets in thismanual are arranged by chapters according totheir characteristics. Each data sheet uses theitem nomenclature as its title, In most cases, aDODIC (in parentheses) will follow the itemname, References and cross-references arelocated in Appendix A thru Appendix H.

c. Throughout this manual, the termCAD shall be synonymous with and collectivelyrepresent FSC 1377 cartridges, cartridge actu-ated devices, and explosive detonating cordsused in aircraft/helicopter emergency escape sys-tems, fire extinguisher systems, and equip-ment/ stores jettison and separation systems.The term PAD shall be synonymous with andcollectively represent FSC 1377 rocket cata-pults and rocket motors used in aircraft escapesystems.

d . T h e N a v a l O r d a n c e S t a t i o n(NAVORDSTA), Indian Head, MD 20640-5000(Code 5320C) has been designated as theCognizant Field Activity (CFA) for CADS andPADs. Any questions concerning theCADs/PADs described in this publication shouldbe directed to this station, Code 5320C.

1-2. Scope

a. This manual contains descriptive andtechnical data for 1377 class CADS and PADsused by the Army For each CAD/PAD, thereare illustrations, descriptions, and technicaldata related to the CAD/PAD use, characteris-tics, shipping and storage, and function, plus alist of reference publications,

b. Service life is the period of time aCAD/PAD can be issued and used with anensured high degree of reliability, Performanceof CADs/PADs is influenced by the environmentto which they are exposed (e.g., temperature,humidity vibration, shock). For current dataon Service life (Shelf & Installed), refer toAppendix B of TB 9-1300-385. Updates to theTB are issued quarterly.

c. Shelf life is the period of time, begin-ning from date of manufacture, that aCAD/PAD can remain in its hermetically-sealedcontainer and still be serviceable. Shelf life isalways computed from date of manufactureavailable from the lot number.

d. Installed life is the period of time aCAD/PAD is allowed to be used after its hermeti-cally-sealed container is opened, The installedlife expiration date shall never exceed the shelflife expiration date as established from the dateof manufacture,

e. The shelf life and installed life are themaximum approved limits established for Armyuse. TB 9-1300-385 shall be consulted prior toinstalling any CAD/PAD and for periodic inspec-tions of installed CADs/PADs to ensure the lotsinstalled in operational Army aircraft/helicopt-ers/equipment have not been suspended orrestricted from use.

f. In the event of differences concerningthe shelf lives and installed lives, TB 9-1300-385 shall take precedence,

g. CAD/PAD shelf lives and installedlives are not to be combined. A CAD/PAD isover age is either of these limits is exceeded.

h. Information concerning supply opera-tion, safe handling, and maintenance of thesedevices can be found in TM 9-1377-200-20&P.

i. Included for the devices in this man-ual are the Type Classification and LogisticsControl Code (LCC). Devices with the follow-ing type classifications are included:

(1) Standard (LCC-A, LCC-B)

(2) Contingency (CON)

(3) Limited Procurement

(4) Reclassified Obsolete (OBS) for reg-ular Army use, but used by National Guard orReserve Limits.

(5) Reclassified OBS for all Army usebut used by Marine Corps, Air Force, or Navy.

stocks remain.(6) Reclassified OBS, no uses, but US

1-1

TM 43-0001-39

(7) Reclassified OBS for all US use;no US stocks remain (foreign use or stock mayremain).

j. Numerical values, such as weights,dimensions, etc., are nominal values exceptwhen specified as minimum or maximum lim-its. Actual values may vary slightly from thesevalues due to established tolerance limits.Allowable tolerance limits can be obtained fromthe drawings indicated in the data sheets.

k. The FSCM is now replaced by CAGE(Commercial and Government Entity) Code inthe Tabulated Data section of data sheets.

1.3. DOT Shipping Class and Designation

The DOT classification changed effective21 December 1990. Users of this manual mustconsult the Joint Hazard Classification System(JHCS) for Ammunition and Explosives(updated quarterly) for DOT HazardousMaterials Description (Proper Shipping Name)and Identification Number (United NationsSerial Number) for each item herein. This datais advisory only for shipments between Depots,user storage, and user facilities. Data in the lat-

est issue of the JHCS will alwaysdence unless written authorizationtrary is obtained from the PICA

take prece-to the con-(AMCCOM

Attn: DRSMC-DSD-AS (R), Rock Island, IL61299). Additional data on this matter is cur-rently being developed and will be incorporatedin future changes to this manual as it becomesofficial.

1-4. Disposal

Disposal of CADs/PADs determined to bein a hazardous, damaged, or overaged conditionis the responsibility of Explosive OrdnanceDisposal (EOD) personnel, A CAD/PAD mayonly be disassembled by EOD personnel inorder to render the unit safe. No other dis-assembly is authorized, When a unit has beenrendered safe by EOD personnel, it shall thenbe disposed of in accordance with TM 9-1300-206, DARCOM Reg 385-100, or applicableDepot Maintenance Work Requirement(DMWR).

1-5. Reference Publications

Refer to Appendix A for reference publica-tions.

1-2

TM 43-0001-39

CHAPTER 2

CARTRIDGESAIRCRAFT FIRE EXTINGUISHER

2-1. General b. The cartridges described in this chap-ter are electrically initiated, These cartridges

a. This chapter contains descriptive and shall not be resistance-checked either prior totechnical data pertaining to the aircraft fire or after installation in the device of intendedextinguisher cartridges used in Army air- application. Prior to installation of these car-craft/helicopter fire extinguishing systems. tridges, all circuits of the actuating system

shall be open.

2-1 (2-2 blank)

TM 43-0001-39

CARTRIDGE, AIRCRAFT FIRE EXTINGUISHER (M182)

Type Classification:

Refer to associated aircraft subsystem.

Use:

To release fire extinguishing fluid into thearea surrounding an aircraft engine in theevent of a fire.

Description:

The cartridge consists of a machined brasscasing with a hexagonal midsection and athreaded end enclosing a pair of electrically-fired DuPont E-92 type squibs, placed side byside. The output end of the cartridge iscrimped over a brass slug,

Each squib is a self-contained unit con-tained in a thin shell of bronze alloy, 0.272-inch

in diameter, and with an integrally-formed con-vex head.

In the assembly one lead wire of eachsquib is brought through a phenolic insulatorand soldered to a common center contact, Theinsulator is sealed in place by crimping the cas-ing over its edge, The other wire of each squibis brought into electrical contact with the car-tridge casing. Joined in parallel to common elec-trical contacts, both squibs fire simultaneously.

Each squib creates sufficient force to rup-ture the frangible disc in the valve body of thecontainer.

The cartridge is seated in the firing headof the valve body fixed to the underside of theextinguishing fluid container, This equipmentis secured within an access pocket in the wingadjacent to the engine area it is to protect.

2-3

TM 43-0001-39

Functioning

An insulated plug, attached to the firinghead of the container, connects with the air-craft electric supply and to a firing switch inthe pilot’s compartment. When the firingswitch is actuated, electric current causes thesquibs to fire, creating gas pressure which pro-pels the slug toward the seal disc, The slugpierces the segmented frangible seal disc in theexit valve body. The fluid (CF2Br2 or CF3Br),which has been held under gas pressure (nitro-gen) in the container, is thereby released, andflows from the fluid container in the wingaccess pocket to the distributing nozzles in theengine area.

Gas, developed by the extinguishingagent, reduces the oxygen content in the enginearea to a point where combustion cannot be sup-ported, thus quenching the fire.

Recommended firing current is 8 amperes.

Tabulated Data

NSN ----------------------------- 1377-00-756-1384DODIC --------------------------- M182Drawing number -------------- 2518519Vendor CAGE Code and

part number ----------------- (33525) 895188replaces 841155

Item weight --------------------- 0.17 lb (0,08 kg)Diameter ------------------------ 1 in. (2.54 cm)Length --------------------------- 1.38 in. (3.5 cm)Method of actuation --------- ElectricalBody material ------------------ BrassPropellant/explosive material:

Type ---------------------------- Lead azide, Type IIWeight ------------------------- 0.00029 lb (2.03

grains)

Performance:

Packaging:

Inner Container:Reference --------------------- MIL-C-10464

Type ----------------------------

Dimensions -------------------Items per package ----------Weight -------------------------

Outer Container:Reference ---------------------

Type ----------------------------

Dimensions -------------------

Weight -------------------------Cube ----------------------------

Temperature Limits:

Upper -----------------------------Lower -----------------------------

Hermetically-seal-ed metal container3 in. dia x 22 (es)1.25 lb

SPI (AM) P-1377-M182PPP-B-1672-TypeII, Style D18 in. x 12 in. x4.5 in.2.5 lb0.56 cu ft

+160°F (71°C)-65°F (-54°C)

Shipping and Storage Data:

Quantity distance class -----Storage compatibility

group ---------------------------DOT shipping class -----------DOT designation --------------

References:

TM 9-1377-200-20&PTM 55-1520-209-23TM 55-1520-227-23TM 55-1520-240-23TM 55-1015-204-23TM 55-1510-213-23TB 9-1300-385, App B

1.4

scACTUATING CAR-TRIDGES, EX-PLOSIVE, FIREEXTINGUISHER,HANDLECAREFULLY

2-4

TM 43-0001-39

CARTRIDGE, AIRCRAFT FIRE EXTINGUISHER: (M193)


Refer to aircraft subsystem.

Use:

To release fire extinguishing agent intothe area surrounding an aircraft engine in theevent of a fire.

NOTE

To be replaced by MH92.

Description:

The aircraft fire extinguisher cartridgewhich is electrically initiated, consists of an alu-minum hexagonal midsection with a threadedend, enclosing an electrically fired squib explo-sive. Two threaded electrical connectors, one ofwhich is insulated from the body of the car-

tridge, provides the means for completing theelectrical circuit through a grounded bridge-wire to the aircraft electrical system.

The aircraft fire extinguisher cartridge isthreaded into the discharge valve body of thefire extinguishing agent container, This equip-ment is secured within an access area aboveand between the engines.

Functioning

When the fire control switch is operated,electric current causes the squib to fire, creat-ing gas pressure which separates the splitsleeve from the housing. When the split sleeveseparates, pressure from the fire extinguisheragent then is released and flows from the con-tainer to the distributing nozzles in the enginearea.

Gas developed by the extinguishing agentreduces the oxygen content in the engine areato a point where combustion cannot be sup-ported, thus quenching the fire.

2-5

TM 43-0001-39

Tabulated Data

NSN ----------------------------- 1377-00-930-9390DODIC --------------------------- M193Drawing number -------------- 2519614Vendor (CAGE code) and

part number ----------------- (05167) 13083-5Item weight --------------------- 0.06 lb (0.03 kg)Diameter ------------------------ 0.906 in. (2.54 cm)Length --------------------------- 2.5 in. (6.4 cm)Method of actuation --------- ElectricalBody material ------------------ AluminumPropellant/explosive material:

Type ----------------------------Weight -------------------------

Performance:

Bridgewire resistance -------

Minimum pressure:-65°F (-54°C) ----------------+70°F (+21°C) -------------+ 160°F (+71°C) -----------

Packaging

Inner Container:Reference ---------------------Type ----------------------------

Dimensions -------------------

Items per package ----------

Lead Azide, Type II0.4409 lb. (3086.3grains)

.90 ohm to1.40 ohm

475 psi in 6 ms600 psi in 4 ms670 psi in 4 ms

PPP-C-96Hermetically seal-ed metal container2-1/2 in. x 7/8 in.dia4

Weight ------------------------- .75 lbOuter Container:

Reference --------------------- PPP-B-1672Type ---------------------------- Wood boxDimensions ------------------- .66 x .66x 1.00 ftWeight ------------------------- 2.5 lbCube ---------------------------- .440 ft

Temperature Limits:

Upper ----------------------------- +160°F(+71°C)Lower ----------------------------- -65°F (-54°C)


Quantity distance class ----- 1.4Storage compatibility

group --------------------------- SDOT shipping class ----------- CDOT designation -------------- ACTUATING

CARTRIDGES,EXPLOSIVE,FIREEXTINGUISHER,HANDLECAREFULLY

References:

TM 9-1377 -200 -20&PTM 55-1520-204-23TM 55-1520-213-23TM 55-1520-209-23TM 55-1510-227-23TM 55-1510-240-23TB 9-1300-385, Appendix B

2-6

TM 43-0001-39

CARTRIDGE, AIRCRAFT FIRE EXTINGUISHER: (M232)

Type Classification


Use:

To release fire extinguishing fluid into thearea surrounding an aircraft engine in theevent of a fire.

Description:

The cartridge consists of a hexheaded alu-minum casing, and a threaded end, enclosing apair of electrically-fired Dupont E-92 typesquibs, placed side by side. The output end ofthe cartridge is crimped over a brass slug. Onelead wire of each squib is brought through a phe-nolic insulator and soldered to a common cen-ter contact. The insulator is sealed in place bycrimping the casing over its edge. The otherwire of each squib is brought into electrical con-

tact with the cartridge case, Both squibs firesimultaneously.

Functioning

An insulated plug, attached to the firinghead of the container, connects with the air-craft electric supply and to a firing switch inthe pilot’s compartment. When the firingswitch is actuated, electric current causes thesquibs to fire, creating gas pressure which pro-pels the slug toward the seal disc, The slugpierces the segmented frangible seal disc in theexit valve body. The fluid (CF2Brs or CF3Br),which has been held under gas pressure (nitro-gen) is released. The fluid flows from thecontainer in the wing access pocket to the dis-tributing nozzles in the engine area.


2-7

TM 43-0001-39

Tabulated Data:

NSN . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NSN . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NSN . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DODIC ---------------------------Drawing number --------------

Vendor (CAGE code) andpart number -----------------

Item weight ---------------------

Diameter ------------------------Length ---------------------------Method of actuation ---------

Body material ------------------

1377-01-257-13591377-00-087-71031377-00-824-5858M2322519707/1660AS200

8733640.034 lb(0.0154 kg)1 in. (2.54 cm)2.560 in. (6.50 cm)Electrically fired 8amperesAluminum

Propellant/explosive material:Type ---------------------------- Lead AzideWeight ------------------------- 0.00037 lb (2.6

grains)

NOTE

M232 P/N 1660AS200 is a replacementfor M232 P/N 2519707, NSN 1377-00-824-5858/1377-00-087-7103, The exter-nal physical characteristics are identicalexcept for the identification markings.Continued use of M232 P/N 2519707 isauthorized until stocks are exhausted.

Firing Temperature Limits:Upper --------------------------Lower --------------------------

Packaging


Dimensions -------------------Items per package ----------


Type ----------------------------Dimensions -------------------

Weight -------------------------Cube ----------------------------

+160°F (+71°C)-65°F (-54°C)

MIL-C-10464Hermetically seal-ed metal container

2

PPP-B-621 Class 2Style 4Wood box4.75 x 3.5x 3.5 in.(12.07 X 8.89X 8.89cm)0.3 lb (0.136 kg)0.0337 cu ft



group --------------------------- SDOT shipping class ----------- CDOT designation- ------------ ACTUATING

CARTRIDGES,EXPLOSIVE FIREEXTINGUISHER,HANDLECAREFULLY

Performance: References:

Bridgewire resistance is 0.025 ohms minimum TM 9-1377-200-20&Pand 0.100 maximum, The cartridge shall pro- TM 55-1520-227-23vide sufficient energy to extrude the lead TM 55-1520-240-23crusher to a minimum length of 0.224 inches. TB 9-1300-385, Appendix B

2-8

TM 43-0001-39

CARTRIDGE, AIRCRAFT FIRE EXTINGUISHER CCU-90/A (MH92)


Refer to aircraft subsystem

Use:

To release fire extinguishing agent intothe engine compartment on the UH-60 helicop-ter in the event of a fire.

Description:

The aircraft fire extinguisher cartridge iselectrically initiated. It consists of an alumi-num hexagonal mid-section with a threadedend enclosing an electrically fired squib.There

are two threaded electrical connectors, one isinsulated from the body of the cartridge and pro-vides a path for completing the electrical cir-cuit. The other connection is connected toground.

Functioning

The aircraft fire extinguisher cartridge isthreaded into the discharge valve body of thefire extinguishing agent container. Switches forcompleting the electrical circuit are located inthe aircraft cockpit. Placing the switch in thefire position completes the electrical circuit,thus firing the squib and releasing the fire extin-guishing agent.

2-9

TM 43-0001-39

Tabulated Data

NSN . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DODIC ---------------------------Drawing number --------------Vendor (CAGE code) and

part number -----------------Item weight ---------------------Diameter ------------------------Length ---------------------------Method of actuation ---------Body material ------------------

1377-01-185-2622MH921512AS105

(30003) 390400200.066 lb (0.03 kg)0.875 in, (2.22, cm)2.500 in. (6.35 cm)Electrically firedAluminum

Propellant/explosive material:Type ---------------------------- RDXWeight ------------------------- 0.000441 lb (3,0865

grains)

Performance:

Bridgewire resistance is 0.90 ohms minimumand 1.40 ohms maximum. Pressure rangesfrom 475 psi at -65°F to 670 psi at + 160°F.Ignition delay shall not exceed 25 milliseconds.

Firing Temperature Limits:Upper -------------------------- +160°F (+71°C)Lower -------------------------- -65°F (-54°C)

Packaging


Type ----------------------------


Outer Container:Reference ---------------------Type ----------------------------Dimensions -------------------Weight -------------------------Cube ----------------------------

Hermetically seal-ed metal container6 x 2-5/8 dia4.50

PPP-B-636Fiberboard box1.54 X 1.04X .27 ft2.5 lb.560 ft



group --------------------------- sDOT shipping class ----------- CDOT designation -------------- Actuating Car-

tridge, ExplosiveFire Extinguisher,Handle Carefully

References:

TM 9-1377-200-20&PTM 55-1520-209-23TM 55-1520-227-23TM 55-1520-240-23TM 55-1015-204-23TM 55-1510-213-23TB 9-1300-385, Appendix B

2-10

TM 43-0001-39

CARTRIDGE, AIRCRAFT FIRE EXTINGUISHER (MT20)



Use:

To release fire extinguishing fluid into thearea surrounding an aircraft engine in theevent of a fire in the UH-60 helicopter.

Description:

The cartridge consists of a hexheaded alu-minum casing, and a threaded end, enclosing apair of electrically-fired Dupont E-92 typesquibs, placed side by side, The output end ofthe cartridge is crimped over a brass slug. Onelead wire of each squib is brought through a phe-nolic insulator and soldered to a common cen-ter contact. The insulator is sealed in place bycrimping the casing over its edge, The otherwire of each squib is brought into electrical con-

tact with the cartridge case. Both squibs firesimultaneously.

Functioning

An insulated plug, attached to the firinghead of the container, connects with the air-craft electric supply and to a firing switch inthe pilot’s compartment. When the firingswitch is actuated, electric current causes thesquibs to fire, creating gas pressure which pro-pels the slug toward the seal disc. The slugpierces the segmented frangible seal disc in theexit valve body. The fluid (CF2Brs or CF3Br),which has been held under gas pressure (nitro-gen) is released. The fluid flows from thecontainer in the wing access pocket to the dis-tributing nozzles in the engine area.


2-11

TM 43-0001-39

Tabulated Data:


part number -----------------Item weight ---------------------

Diameter ------------------------Length ---------------------------Method of actuation ---------

Body material ------------------

1377-01-263-3627MT201512AS105

8978990.034 lb(0.0154 kg)1 in. (2.54 cm)2.560 in. (6.50 cm)Electrically fired 8amperesAluminum

Propellant/explosive material:Type ---------------------------- Lead AzideWeight ------------------------- 0.00037 lb (2.6

grains)

Performance:

Bridgewire resistance is 0.025 ohms minimumand 0.100 ohms maximum. The cartridge shallprovide sufficient energy to extrude the leadcrusher to a minimum length of 0.224 inches.

Firing Temperature Limits:Upper -------------------------- + 160°F (+71°C)Lower -------------------------- -65°F (-54°C)

Packaging


Type ----------------------------

Dimensions -------------------Items per package ----------


Type ----------------------------Dimensions -------------------

Weight -------------------------Cube ----------------------------

Hermetically seal-ed metal container

2

PPP-B-621 Class 2Style 4Wood box4.75 x 3.5 x 3.5 in(12.07 X 8.89X8.89 cm)0.3 lb (0.136 kg)0.0337 cu ft




References:

TM 9-1377-200-20&PTM 55-1520-227-23TM 55-1520-240-23TB 9-1300-385, Appendix B

1.4

SCACTUATINGCARTRIDGE,EXPLOSIVE FIREEXTINGUISHER,HANDLECAREFULLY

2-12

TM 43-0001-39

CHAPTER 3

CUTTERS

3-1. General

A cutter is a cartridge or propellant actu-ated device that is used in aerial delivery sys-tems for cargo, helicopter cargo and rescuehoist cable systems and drone recovery sys-tems. Cutters are classified in accordance withthe following characteristics: (1) Method ofActuation - mechanical or electrical, (2)Function Time - nondelay or delay.

3-2. Operation

spring and the release of the firing pin areaccomplished with one motion when the firingpin moves rearward. The sear moves outwardto the cutter body section having an enlargedinternal diameter, which then permits the searto move sideward to release the firing pin. Thefiring pin is propelled forward under the actionof the spring force and strikes the primer,which ignites the delay element, if applicable,then the propellant. Under the force of the pro-pellant gas pressure, the cutter blade ispropelled onto the anvil severing the wires orcable.

a. Actuation of the mechanical cutter is b. Function of electrically or mechani-accomplished by applying a pull force to thecable or lanyard with sear attached, The lan-

cally initiated cutters is basically the same.The cutters have a specific nondelay or delay

yard sear is engaged in the firing pin; therefore,the pull of the lanyard applies a load to the fir-

time and shall be used only for their designed

ing pin spring. Compression of the firing pinapplication.

3-1 (3-2 blank)

TM 43-0001-39

CUTTER, CARTRIDGE ACTUATED: M21 (M500)

Type Classification: Functioning:

ATC-S LCC-A

To sever a nylon reefing line which allowsthe parachute to fully deploy The cutter isinstalled in a mounting bracket which isattached to the parachute.

Description:

The M21 reefing line cutter is a cartridgeactuated, one shot, disposable mechanical unitwith the cartridge sealed internally, Major com-ponents consist of case, firing pin assembly, lan-yard, knife assembly delay assembly and cotterpin.

A drogue chute is used to pull the load out ofthe delivery aircraft and to deploy the mainchute, which inflates in a reefed configurationThe deployment of the main chute applies a ten-sile force to the lanyard assembly, which isattached to the firing pin. Compression of thefiring pin spring and release of the firing pinare accomplished with the same motion. Thepotential energy stored in the spring propelsthe firing pin forward, striking the primer. Theflash of the primer ignites the 2-second pyro-technic delay mix which, in turn, sets off the pro-pellant charge behind the cutter blade assembly.

Under the force of the propellant gas pres-sure, the cutter blade separates from the knife-delay assembly and is propelled forward in thebore of the housing The impact of the blade onthe anvil severs the nylon reefing line insertedin the cutter, allowing full deployment of themain parachute.

Change 1 3-3

TM 43-0001-39

NSN -------------------------------DODIC ---------------------------Drawing number --------------Vendor (CAGE code) and

part number ------------------Item weight ---------------------Diameter -------------------------Length ----------------------------Method of actuation ----------

Body material ------------------

Propellant/ExplosiveMaterial:Type ----------------------------

Weight --------------------------

Printer --------------------------

Delay Time:-65°F . . . . . . . . . . . . . . . . . . . . . . . . . . . .+70°F ---------------------------

+160°F -------------------------

Inner Container:Reference ---------------------- MIL-P-

1377-00-060-0885M5008875978

(19200) 8875978

0.75 in. (1.905 cm)6.0 in. (15.24 cm)Manual percussionprimerAluminum alloy/carbon steel blade

Bullseye black pow-der0.0040 lb (28grains)Percussion Primer,M42

3.0 sec maximum1.6 sec minimum2.4 sec maximum1.2 sec minimum

25732/8863435Type ---------------------------- Fiberboard boxDimensions ------------------- PPP.B-636

Items per package ---------- 80Weight -------------------------- 40 lb

Outer Container:Reference ----------------------Type ----------------------------

Dimensions -------------------

Weight --------------------------Cube ----------------------------

Temperature Limits:

Upper -----------------------------Lower -----------------------------

8863436Wirebound woodbox Type II Class 2MIL-B-247212-11/16 x 11-3/8 x7 in.50 lb0.6 cu ft

+160°F (+71°C)-65°F (-54°C)


Quantity distance class ------Storage compatibility

group --------------------------- SDOT shipping class -----------DOT designation --------------

UN Code -------------------------UN Proper shipping name -

References:

TM 9-1377-200-20&PTM 10-1670-215-23TB 9-1300-385, App B

1.4

CEXPLOSIVECABLE CUTTER,HANDLECAREFULLYKEEP FIRE AWAY0070Cutter, Cable,Explosive

3-4 Change 1

TM 43-0001-39

CUTTER, CARTERIDGE ACTURATED: M22 (M504)


ATC-S LCC-A

To sever a nylon reefing line which allowsthe parachute to fully deploy, The cutter isinstalled in a mounting bracket which isattached to the parachute.

The M22 reefing line cutter is a cartridgeactuated, one shot, disposable mechanical unitwith the cartridge sealed internally Major com-ponents consist of case, firing pin assembly, lan-yard, knife assembly delay assembly, and cotterpin.

Functioning:

A drogue chute is used to pull the load out ofthe delivery aircraft and to deploy the mainchute, which inflates in a reefed configuration.The deployment of the main chute applies a ten-sile force to the lanyard assembly, which isattached to the firing pin. Compression of thefiring pin spring and release of the firing pinare accomplished with the same motion. Thepotential energy stored in the spring propelsthe firing pin forward, striking the primer. Theflash of the primer ignites the 10-second pyro-technic delay mix which, in turn, sets off the pro-pellant charge behind the cutter blade assembly.

Under the force of the propellant gas pres-sure, the cutter blade separates from the knife-delay assembly and is propelled forward in thebore of the housing. The impact of the blade onthe anvil severs the nylon reefing line insertedin the cutter, allowing full deployment of themain parachute.

Change 1 3-4.1

TM 43-0001-39

Tabulated Data:

NSN -------------------------------DODIC ---------------------------Drawing number --------------Vendor (CAGE code) and

part number------------------Item weight ---------------------Diameter -------------------------Width -----------------------------Height ----------------------------Length ----------------------------Method of actuation ----------

Body material ------------------

Propellant/ExplosiveMaterial:‘hype ----------------------------

Weight --------------------------

Net explosive wt(incl. delay elements) ---

Primer --------------------------

Performance:

Delay Time:-65°F ----------------------------+70°F ---------------------------+160°F -------------------------

Packaging:

Inner Container:Reference ----------------------

1377-00-060-0886M5048875979

(19203)

0.75 in. (1.905 cm)1.07 in.8.85 in.5.1 in,Manual percussionprimerAluminum alloy/carbon steel blade

Bullseye black pow-der0.00043 lb(3 grains)

0.0064 lbPercussion Primer,M42

15 sec maximum10 sec nom,8 sec minimum

754020103653

Type ----------------------------Dimensions -------------------Items per package ---------- 1Weight --------------------------

Outer Container:Reference ----------------------Type ----------------------------

Dimensions -------------------

Weight -------------------------Cube ----------------------------

Temperature Limits:

Upper -----------------------------Lower -----------------------------

Fiberboard box6 x 4.75 in.

3 lb

8863436Wirebound woodbox Type II Class 2MIL-B-242712-11/16 X 11-3/8 x7 in.50 lb0.6 cu ft

+160°F (+71°C)-65°F (-54°C)


Quantity distance class ------Storage compatibility


UN Code -------------------------UN Proper shipping name -

References:

TM 9-1377-200-20&PTM 10-500/TO 13C7-1-5TB 9-1300-206/TO11A-1-37

1.4

SCEXPLOSIVECABLE CUTTER,HANDLECAREFULLY.KEEP FIRE AWAY0070Cutter, Cable,Explosive

3-4.2 Change 1 *U.S. G.P.O.:1994-546-043:80739

TM 43-0001-39

CUTTER, CARTRIDGE ACTUATED: (M554)

Type Classification: Description:


Use: The cable cutter consists of an aluminumbody two steel knives, two Holex 8830-2 car-

To sever stainless steel cable that has a tridges, a protective sleeve, a cartridge O-ring,breaking strength of 25,000 lbs minimum. and a knife O-ring with a backup ring.

3-5

TM 43-0001-39

Functioning Packaging

Firing of the electrically initiated car-tridges produces gas pressure within the cutterbody which drives two knives onto the cable, cut-ting the cable.

Tabulated Data:

NSN ----------------------------- 1377-00-412-4377DODIC --------------------------- M554Drawing number -------------- 14195-1Vendor (CAGE code) and

part number ----------------- (96603) 14195-1Item weight --------------------- 1.26 lb (0.6 kg)Diameter ------------------------ 2.0 in, (5.08 cm)Length --------------------------- 7.0 in, (17.78 cm)Method of actuation --------- Electrically firedBody material ------------------ AluminumPropellant/explosive material:

Type ---------------------------- HI TEMPWeight ------------------------- 0.00195 lb (13.658

grains)

Performance:

No-Fire --------------------------- 1.0 amp max for 5minutes

Bridgewire resistance ------- 1.05 + 0.05 ohmsInsulation resistance -------- 2 megohms min at

500 VdcFiring current ------------------ 4.5 amps min

Firing Temperature Limits:

Upper ----------------------------- +125°F (+52°C)Lower ----------------------------- -65°F (-54°C)

Inner Container:Reference --------------------- MIL-B-117Type ---------------------------- BagDimensions ------------------- 4 x 12Items per package ---------- 1Weight ------------------------- 1.25 lb

Outer Container:Reference --------------------- PPP-B-1672Type ---------------------------- Fiberboard boxDimensions ------------------- .70 x .70 x 1.04 ftWeight ------------------------- 2.5 lbCube ---------------------------- .509 cu ft

Shipping and Storage Data



References:

TM 9-1377-200-20&PTM 55-1520-217-XX-1-23TM 55-1520-217-XX-2-23TB 9-1300-385, App B.

1.4

SCEXPLOSIVECABLE CUTTER,HANDLECAREFULLY,KEEP FIRE AWAY

3-6

TM 43-0001-39

CUTTER, CARTRIDGE ACTUATED: P/N 303104-1 (MU02)


Standard. The cutter contains an electrically firedcartridge, shear screw, cutter, body, and anvil.

Functioning:Use:

Firing of the electrically initiated pressureUH-1 HELICOPTER or as otherwise cartridge produces sufficient gas pressure to

applied. overcome the shear screw. The cutter blade isdriven onto the anvil cutting the cable thatpasses through the cutter body.

3-7

TM 43-0001-39

Tabulated Data:


part number -----------------

Item weight ---------------------Diameter ------------------------Length ---------------------------Method of actuation ---------Bode material ------------------

1377-01-087-5166MU02

(22567) 303104-1(82402) 42277E1820.25 lb (0.1134 kg)0.625 in. (1.59 cm)2.99 in. (7.59 cm)Electrically firedSteel

Propellant/explosive material:Type ---------------------------- Bullseye black

powderWeight ------------------------- 0.000243 lb (1.7

grains)

Performance:

Bridgewire resistance ------- .9 to 1.1 ohm


Upper -----------------------------Lower -----------------------------

Packaging:


+165°F (+74°C)-65°F (-54°C)

MIL-C-10464Type I hermeticallysealed metal con-tainer

Dimensions ------------------- 2.25 x 2.25 x 4.50in.

Items per package ---------- 1Weight ------------------------- .25 lb

Outer Container:

Reference ------------------------ PPP-B-1672Type ----------------------------- IIDimensions --------------------- 1.54 x 1.04x .35 ftWeight ---------------------------- 2.50 lbCube ----------------------------- .560 cu ft



group ---------------------------DOT shipping class -----------

DOT designation --------------

References:

TM 9-1377-200-20&PTM 55-1520-210-23 (Series)TM 55-1520-237-23TB 9-1300-385, App B

1.4

SC

EXPLOSIVECABLE CUTTER,HANDLECAREFULLY,KEEP FIRE AWAY

3-8

TM 43-0001-39

CUTTER, ASSEMBLY P/N FTL 3648-2 (MU03)



Use:

Designed for interim high altitude para-chute delivery systems.

Description:

The cutter contains a thermal battery elec-trically initiated cartridge, a mechanical firingpin, steel cutter, and aluminum body.

Functioning:

When the ASPSU is dropped from the air-craft, a mechanical firing pin mechanism is actu-

ated by a pull from a static line attached to theaircraft. This action cocks and releases a firingpin, which impacts the percussion primer of thethermal battery. The thermal battery fires andproduces 19 volts within 0.500 second and main-tains a voltage between 19 and 35 volts for aminimum of 120 seconds, with a 28-milli-ampere current drain. This energy is stored incapacitors within the cutter and altitude sensormodules until the preselected altitude isreached. At that time the firing circuit is trig-gered, and an electric current pulse of at least7.65 amperes is applied to the cartridge-actuated cutter. The cutter then fires, severingthe 9,000-pound (40.03kN)-test woven nylonline. The G-12 main parachute is then allowedto open.

3-9

TM 43-0001-39

Tabulated Data

NSN ----------------------------- 1377-01-064-4927DODIC --------------------------- MU03Drawing number -------------- 11-1-3043Vendor (CAGE code) and

part number ----------------- (26687) FTL3648-2

Item weight --------------------- 1.81 lb (0.82 kg)Diameter ------------------------Length ---------------------------Method of actuation --------- ElectricBody material ------------------ SteelPropellant/explosive material:

Type ----------------------------Weight -------------------------

Packaging:


Dimensions -------------------


HI TEMP0.0004 lb (2.8grains)

MIL-B-81705Hermetically seal-ed antistatic plasticbag11 x 3.5 x 3.5 in.(27.9 x 8.9 x8.9 cm)1

Weight ------------------------- 4.688 lbOuter Container:

Reference --------------------- PPP-B-621Type ---------------------------- Wood BoxDimensions -------------------Weight -------------------------Cube ----------------------------




Temperature Limits:

Upper -----------------------------Lower -----------------------------

References:

TM 9-1377-200-20&PTB 9-1300-385, App B

1.4


+160°F (+71°C)-65°F (-54°C)

3-10

TM 43-0001-39

CUTTER, DELAY, PROPELLANT ACTUATED: (MU11)



Use:

To sever a nylon reefing line which allowsthe parachute to fully deploy The cutter isinstalled in a mounting bracket which isattached to the parachute.

Description:

The MU11 reefing line cutter is a car-tridge actuated, one shot, disposable mechani-cal unit with the cartridge sealed internally.Major components consist of case, firing pinassembly, lanyard, knife assembly, delay assem-bly and cotter pin.

Functioning:

A drogue chute is used to pull the load outof the delivery aircraft and to deploy the mainchute, which inflates in a reefed configuration.The deployment of the main chute applies a ten-sile force to the lanyard assembly which isattached to the firing pin. Compression of thefiring pin spring and release of the firing pinare accomplished with the same motion. Thepotential energy stored in the spring propels

the firing pin forward, striking the primer. Theflash of the primer ignites the four-second pyro-technic delay mix which, in turn, sets off the pro-pellant charge behind the cutter blade assembly.

Under the force of the propellant gas pres-sure, the cutter blade separates from the knife-delay assembly and is propelled forward in thebore of the housing. The impact of the blade onthe anvil severs the nylon reefing line insertedin the cutter, allowing full deployment of themain parachute.

Tabulated Data:

NSN -----------------------------DODIC ---------------------------Drawing number --------------Vendor (CAGE code) and

part number -----------------Item weight ---------------------Diameter ------------------------Length ---------------------------Method of actuation ---------

Body material ------------------

1377-01-288-0418MU116261278

11862.7 lb0.75 in. (1.905 cm)6.0 in. (15.24 cm)Manual percussionprimerAluminumalloy/carbon steelblade

3-11

TM 43-0001-39

Propellant/explosive material:Type ---------------------------- Bullseye black

powderWeight ------------------------- 0.0040 lb (28

grains)

Performance:

Delay Times:-65°F --------------------------- 3.0 sec mm+70°F ------------------------- 1.6 sec min 2.4 sec

max+ 160°F ------------------------ 1.2 sec min

Packaging:

Inner Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiberboard boxDimensions -------------------Items per package ---------- 80Weight ------------------------- 43 lb

Outer Container:Reference --------------------- MIL-B-2427Type ---------------------------- Wood box

Dimensions ------------------- 15-13/16 x 12-15/16in.

Weight ------------------------- 50 lbCube ----------------------------

Temperature Limits:

Upper ----------------------------- +160°F (+71°C)Lower ----------------------------- -65°F (-54°C)




References:

TM 9-1377-200-20&PTM 10-1670-215-23TB 9-1300-385, App B

1.4


3-12

TM 43-0001-39

CHAPTER 4

TIME DELAY CARTRIDGES

4-1. General b. Time delay cartridges are designed tofunction at specific delay times and shall only

a. Delay cartridges consist of a body a be used for designed application.primer seat, a primer, a time delay charge, anoutput charge, and a closure disc. The composi- c. This chapter contains technical datation and the measure of the delay element for the time delay cartridges used by the Army.(charge) determine the length of the delay.

4-1 (4-2 blank)

TM 43-0001-39

CARTRIDGE, DELAY CCU-57/B (MF35)


ATC-S LCC-A

Use:

The CCU-57/B (MF35) delay cartridge issealed in the TCU-1B thruster. The TCU-1Bthruster is part of a high speed aerial deliverysystem.

Description:

Major components consist of aluminumcase, primer, O-ring, delay charge and main out-put charge.

Functioning:

Firing of the M42 primer ignites the 0.4second delay train which in turn fires the mainoutput charge that provides gas pressure forthe thruster.

Tabulated Data:

NSN ----------------------------- 1377-01-084-6046DODIC --------------------------- MF35

Drawing number -------------- 5184858Vendor (CAGE code) and

part number ----------------- (53711) 5184858Item weight ---------------------Diameter ----------------------- 0.375 in. (0.9525

cm)Length --------------------------- 2 in. (5.08 cm)Method of actuation --------- Percussion primer

M43Body material ------------------ Aluminum alloyPropellant/explosive material:

Type ----------------------------

Weight -------------------------

Performance:

Delay time ----------------------Thrust (upper limit) ---------

Minimum stroke --------------

Black powder andHES 58080.0025 lb (17.5grains)

0.4 + 0.1 second2000 lb (900 kg)max1.5 in. (3.8 cm)

4-3

TM 43-0001-39

Firing Temperature Limits: DOT shipping class ----------- CDOT designation -------------- SMALL ARMS

Upper ----------------------------- +200°F (+93°C) AMMUNITION,Lower ----------------------------- -65°F (-54°C) CLASS C,

HANDLEPackaging:

This item cannot be procured or packagedseparately. It is installed in the TCU-1B thrus-ter as a sealed-in-device.



group --------------------------- S

References:

TM 9-1377-200-20&PTM 9-1300-385, App B.

CAREFULLYKEEP FIRE AWAY

4-4

TM 43-0001-39

CARTRIDGE, DELAY CCU-89/B: (MH88)



Use:

The MH88 activates the release mecha-nism used in the parachute harness of cargodropped from aircraft. The release mechanismallows the parachute to detach from the cargoafter landing. This prevents the parachutefrom dragging the cargo and causing damage.

Description:

The cartridge consists of a cylindrical alu-minum body primer (ignition device), washer,ignition charge, delay charge, filler charge, out-put charge, and metal closure charge.

Functioning:

Primer initiation ignites a compositionigniter charge adjacent to the delay column.Upon the elapse of approximately 20 secondsthe delay mix ignites the filler and outputcharge.

4-5

TM 43-0001-39

CARTRIDGE, DELAY CCU-89/B: MH88

Tabulated Data:

NSN . . . . . . . . . . . . . . . . . . . . . . . .DODIC ---------------------------Drawing number --------------Vendor (CAGE code) and


1377-01-178-6691MH885185107

(30003) 5185107

0.506 in. (1.29 cm)2.0 in. (5.08 cm)Percussion (M42)Aluminum

Propellant/explosive material:Type -----------------------------

Weight -------------------------

Performance:

20 second delay.

Packaging:

Inner Container:Reference ---------------------Type ----------------------------Dimensions -------------------Items per package ----------Weight -------------------------

Tungsten delaycomposition0.00616 (42 grains)

10

Outer Container:Reference ---------------------Type ---------------------------- Wood boxDimensions ------------------- 8.38 x 8.38 x 14.63

in.Weight -------------------------Cube ---------------------------- 0.6 cu ft

Temperature Limits:

Upper ----------------------------- +160°F (+71°C)Lower ----------------------------- -65°F (-54°C)




References:

TM 9-1377-200-20&PTM 10-1670-215-23TB 9-1300-385, App B.

1.4

SCSMALL ARMSAMMUNITION,HANDLECAREFULLY,KEEP FIRE AWAY

4-6

TM 43-0001-39

CARTRIDGE, DELAY: (M308)


ATC-S LCC-A The M252 delay cartridge is cylindrical inshape, It consists of the body a primer seat,

Use: washer, M42 primer, A1A igniter charge, delayPower device for the 5,000 lb. capacity charge, output charge, and closing disc.

cargo parachute release. Functioning:

NOTE Its function is to allow a nominal 20-second delay, during which cargo descent is sta-

Replacement is MH88. bilized, before tripping a spinner mechanismwhich allows the parachute to release upon land-ing.

4-7

TM 43-0001-39

When the cargo is jettisoned from the air-craft, parachute deployment activates the firingmechanism. This compresses a spring behindthe firing pin. The stored energy of the com-pressed spring drives the firing pin into theM42 percussion primer of the M252 cartridge.

Primer initiation ignites an A1A composi-tion igniter charge adjacent to the delaycolumn. Upon the elapse of approximately 20seconds, the delay mix ignites the filler and out-put charge; the resulting gases rotate the spin-ner on the release mechanism which releasesthe ground disconnect pin attached to thecatch. Upon ground contact (no load on therelease), the rotated spinner allows the latchholding the cargo to release. Thus, the para-chute is prevented from dragging or causingthe cargo to tumble along the ground.

Tabulated Data:


part number -----------------

Item weight ---------------------

Diameter ------------------------

Length ---------------------------Method of actuation ---------

Body material ------------------

1377-00-958-1048M3088886478 (19203)

(81337) 11-1-329(26687)0.007 lb (0.0032kg)0.375 in. (0.9525cm)2 in. (5.08 cm)Percussion primerM42Steel

Propellant/explosive material:Type ---------------------------- Lead azideWeight ------------------------- 0.006 lb (42 grains)

Performance:

Delay time ---------------------- 20 seconds


Upper ----------------------------- +160°F (+71°C)Lower ----------------------------- -65°F (-54°C)

Packaging:

Inner Container: 1Reference --------------------- PPP-B-636Type ---------------------------- Fiberboard boxDimensions -------------------Items per package ---------- 100Weight ------------------------- 0.70 lb (0.32 kg)

Inner Container: 11Reference --------------------- MIL-B-117Type ---------------------------- Barrier bagDimensions -------------------Items per package ---------- 1Weight ------------------------- 1.5 lb (0.68 kg)

Outer container:Reference --------------------- PPP-631Type ---------------------------- Class 2/Style 4Dimensions ------------------- Wood boxWeight ------------------------- 30 lb (13.6 kg)Cube ----------------------------

Skipping and Storage Data:


group --------------------------- SDOT shipping class ----------- CDOT designation -------------- SMALL ARMS

AMMUNITION,HANDLECAREFULLY,KEEP FIRE AWAY

References:

TM 9-1377-200-20&PTM 10-1670-215-23TB 9-1300-385, App B.

4-8

TM 43-0001-39

CHAPTER 5

EMERGENCY ESCAPE SYSTEMS FORHELICOPTERS, AH-64

Section I. AH-1 (COBRA)

5-1. General (for Army AH-1 (Cobra)Helicopter)

a. Section I of this chapter contains des-criptive and technical data pertaining to sys-tems used for the Army AH1E-F/P/S (MOD)Helicopter Personnel Emergency EscapeSystems. Each system is used to explosively cutthe windows of the canopy and doors from thecanopy support structure to provide a rapidmeans of escape/access to/from the crew com-partment.

b. The system consists of four linearexplosive window cutting assemblies (WCA)which are installed around the rim of the can-opy and door windows of the crew compartment(fig. 5-1), three armed/firing mechanisms, andinterconnecting flexible confined detonatingcords (FCED) and rigid shielded mild detonat-ing cord (SMDC) lines (fig. 5-2). One armed/fir-

ing mechanism is located in the pilot’sinstrument panel to the left of the glare shield,another is located in the gunner/copilot’s rightconsole, and the third is in the nose of the heli-copter located to provide external access by res-cue personnel, Any one of the three armed/fir-ing mechanisms can be used to actuate thelinear explosive escape system.

c. The detonating cord set consists ofeight SMDC assemblies, two FCDC assembliesand four WCA assemblies. Each type assemblyis described in this section. Individual detonat-ing cord lines are listed in table 5-1. Table 5-2lists these components and their location andfunction. Table 5-3 lists detonating cord assem-blies used in AH-1 series Army helicopters.

d. Section I also contains descriptive infor-mation pertaining to the inert connectors usedin the helicopter canopy removal system.

5-1

TM 43-0001-39

Figure 5-1. Attack Helicopter, Model AH-1, All Modifications,Emergency Canopy Jettison Elements.

5-2

TM 43-0001-39

Table 5-1. Explosive Components Technical Data and Cross-Reference

AH-1 Series

DODIC

MD15

MD16

MD17

MD18

MD33

MD34

MD35

MD36

ME83

Assembly

FCDC

FCDC

SMDC

SMDC

WCA

WCA

WCA

WCA

***CORDSET, DETO-NATING

ARMED/

MECHAN-ISM

*T-McC-SP/N

813592-6

813592-5

813475-19

813475-27

814280-15

814280-9 or814280-13

814280-102or 814280-11

814280-101or 814280-9

. . . . . . . . . . . . . . . . . .

813633-4

**Bell P/N

209-030-711-11

209-030-711-13

209-030-711-19

209-030-711-27

209-030-711-105

209-030-711-99

209-030-711-37

209-030-711-103

. . . . . . . . . . . . . . . . . . . . . . .

209-030-711-61

NSN1377-oo-

410-8271

409-1099

410-8297

409-1098

409-1096

409-1095

106-7773

409-1097

01-060-8531

410-8265

Length (IN.)

67,5

22.4

6.5

6.6

150,0

110.0

110,0

150.0

. . . . . . . . . . . . . . . . . .

6.5

ExplosiveWeight (LB)

0,01115

0,00787

0.00065

0.00063

0.00461

0.00390

0.00375

0.00466

0.03268

0.00019FIRING

*CAGE Code 06331**CAGE Code 97499***Contains one each of of all items except the armed/firing mechanism

5-3

TM 43-0001-39

DODIC

MD15

MD16

WCA

MD17

MD18

MD33

MD34

MD35

MD36

ME83

—

Table 5-2. Summary of Devices in AH-1Series Canopy Release System

Nomenclature

Flexible ConfinedDetonating Cord(FCDC) 857AS500-2

FCDC - 857AS500-1

Shielded MildDetonating Cord(SMDC) - 857AS400-1

SMDC - 857AS400-2

Window CuttingAssembly (WCA) -857AS300-4 or857AS300-15

WCA - 857AS300-3 or857AS300-13

WCA - 857AS300-2 or857AS300-11

WCA - 857AS300-1 or857AS300-9

Cord Set, Detonating,Canopy RemovalSystem 857AS600

Armed/FiringMechanism

Quantity/Location

1- Between left junc-tion manifold and WCAgunner’s door

1- Between right junc-tion manifold and WCApilot’s door

1- Between left junc-tion manifold and WCApilot’s window

1- Between right junc-tion manifold and WCAgunner’s window

1- Pilot’s canopy win-dow

1- Gunner’s canopywindow

1- Gunner’s door win-dow

1- Pilot’s door window

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

3- One each at pilot’sand gunner’s stationsand one in fuselagenose

*Function

Provides flexible explo-sive media betweenjunction manifold and

Provides flexible explo-sive media betweenjunction manifold and

Provides explosivemedia between junctionmanifold and WCA

Provides explosivemedia between junctionmanifold and WCA

Explosively cuts(removes) and ejectsglass from pilot’s can-opy window

Explosively cuts(removes) and ejectsglass from gunner’scanopy window

Explosively cuts(removes) and ejectsglass from gunner’sdoor window

Explosively cuts(removes) and ejectsglass from pilot’s doorwindow

System procurement

Initiates detonationwave to actuate windowcutting assemblies

*Service life at end of table.

5-4

TM 43-0001-39

Table 5-2. Summary of Devices in AH-1 Series

DODIC

INERT

INERT

INERT

Canopy Release System (Continued)

Nomenclature

In-line connector857AS103-1

Tee Connector857AS101-1

Cross Connector857AS102-1

*Service Life: (Explosive Devices)

Service life listed in this TM is nominal.Specific service life data is listed in TB 9-1300-385, App B. Updates to the TB are issued quar-terly

Quantity/Location

1- Forward bulkheadsection

1- Behind gunner’sseat

2- Upper right canopystructure and upper leftcanopy structure

**Function

Detonation transfermedia



**Service Life: (Inert Connectors)

Item is an assembly of metal parts only.Replacement is determined by “On Condition”(OC), after inspection for visible wear or defect,

5-5

TM 43-0001-39

Table 5-3. Detonating Cord Assemblies and ElementsUsed in Army Helicopters: AH-1 Series

NSN

1377-00-409-1100

1377-00-410-8222

1377-00-410-8228

1377-00-410-8266

1377-00-410-8289

1377-01-032-1047

1377-01-032-1048

1377-01-032-1049

1377-01-032-1050

1377-01-032-3279

1377-01-032-3280

1377-01-100-1718

1377-01-032-3283

1377-01-032-3286

1377-01-033-5088

1377-01-035-4124

1377-01-037-4090

DODIC

MS50

MS49

. . . .

MS47

MS48

MS76

MS77

MS78

MS79

MS60

MS61

MS62

MS59

MS58

---

MS51

MS53

Nomenclature

Cord, Detonating(SMDC)


Manifold, Junction(Inert)



Cord, Detonating(LSC)

Cord, Detonating(LSC)

Cord, DetonatingWindow Cutting Assy

Cord, DetonatingWindow Cutting Assy






Arm, Fire Initiator



*(CAGE) P/N

(97499) 209-030-711-25(06331) 813475-25

(97499) 209-030-711-21(06331) 813475-21

(97499) 209-030 -711-9(06331) 813487-2

(97499) 209-030-711-15(06331) 813475-15

(97499) 209-030-711-17(06331) 813475-17

(97499) 209-033-009-1(06331) 816986-1

(97499) 209-033-009-3(06331) 816986-3

(97499) 209-033-010-103(06331) 816987-103

(97499) 209-033-010-105(06331) 816987-105

(97499) 209-033-011-123(06331) 813475-123

(97499) 209-033-011-23(97499) 209-033-011-49

(30003) 813-475-127

(97499) 209-033-011-125(06331) 813475-125

(97499) 209-033-011-119(06331) 813475-119

(97499) 209-033-008-101(06331) 814033-101

(97499) 209-033-011-105(06331) 813475-105

(97499) 209-033-011-109(06331) 813475-109

*Coxmnercial And Government Entity (CAGE)(Formerly FSCM Code).

5-6

TM 43-0001-39

Table 5-3. Detonating Cord Assemblies and ElementsUsed in Army Helicopter AH-1 Series (Continued)

NSN

1377-01-037-4091

1377-01-037-4092

1377-01-037-4093

1377-01-037-4094

1377-01-037-4095

1377-01-037-4096

1377-01-037-9237

1377-01-062-4195

DODIC

. . . .

. . . .

MS57

MS56

MS55

MS54

MS52

. . . .

Nomenclature

Pin Puller, Explosive

Manifold, Junction(Inert)






Connector, In-line(Inert)

*(CAGE) P/N

(97499) 209-033-006-101(06331) 816984-107

(97499) 209-033-011-101(06331) 817295-101

(97499) 209-033-011-117(06331) 813475-117

(97499) 209-033-011-115(06331) 813475-115

(97499) 209-033-011-113(06331) 813475-113

(97499) 209-033-011-111(06331) 813475-111

(97499) 209-033-011-107(06331) 813475-107

(97499) 209-033-011-103(06331) 819347-103

*Coxmnercial And Government Entity (CAGE)(Formerly FSCM Code Number).

5-7

TM 43-0001-39

Figure 5-2. Canopy Jettison Removal System (Schematic) for the AH-1 Series.

5-8

TM 43-0001-39

CORD, DETONATING, ASSEMBLY, FLEXIBLE CONFINED (FCDC) (GUNNER): (MD15)



Use:

To provide and interconnecting explosivemedia to the Window Cutting Assembly (WCA)of the gunner’s canopy door used in theEmergency Canopy Removal System of the AH-1 series Helicopter.

Description:

Major components of the FCDC assemblyare housing, threaded fittings, seals, loadedcharge case, lead sheath assembly, and pre-scribed amounts of Hexanitrostilbene (HNS).This FCDC lead sheathed assembly is located in

the canopy between the left junction manifoldand the adapter to the WCA in the gunner’s can-opy door.

NOTE

The MD15 is identical in design and physi-cal appearance to the MD16, The differ-ence is in length and amount of explosive,

Functioning

When any one of the three armed/firingmechanisms is actuated, the FCDC linereceives a detonating stimulus via a junctionmanifold and transmits it to the WCA in thegunner’s canopy door.

5-9

TM 43-0001-39

Tabulated Data:

NSN ----------------------------- 1377-00-410-8271DODIC --------------------------- MD15Drawing number -------------- 857AS500-2Vendor (CAGE code) and

part number ----------------- (97499) 209-030-711-11 (06331)813592-6

Item weight ---------------------Diameter ------------------------ 0,5 in, (1.27 cm)Length --------------------------- 67,5 in, (171,45 cm)Method of actuation --------- High order detona-

tion waveBody Material ------------------ Lead 6% antimony

alloy sheathedPropellant/explosive material:

Types --------------------------- HNS, Type I GradeA

Weight ------------------------- 0.01115 lb. (78.05grains)

Performance:

Minimum detonationvelocity ------------------------ 6050 meters/see at

-65° (-54°C)

Inner container:Reference --------------------- MIL-B-817051

857AS500-2Type ---------------------------- Sealed bagDimensions ------------------- 68’ long x 1“ dia

(172.7 cm long x2.5 cm dia)

Items per package ---------- 1Weight ------------------------- 0.5 lb (0.23 kg)

Outer Container:Reference --------------------- Commercially

packedType ---------------------------- IIDimensions ------------------- 1.54 x 1.04x .27Weight ------------------------- 1.50 (lb)Cube ---------------------------- .464 cu ft



group --------------------------- SDOT shipping class ----------- CDOT designation -------------- Flexible Linear

Shaped Charge,Handle CarefullyKeep Fire Away

Firing Temperature Limits:Reference:

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TM 9-1300-385, App B.

5-10

TM 43-0001-39

CORD, DETONATING, ASSEMBLY, FLEXIBLE CONFINED (FCDC) (PILOT): (MD16)



Use:

To provide and interconnecting explosivemedia to the Window Cutting Assembly (WCA)of the pilot’s canopy door used in theEmergency Canopy Removal System of the AH-1 series Helicopter,

Description:

Major components of the FCDC Assemblyare housing, threaded fittings, seals chargecase, Hexanitrostilbene (HNS), lead sheathedassembly This FCDC lead sheathed assemblyis located in the canopy between the left junc-

tion manifold and the adapterthe pilot’s canopy door,

NOTE

to the WCA in

The MD16 is identical in design and physi-cal appearance to the MD 15. The differ-ence is in length and amount of explosive.

Functioning:

When any one of the three armed/firingmechanisms is actuated, the FCDC linereceives a detonating stimulus via a junctionmanifold and transmits it to the WCA in thepilot’s canopy door.

5-11

TM 43-0001-39

Tabulated Data:

NSN . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DODIC ---------------------------Drawing number --------------Vendor (CAGE Code) and

part number -----------------

Item Weight --------------------Diameter ------------------------Length ---------------------------Method of actuation ---------

Body Material ------------------

1377-00-409-1099MD16857AS500-1

(97499) 209-030-711-13 (0633.1)813592-5

0.5 in. (1.27 cm)22.4 in. (58.9 cm)High order detona-tion waveLead 6% antimonyalloy sheathed

Propellant/explosive material:Type ---------------------------- HNS, Type I, grade

AWeight ------------------------- 0.00187 lb (55.09

grains)

Performance:

Minimum detonationvelocity ------------------------ 6050 meter/see at

-65°F (-54°C)


Upper ----------------------------- +200°F (+93° C)Lower ----------------------------- -65°F (-54° C)

Packaging:


Type ----------------------------



Type ----------------------------Dimensions -------------------Weight -------------------------Cube ----------------------------

Type I, Hermeti-cally sealed metalcontainer62-1/2 x 1/2 in.10.2 lb (0.09 kg)

CommerciallypackedII1.54 X 1.04X .27 ft2 lb.464 ft




References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B.

1.4

SCFLEXIBLELINEAR SHAPEDCHARGE, METALCLAD, HANDLECAREFULLYKEEP FIRE AWAY

5-12

TM 43-0001-39

CORD, DETONATING, ASSEMBLY, SHIELDED MILD (SMDC): (MD17)



Use:

To provide an interconnecting explosivemedia to the Window Cutting Assembly (WCA)of the pilot’s canopy door used in theEmergency Canopy Removal System of the AH-1 series Helicopter,

Description:

Major components of the FCDC Assemblyare (MD17) are threaded fittings, seals wash-ers, inner and outer ferrules, loaded booster

shell, and silver sheathed mild detonating cord.This assembly is located between the left junc-tion manifold and the WCA in the pilot’s can-opy door.

Functioning:

Upon actuation of the system by armingand firing any one of the three armed/firingmechanisms, a detonation wave is received viathe left junction manifold and is boosted by theloaded booster shell. The stimuli from thebooster actuates the HNS within the SMDCassembly to the adapter of the pilot’s canopyWCA.

5-13

TM 43-0001-39

Tabulated Data:


part number -----------------


Body Material ------------------

1377-00-410-8297MD17857AS400-1

(97499) 209-030-711-19 (06331)813475-19

0.23 in. (0.58 cm)6.45 in. (16.4 cm)High order detona-tion waveSilver sheathed,high fine silver99.95%

Propellant/explosive material:Type ---------------------------- HNS, Type I, grade

AWeight ------------------------- 0.00065 lb (4.55

grains)

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging

Inner Container:Reference --------------------- MIL-B-81795

Type ----------------------------

Dimensions -------------------

Items per package ----------Weight -------------------------

Outer Container:Reference ---------------------Type ----------------------------

Dimensions -------------------Weight -------------------------Cube ----------------------------

Type II, heatsealed, anti-staticplastic bag12 in. long x 1. in.dia (30.4 cm long x2,54 cm dia)10.2 lb (0.091 kg)

PP-B-621Class II style 4Wood BOX

1.54 X 1.04X .27 ft2 lb.464 ft




References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

1.4

SCLINEAR SHAPEDCHARGE, METALCLAD, HANDLECAREFULLYKEEP FIRE AWAY

5-14

TM 43-0001-39

CORD, DETONATING, ASSEMBLY, SHIELDED, MILD (SMDC): (MD18)



Use:

To provide an interconnecting explosivemedia to the Window Cutting Assembly (WCA)of the gunner’s canopy window used in theEmergency Canopy Removal System of the AH-1 series Helicopter.

Description:

Major components of the SMDC Assembly(MD18) are threaded fitting seals, washers,inner and outer ferrules, loaded booster shell,and silver sheathed mild detonating cord,

This assembly is located between the rightjunction manifold and the WCA of the gunner’scanopy window.

Functioning:

Upon actuation of theand firing any one of the

system by armingthree armed/firing

mechanisms, a detonation wave is received viathe left junction manifold and is boosted by theloaded booster shell. The stimuli from thebooster actuates the HNS within the SMDCassembly to the adapter of the gunner’s canopyWCA.

NOTE

The MD18 is identical to the MD17 inphysical appearance and design, The dif-ference is in length and amount of explo-sive,

5-15

TM 43-0001-39

Tabulated Data:


part number -----------------


Body Material ------------------

1377-00-409-1098MD18857AS400-2

(97499) 209-030-711-27 (06331)813475-27

0.23 in. (0,58 cm)6.0 in. (15.24 cm)High order detona-tion waveSilver sheathed,high fine silver99.95%

Propellant/explosive material:Type ---------------------------- HNS, Type I Grade

AWeight ------------------------- 0.00063 lb (4,41

grains)

Performance:


-65°F (-54°C)


Upper -------------------------- +200°F (+93°C)Lower -------------------------- -65° F (-54°C)

Packaging:


Type ----------------------------

Dimensions -------------------


Outer Container:Reference ---------------------Type ----------------------------

Weight -------------------------Cube ----------------------------

Type II, heat sealedanti-static plasticbag12 in. long x 1. in.dia (30.48 cm long x2.54 cm dia)10.2 lb (0.91 kg)

PPP-C-1672Class II style 4Wood BOX

2 lb.464 ft




References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

1.4

SCLINEAR SHAPEDCHARGE, METALCLAD, HANDLECAREFULLY,KEEP FIRE AWAY

5-16

TM 43-0001-39

CUTTING ASSEMBLY, WINDOW (WCA): (MD33)



Use:

An explosive device used in the AH-IS(MOD) Helicopter Emergency Canopy RemovalSystem to assure exit from or access to the crewcompartment of the aircraft in an emergency.

Description:

Major components of the WCA are: mani-fold release assemblies and window cuttingretainer subassemblies for doors and windows,

linear explosive, resilient back-up cushion,retainer, and seal,

The assemblies are located on the periph-ery of the four windows in the crew compart-ment.

Functioning

Upon actuation of the system by armingand firing any one of the three armed/firingmechanisms, a detonation wave is received viathe interconnecting FCDC and SMDC lines tothe linear explosive of the WCA. The explosiveforce is outward, simultaneously cutting outthe four plastic window glasses of the crew com-partment,

5-17

TM 43-0001-39

Tabulated Data:


part number -----------------

Item Weight --------------------Width -----------------------------Height ----------------------------Length ---------------------------Method of actuation ---------

Body Material ------------------

1377-00-409-1096MD33857AS300-4

(97499) 209-030-711-35 (06331)813475-1045 lb (2.27 kg)32 in. (81.3 cm)5 in. (12.7 cm)62 in. (157,5 cm)High order detona-tion waveLead 6% antimonyalloy sheathed -

Propellant/explosive material:Type ----------------------------

Weight -------------------------

Performance:

Minimum detonationvelocity ------------------------

Packaging:


HNS, type II, gradeB0.004608 lb (32.3grains)

6050 meter/see at-65°F (-54°C)

MIL-B-81705Type II, heat sealedanti-static plasticbag

Dimensions ------------------- 72x 32x 5 in,Items per package ---------- 1Weight ------------------------- 3 lb

Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiber board boxDimensions ------------------- 6,63 x 3.29x 1.05 ftWeight ------------------------- 52 lbCube ---------------------------- 23.108 ft

Temperature Limits:

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)



group --------------------------- SDOT shipping class ----------- CDOT designation -------------- CLASS C EXPLO-

SIVE, HANDLECAREFULLYKEEP FIRE AWAY

References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

5-18

TM 43-0001-39




Use:

An explosive device used in the AH-1 S(MOD) Helicopter Emergency Canopy RemovalSystem to assure exit from or access to the crewcompartment of the aircraft in an emergency

Description:

foldMajor components of the WCA are: mani-release assemblies and window cutting

retainer sub-assemblies for doors and window,linear explosive, resilient back-up cushion,retainer, and seal.

The assemblies are located on the outeredge of the four windows in the crew compart-ment.

Functioning:

Upon actuation of the system by armingand firing any one of the three armed/firingmechanisms, a detonation wave is received viathe interconnecting FCDC and SMDC lines tothe linear explosive of the WCA. The explosiveforce is outward, simultaneously cutting outthe four plastic window glasses of the crew com-partment.

5-19

TM 43-0001-39

Tabulated Data:

NSN - - - - - - - - - - - --- - - - - - - - - - - DODIC ---------------------------Drawing number --------------Vendor (CAGE Code) and

part number -----------------


Body Material ------------------

1377-00-409-1095MD34857AS300-3

(97499) 209-030-711-29 (06331)813475-95 lb (2.27 kg)32 in. (81.3 cm)5 in. (12.7 cm)62 in. (157.5 cm)High order detona-tion waveLead 6% antimonyalloy sheathed


Weight -------------------------

Performance:


Packaging:


HNS, type II, gradeB0.003902 lb (27.3grains)

6050 meter/sec at-65°F (-54°C)




Temperature Limits:

Upper -----------------------------Lower -----------------------------

40x 70 in.15.00 lb

PPP-B-636Fiber board box5.60 X 3.42x 1.08 ft47 lb20.728 ft

+200°F (+93°C)-65°F (-54°C)




SIVE, HANDLECAREFULLY,KEEP FIRE AWAY

References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

5-20

TM 43-0001-39




Use:

An explosive device used in the AH-1 S(MOD) Helicopter Emergency Canopy RemovalSystem to assure exit from or access to the crewcompartment of the aircraft in an emergency.

Description:

foldMajor components of the WCA are: mani-release assemblies and window cutting



Functioning:

Upon actuation of the system by armingand firing any one of the three armed/firingmechanisms, a detonation wave is received viathe interconnecting FCDC and SMDC lines tothe linear explosive of the WCA. The explosiveforce is outward, simultaneously cutting outthe four plastic window glasses of the crew com-partment.

5-21

TM 43-0001-39

Tabulated Data:


part number -----------------


Body Material ------------------

1377-00-106-7773MD35857AS300-2

(97499) 209-030-711-29 (06331)813475-1025 lb (2.27 kg)32 in. (81.3 cm)5 in. (12.7 cm)62 in. (157.5 cm)High order detona-tion waveLead 6% antimonyalloy sheathed


Weight -------------------------

Performance:


Packaging:


HNS, type II, gradeB0.003902 lb (24,7grains)

6050 meter/sec at-65°F (-54°C)


Dimensions ------------------- 38x 65 in.Items per package ---------- 1Weight ------------------------- 3 lb

Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiber board boxDimensions ------------------- 15-1/2 X 40-1/2X

65-1/2 in.Weight ------------------------- 46 lbCube ---------------------------- 23.949 ft

Temperature Limits:

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)




SIVE, HANDLECAREFULLYKEEP FIRE AWAY

References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

5-22

TM 43-0001-39




Use:

An explosive device used in the AH-1 S(MOD) Helicopter Emergency Canopy RemovalSystem to assure exit from or access to the crewcompartment of the aircraft in an emergency.

Description:

Major components of the WCA are: mani-fold release assemblies and window cutting



Functioning:

Upon actuation of the system by armingand firing any one of the three armed/firingmechanism, a detonation wave is received viathe interconnecting FCDC and SMDC lines tothe linear explosive of the WCA. The explosiveforce is outward, simultaneously cutting outthe four plastic window glasses of the crew com-partment.

5-23

TM 43-0001-39

Tabulated Data:

NSN ----------------------------- 1377-00-106-1097DODIC --------------------------- MD36Drawing number -------------- 857AS300-1Vendor (CAGE Code) and

part number ----------------- (97499) 209-030-711-29 (06331)813475-101

Item Weight -------------------- 5 lb (2.27 kg)Width ----------------------------- 32 in. (81.3 cm)Height ---------------------------- 5 in. (12.7 cm)Length --------------------------- 62 in. (157.5 cm)Method of actuation --------- High order detona-



Type ---------------------------- HNS, type II, gradeB

Weight ------------------------- 0.004365 lb (30.6grains)

Performance:


-65°F (-54°C)

Packaging:

Inner Container:Reference --------------------- MIL-B-81705Type ---------------------------- Type II, heat sealed

anti-static plasticbag

Dimensions ------------------- 29,5 x 7 x 75.5 in.Items per package ---------- 1Weight ------------------------- 3 lb

Outer Container:Reference --------------------- PPP-C-636Type ---------------------------- Fiber board boxDimensions ------------------- 6.54 x 2.83x .98 ftWeight ------------------------- 50 lbCube ---------------------------- 18.138 ft

Temperature Limits:

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65° F (-54°C)




SIVE, HANDLECAREFULLY,KEEP FIRE AWAY

References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

5-24

TM 43-0001-39

CORD, DETONATING, ASSEMBLY, SHIELDED, MILD (SMDC): (MS47)


Refer to aircraft subsystem,

Use:


Description:

Major components of the SMDC Assemblyare threaded fitting, seals, washers, inner andouter ferrules, loaded booster shell, and silversheathed mild detonating cord.

Functioning:

Upon actuation of the system by armingand firing any one of the three armed/firingmechanisms, a detonation wave is received viathe junction manifold and is boosted by theloaded booster shell. The stimuli from thebooster actuates the HNS within the SMDCassembly,

NOTE

The MS47 thru MS62 are identical inphysical appearance and design, The dif-ference is in length and amount of explo-sive.

5-25

TM 43-0001-39

Tabulated Data:

NSN ----------------------------- 1377-00-410-8266DODIC --------------------------- MS47Drawing number -------------- 857AS400-15Vendor (CAGE Code) and

part number ----------------- (30003) 813475-15209-030-711-15

Item Weight -------------------- 0.268 lbDiameter ------------------------ 0,18 in.Length --------------------------- 32,0 in.Method of actuation --------- High order detona-

tion waveBody Material ------------------ Silver sheathed,

high fine silver99.95%

Propellant/explosive material:Type ---------------------------- HNS, type II, grade

AWeight ------------------------- 0,001860 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:


Type ---------------------------- Bag, sealedDimensions ------------------- 6 x 55 in.Items per package ---------- 1Weight ------------------------- 0.50 lb

Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiber board boxDimensions ------------------- 3.20 x 1.60x 1.08 ftWeight ------------------------- 15 lbCube ---------------------------- 5.530 ft

Temperature Limits:



group --------------------------DOT shipping class -----------DOT designation --------------

References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

1.4


5-26

TM 43-0001-39




Use:


Description:


Functioning:

Upon actuation of the system by armingand firing any one of the three armed/firingmechanisms, a detonation wave is received viathe junction manifold and is boosted by theloaded booster shell. The stimuli from thebooster actuates the HNS within the SMDCassembly.

NOTE

The MS47 thru MS62 are identical inphysical appearance and design. The dif-ference is in length and amount of explo-sive.

5-27

TM 43-0001-39

Tabulated Data: Packaging:


part number ----------------- (30003) 813475-15209-030-711-17

Item Weight -------------------- 0.227 lbDiameter ------------------------ .18 in,Length --------------------------- 30 in.Method of actuation --------- High order detona-




AWeight ------------------------- 0,001561 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Inner Container:Reference --------------------- MIL-B-117Type ---------------------------- Bag, sealedDimensions ------------------- 4 x 40 in.Items per package ---------- 1Weight ------------------------- 0.501 lb

Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiber board boxDimensions ------------------- 3.06 x 1.25 x .93 ftWeight ------------------------- 15 lbCube ---------------------------- 3.568 ft



group --------------------------- SDOT shipping class ----------- CDOT designation -------------- LINEAR SHAPED

CHARGE, METALCLAD, HANDLECAREFULLY,KEEP FIRE AWAY

References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

5-28

TM 43-0001-39



Refer to aircraft subsystem,

Use:


Description:


Functioning


NOTE


5-29

TM 43-0001-39

Tabulated Data:


part number -----------------


Body Material ------------------

1377-00-410-8222MS49857AS400-21

(30003) 813475-21209-030-711-210.389 lb0.18 in.34 in.High order detona-tion waveSilver sheathed,high fine silver99.95%


AWeight ------------------------- 0.002685 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:



MIL-B-117Bag, sealed6 x 47 in.10.50 lb

PPP-B-636Fiber board box3.62 X 3.29 × 1.33 ft20 lb11.464 cu ft




References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

1.4


5-30

TM 43-0001-39




Use:


Description (General all sizes)


Functioning


NOTE


5-31

TM 43-0001-39



part number ----------------- (30003) 813475-25209-030-711-25

Item Weight -------------------- 0.543 lbDiameter ------------------------ 0.18 in.Length --------------------------- 52 in.Method of actuation --------- High order detona-




AWeight ------------------------- 0.003856 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)


Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiber board boxDimensions ------------------- 3.50 x 4.75 x 1.37 ftWeight ------------------------- 17 lbCube ---------------------------- 22.776 cu ft





References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

5-32

TM 43-0001-39


Type Classification: Functioning

Refer to aircraft subsystem. Upon actuation of the system by armingand firing any one of the three armed/firing

Use: mechanisms, a detonation wave is received viathe junction manifold and is boosted by the

To provide an interconnecting explosiveloaded booster shell. The stimuli from thebooster actuates the HNS within the SMDC

media to the Window Cutting Assembly (WCA) assembly.of the gunner's canopy window used in theEmergency Canopy Removal System of the AH-1 series Helicopter.

Description: (General all sizes) NOTE

Major components of the SMDC Assembly The MS47 thru MS62 are identical inare threaded fitting, seals, washers, inner and physical appearance and design. The dif-outer ferrules, loaded booster shell, and silver ference is in length and amount of explo-sheathed mild detonating cord. sive.

5-33

TM 43-0001-39



part number ----------------- (30003) 813475-105209-033-011-105





AWeight ------------------------- 0,002872 lb

Performance:

Minimum detonationvelocity ------------------------ 6050 meter/sec at

-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)


Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiber board boxDimensions ------------------- 4.02 x 2.33x 2.54 ftWeight ------------------------- 20 lbCube ---------------------------- 23.791 cu ft




CHARGE, METALCLAD, HANDLECAREFULLYKEEP FIRE AWAY

References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

5-34

TM 43-0001-39




Use:




Functioning


NOTE


5-35

TM 43-0001-39

Tabulated Data:


part number -----------------


Body Material ------------------

1377-01-037-9237MS52857AS400-107

(30003) 813475-107116415-70.183 lb0.18 in.22 in.High order detona-tion waveSilver sheathed,high fine silver99.95%


AWeight ------------------------- 0.001455 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:


Outer Container:Reference --------------------- PPP-B-566Type ---------------------------- Fiber board boxDimensions ------------------- 3.0 x 1.18 x .98 ftWeight ------------------------- 15 lbCube ---------------------------- 3.461 cu ft




References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

1.4


5-36

TM 43-0001-39




Use:


Description: (General all sizes)


Functioning


NOTE

The MS47 thru MS62 are identical inphysical appearance and design, The dif-ference is in length and amount of explo-sive,

5-37

TM 43-0001-39

Tabulated Data:


part number ----------------- (30003) 813475-109116415-9




Type ---------------------------- HNS. type II. gradeA

Weight ------------------------- 0.001463 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:


Type ---------------------------- Bag. sealedDimensions ------------------- 24x 4 in.Items per package ---------- 1Weight -------------------------





References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385. App B

1.4

SCFLEXIBLELINEAR SHAPEDCHARGE,HANDLECAREFULLY)KEEP FIRE AWAY

5-38

TM 43-0001-39




Use:




Functioning


NOTE


5-39

TM 43-0001-39

Tabulated Data


part number -----------------


Body Material ------------------

1377-01-037-4096MS54857AS400-111

(30003) 813475-111116415-110.114 lb0.18 in.13 in.High order detona-tion waveLead 6% antimonyalloy sheathed


AWeight ------------------------- 0.001036 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:


Type ---------------------------- Bag, sealedDimensions - - - - - - - - - - - - - - - - 6 x 19 in.Items per package ---------- 1Weight -------------------------





References:

TM 9-1377-200-208zPTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

1.4

SCFLEXIBLELINEAR SHAPEDCHARGE,HANDLECAREFULLY,KEEP FIRE AWAY

5-40

TM 43-0001-39




Use:


Description:


Functioning:


NOTE


5-41

TM 43-0001-39

Tabulated Data:


part number ----------------- (30003) 813475-113116415-13




Type ---------------------------- HNS, type II, gradeA

Weight ------------------------- 0.001632 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:


Type ---------------------------- Bag, sealedDimensions ------------------- 6 x 48 in.Items per package ---------- 1Weight ------------------------- 0.50 lb




group --------------------------- SDOT shipping class ----------- CDOT designation -------------- FLEXIBLE

LINEAR SHAPEDCHARGE,HANDLECAREFULLYKEEP FIRE AWAY

References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

5-42

TM 43-0001-39




Use:


Description:


Functioning:


NOTE


5-43

TM 43-0001-39

Tabulated Data

NSN -----------------------------DODIC ---------------------------Drawing number --------------Vendor (CAGE Code) and

part number -----------------


Body Material ------------------

1377-01-037-4094MS56857AS400-115

(30003) 813475-115116415-150.248 lb0.18 in.33 in.High order detona-tion waveSilver sheathed,high fine silver99.95%


AWeight ------------------------- 0.001852 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:


Type ---------------------------- Plastic bagDimensions ------------------- 6 x 46 in.Items per package ---------- 1Weight ------------------------- 0.25 lb





References:

TM 9-1377-200-208zPTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

1.4


5-44

TM 43-0001-39




Use:


Description:


Functioning


NOTE


5-45

TM 43-0001-39

Tabulated Data:


part number ----------------- (30003) 116415-15813475-115





AWeight ------------------------- 0.002270 lb

Performance:


-65°F (-54°C)

Type ---------------------------- Bag, heat sealedDimensions ------------------- 6 x 65 in.Items per package ---------- 1Weight ------------------------- 0.50 lb






Firing Temperature Limits: References:Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C) TM 9-1377-200-20&P

TM 55-1520-221-23

Packaging:

Inner Container:

TM 55-1520-234-23TB 9-1300-385, App B

Reference --------------------- MIL-B-117

5-46

TM 43-0001-39




Use:


Description:


Functioning:


NOTE


5-47

TM 43-0001-39

Tabulated Data:


part number -----------------


Body Material ------------------

1377-01-032-3286MS58857AS400-119

(30003) 116415-19813475-1190.1151b0.18 in.20 in.High order detona-tion waveSilver sheathed,high fine silver99.95%


AWeight ------------------------- 0.001036 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:


Type ---------------------------- Bag, heat sealedDimensions ------------------- 4 x 22 in.Items per package ---------- 1Weight ------------------------- 0.25 lb

Outer Container:Reference --------------------- PPP-C-1672Type ---------------------------- Fiber board boxDimensions ------------------- 1.54 x 1.04x 0.27 ftWeight ------------------------- 2.0 lbCube ---------------------------- 0.464 cu ft




References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

1.4


5-48

TM 43-0001-39




Use:


Description:


Functioning:


NOTE


5-49

TM 43-0001-39

Tabulated Data


part number -----------------


Body Material ------------------

1377-01-032-3283MS59857AS400-125

(30003) 116415-25813475-1250,0197 lb0.18 in,27 in.High order detona-tion waveSilver sheathed,high fine silver99.95%


AWeight ------------------------- 0.0017631b

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:


Type ---------------------------- Bag, heat sealedDimensions ------------------- 4 x 43 in.Items per package ---------- 1Weight ------------------------- 0,25 lb






References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

5-50

TM 43-0001-39




Use:


Description:


Functioning:


NOTE


5-51

TM 43-0001-39

Tabulated Data:


part number ----------------- (30003) 116415-23813475-123





AWeight ------------------------- 0.001609 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65° F (-54°C)

Packaging:


Type ---------------------------- Bag. heat sealedDimensions ------------------- 6 x 53 in.Items per package ---------- 1Weight ------------------------- 0.25 lb

Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiber board boxDimensions ------------------- 3.64 x 1.33x 0.64 ftWeight ------------------------- 15.0 lbCube ---------------------------- 3.098 cu ft





References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

5-52

TM 43-0001-39




Use:


Description:


Functioning:


NOTE

The MS47 thru MS62 are identical inphysical appearance and design. The dif-ference is in length and amount of explo-s i v e .

5-53

TM 43-0001-39

Tabulated Data:


part number -----------------


Body Material ------------------

1377-01-032-3280MS61857AS400-121

(30003) 116415-21813475-1210.226 lb0.18 in,31 in.High order detona-tion waveSilver sheathed,high fine silver99.95%


AWeight ------------------------- 0.001543 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:


Type ----------------------------Dimensions -------------------Items per package ----------Weight -------------------------


Bag, heat sealed6 x 37 in.10.25 lb

PPP-B-636Fiber board box2.96 X 1.25X 0.93 ft12.0 lb3.441 cu ft




References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

1.4

scLINEAR SHAPEDCHARGE, METALCLAD, HANDLECAREFULLY,KEEP FIRE AWAY

5-54

TM 43-0001-39




Use:


Description:


Functioning:


NOTE


5-55

TM 43-0001-39

Tabulated Data:


part number -----------------


Body Material ------------------

1377-01-100-1718MS62857AS400-127

(30003) 116415-27813475-1270.065 lb0.18 in,8 in.High order detona-tion waveSilver sheathed,high fine silver99.95%


AWeight ------------------------- 0.000727 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:


Type ---------------------------- Bag, heat sealedDimensions ------------------- 4 x 16 in,Items per package ---------- 1Weight ------------------------- 0.25 lb





Reference:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

1.4


5-56

TM 43-0001-39

LINEAR EXPLOSIVE ASSEMBLY (LEA): (MS76)


Refer to aircraft subsystemNOTE

Use:The MS76 and MS77 are identical in phys-

The Linear-Explosive Assembly is used in ical appearance to the M79, The differ-the AH-1 E/F/P helicopter to explosively sever ence is in length and amount of explosive.the canopy door hinge in an emergency.

5-57

TM 43-0001-39

Tabulated Data:


part number -----------------Item Weight --------------------Diameter ------------------------Length ---------------------------Method of actuation ---------

Body Material ------------------

1377-01-032-1047MS766261062

115362-1816986-10.344 lb

N/A30.70 in.High order detona-tion waveLead 6% antimonyalloy sheathed -


AWeight -------------------------

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:

Inner Container:Reference --------------------- MIL-B-117Type ---------------------------- Bag, heat sealed

Dimensions ------------------- 4 x 37 in.Items per package ---------- 1Weight ------------------------- 0.25 lb





References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

1.4

SCFLEXIBLELINEAR SHAPEDCHARGE, METALCLAD, HANDLECAREFULLY,KEEP FIRE AWAY

5-58

TM 43-0001-39

LINEAR EXPLOSIVE ASSEMBLY (LEA): (MS77)


Refer to aircraft subsystemN O T E

Use:The MS76 and MS77 are identical in phys-

The Linear-Explosive Assembly is used in ical appearance to the M79, The differ-the AH-1 E/F/P helicopter to explosively sever ence is in length and amount of explosive.the canopy door hinge in an emergency.

5-59

TM 43-0001-39

Tabulated Data:

NSN ----------------------------- 1377-01-032-1048DODIC --------------------------- MS77Drawing number -------------- 6261062Vendor (CAGE Code) and

pmt. number ----------------- 115362 -3816986-3Item Weight -------------------- 0.0408 lbDiameter ------------------------ N/ALength --------------------------- 38.95 in.Method of actuation --------- High order detona-




Weight ------------------------- 0.006216 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:

Inner Container:Reference --------------------- MIL-B-117Type ---------------------------- Bag, heat sealed

Dimensions ------------------- 4 x 44 in.Items per package ---------- 1Weight ------------------------- 0.50 lb

Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiber board boxDimensions ------------------- 4.00 x 0.81 x 0.73 ftWeight ------------------------- 12.00 lbCube ---------------------------- 2.365 cu ft



group --------------------------- SDOT shipping class ----------- CDOT designation -------------- FLEXIBLE

LINEAR SHAPEDCHARGE, METALCLAD, HANDLECAREFULLY,KEEP FIRE AWAY

References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

5-60

TM 43-0001-39

LINEAR EXPLOSIVE ASSEMBLY, WINDOW (WCA): (MS78)



An explosive device used in the AH-1E/F/P Helicopter Emergency Canopy RemovalSystem to assure exit from or access to the crewcompartment of the aircraft in an emergency.

Major components of the WCA are: mani-fold release assemblies and window cuttingretainer subassemblies for doors and windows,linear explosive, extruded back-up cushion,retainer, and seal.

The assemblies are located on the periph-ery of the four windows in the crew compart-ment .

Functioning:

Upon actuation of the system by armingand firing any one of the three armed/firingmechanisms, a detonation wave is received viathe interconnecting LEA and SMDC lines tothe linear explosive of the WCA. The explosiveforce is outward? simultaneously cutting outthe four plastic window glasses of the crew com-partment.

NOTE

The MS76 and MS77 are identical in phys-ical appearance to the M79. The differ-ence is in length and amount of explosive,

5-61

TM 43-0001-39

Tabulated Data:

NSN ----------------------------- 1377-01-032-1049DODIC --------------------------- MS78Drawing number -------------- 6261063Vendor (CAGE Code) and

part number ----------------- 816987-103 115406-9

Item Weight --------------------Diameter ------------------------Length --------------------------- 55.25 in.Method of actuation --------- High order detona-




Weight ------------------------- 0.005070 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:


Type ---------------------------- Bag, heat sealedDimensions -------------------Items per package ---------- 1Weight -------------------------




group --------------------------- SDOT shipping class ----------- CDOT designation -------------- MILD

DETONATINGFUSE, METALCLAD, HANDLECAREFULLY,KEEP FIRE AWAY

References:

TM 9-1377-200 -20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

5-62

TM 43-0001-39

LINEAR-EXPLOSIVE ASSEMBLY, WINDOW (WCA): (MS79)



Use:

An explosive device used in the AH-1E/F/P Helicopter Emergency Canopy RemovalSystem to assure exit from or access to the crewcompartment of the aircraft in an emergency.

Description:

Major components of the WCA are: mani-fold release assemblies and window cuttingretainer subassemblies for doors and windows,linear explosive, extruded back-up cushion,retainer, and seal.


Functioning:

Upon actuation of the system by armingand firing any one of the three armed/firingmechanisms, a detonation wave is received viathe interconnecting LEA and SMDC lines tothe linear explosive of the WCA, The explosiveforce is outward? simultaneously cutting outthe four plastic window glasses of the crew com-partment.

NOTE

The MS78 is identical in design and physi-cal appearance to the MS79. The differ-ence is in length and amount of explosive.

5-63

TM 43-0001-39

Tabulated Data:


part number -----------------


Body Material ------------------

1377-01-032-1050MS796261063

816987-105115405-7

55.50 in.High order detona-tion waveLead 6% antimonyalloy sheathed


AWeight ------------------------- 0.005488 lb

Performance:


-65°F (-54°C)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:

Inner Container:Reference --------------------- MIL-B-117Type ---------------------------- Bag, heat sealedDimensions ------------------- 66x 35.5 in.Items per package ---------- 1Weight ------------------------- 3 lb





References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TB 9-1300-385, App B

1.4

SCHANDLECAREFULLY,KEEP FIRE AWAY

5-64

TM 43-0001-39

INERT CONNECTORS

Type Classification: interconnecting line assemblies from the nose(external) armed/firing mechanism.

Refer to helicopter subsystem.

Use:

Used in the AH-1 series helicopter canopyrelease system as detonation transfer mediabetween detonating cord sequencing systemassemblies, and as a means to secure the assem-blies to the aircraft structure.

Description:

Three types of inert connectors are usedas detonation transfers in the ballistic sequenc-ing system: the tee, cross, and in-line (union).

There is one tee connector, mountedbehind the gunner’s seat which serves as a junc-tion manifold for the crossover lines betweenthe right and left junction manifolds and the

The system has two cross connectors, onemounted in the upper right canopy structureand the other mounted in the upper left canopystructure. The cross connector mounted on theleft serves as a junction manifold for ballisticsequencing assemblies between the pilot’sarmed/firing mechanism, the WCA for the gun-ner’s door, and the tee connector behind the gun-ner’s seat, The cross connector mounted on theright serves as a junction manifold for ballisticsequencing assemblies between the gunner’sarmed/firing mechanism, the WCA for thepilot’s door, and the tee connector behind thegunner’s seat.

There is one in-line connector mounted atthe forward bulkhead in the nose section whichserves as a connector union between the SMDCassemblies interconnecting the nose (external)armed/firing mechanism, and the junction mani-fold mounted behind the gunner’s seat.

5-65

TM 43-0001-39

Tabulated Data: In-Line Connector:

Tee Connector:

NSN ----------------------------- 1377-00-410-8228Drawing number -------------- 857AS101-2Vendor (CAGE Code) and

part number ----------------- 813487-2 (30003)209-030 -711-9

Weight ---------------------------- 0.112 lbLength --------------------------- 1.680 in.Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . .0.760 in.Depth . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.050 in.

Cross Connector:

NSN ----------------------------- 1377-00-409-1101Drawing number -------------- 857AS102-1Vendor (CAGE Code) and

part number ----------------- 813488-1 (30003)209-030-711-7

Weight ---------------------------- 0.196 lbLength --------------------------- 1.680 in.Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.875 in.Depth ----------------------------- 1.480

NSN ----------------------------- 1377-01-062-4195Drawing number --------------Vendor (CAGE Code) and

part number ----------------- 819397-103Weight ---------------------------- 0.062 lbLength --------------------------- 1.650 in.Diameter ------------------------ 0.060 in.Diameter (hex end

fittings) ------------------------ 0.075 in.

Service Life:

There is no specific service life for inertconnectors because they consist of metal parts,(Refer to TB 9-1300-385, App B). However, dueto installation torques and possible damage dur-ing SMDC line removal, all connectors shouldbe checked for visible wear and tear and, if dam-aged, replaced.

Table 5-3 shows the detonating cord assem-blies, inert connectors, and detonators used inAH-1E/F/P/S (MOD) Army helicopters.

References:

TB 9-1300-385, Appendix B

5-66

TM 43-0001-39

CHAPTER 5

EMERGENCY ESCAPE SYSTEMS FORHELICOPTERS, AH-64

Section II. AH-64 (APACHE)

5-2. General (for Army AH-64 (Apache)Helicopters).

a. Section 2 of this chapter containsdescriptive and technical data pertaining to thesystems used for the Army AH-64 Helicopter.The system is used to explosively cut and ejectthe windows of the canopy and doors from thecanopy and door framing structure to provide arapid means of escape and/or access from/to thecrew compartment.

b. The AH-64 emergency canopy jetti-son system consists of four linear explosive can-opy severance assemblies which are installedaround the rim of the canopy windows and doorwindows of the crew compartment. Also, threearmed/firing initiators (fig. 5-4) and inter-connecting flexible confined detonating cord(FCDC) and shielded mild detonating cord(SMDC) lines. One arxned/firing initiator islocated in the pilot’s instrument panel to theleft of the glare shield, another is located in thegunner/copilots right console, and the third isin the nose of the helicopter which is located toprovide external access by rescue personnel.

Any one of the three armed/firing initiators canbe used to actuate the linear explosive escapesystem.

c. The detonating cord set consists ofnine SMDC lines; five FCDC lines and four can-opy severance assemblies. This chapterdescribes each assembly. Assemblies differ onlyin length and explosive weight. Table 5-4 is alist of the individual detonating cord lines, can-opy severance assemblies and arming/firing ini-tiators. Each explosive item includes theDepartment of Defense Identification Code(DODIC), Hughes Helicopter P/N, NationalStock Number (NSN), Vendor Part Number,Nomenclature, Drawing number, and explosiveweight.

d. This Section also contains descrip-tive information pertaining to the inert connec-tors in the AH-64 Helicopter canopy severancesystem. Table 5-5 has inert items with theNational Stock Number, Vendor Part Number(CAGE Code), Nomenclature, Drawing Numberand Quantity per helicopter.

5-67

TM 43-0001-39

Figure 5-3. AH-64 Emergency Canopy Jettison System Elements

5-68

TM 43-0001-39

TABLE 5-4. AH-64 HELICOPTER CANOPY SEVERANCE SYSTEM (EXPLOSIVE ITEMS)

**EXPLOSIVEDODIC *HUGHES NSN 1377-01- TECHNOLOGY NOMENCLATURE DRAWING EXPLOSIVE

PART NO.LENGTH

PART NO. NO. WEIGHT (LB) (INCHES)

MS80 7-311112017-17

MS81 7-311112017-15

MS82 7311112017-13

MS83 7-311112017-27

MS84 7-311112017-25

MS85 7-311112017-23

MS86 7-311112017-21

MS87 7-311112017-19

MS88 7-311112017-29

MS89 7-311112017-43

MS90 7-31111-2017-31

MS91 7-311112017-33

MS92 7-311112017-35

MS93 7-311112017-37

MS94 7-311112017-5

MS95 7-311112017-747X34.5X1.5

MS96 7-311112017-11

MS97 7-311112017-9

MT06 7-311112017-39

170-5244

170-5245

170-5246

170-5261

170-5262

170-5263

170-5264

170-5265

186-9898

170-5260

186-9899

186.9900

186-9901

186-9902

184-6112

185-6113

185-8908

187-4477

2696496

51134-47

51134-53

51134-51

51134-45

51134-57

51134-55

51134-23

51134-49

51134-35

51135-5

51135-1

51135-2

51135-7

51135-4

51188-1

51390-1

51391-1

41389-1

51207.3

CORD, DETONATING(SMDC)









CORD, DETONATING(FCDC)





CUTTING ASSEMBLYGUNNERS WINDOW

CUTTING ASSEMBLY

PILOT’S WINDOW

CUTTING ASSEMBLYPILOT’S DOOR

CUTTING ASSEMBLYGUNNERS DOOR

INITIATOR, MECHACTUATED JUA-59/A

841AS425-47

841AS425-53

841AS425-51

841AS425-45

841AS425-57

841AS425-55

841AS425-23

841AS425-49

841AS425-35

6260906-5

6260906-1

6260906-2

6260906-7

6206906-4

6206965-1

6260965-3

6260965-4

6260965-2

6260964

0.002028

0.000529

0.001587

0.002601

0.001829

0.000816

0.000529

0.000772

0.000506

0.003024

0.004800

0.007040

0.005104

0.004800

0.004321

0.004079

0.003814

0.003946

0.000269

51.0

4.0

29.0

59.0

36.0

9.0

4.0

8.0

3.0

9.45

15.0

22.0

15.95

15.0

71X24.5X1.5

44X33X1.5

66X23.5X1.5

5.4X2.75X1.9

* CAGE Code element** CAGE Code element

5-69

TM 43-0001-39

TABLE 5-5. AH-64 HELICOPTER CANOPY SEVERANCE SYSTEM (INSERT CONNECTORS)

**EXPLOSIVE*HUGHES NSN 1377-01 TECHNOLOGY NOMENCLATURE DRAWING QTY PERPART NO. PART NO. NO. A/C

7-311112017-3 170-5319 21738-3 CONNECTOR, TEE 6261072 5

7-311112017-41 170-5321 21602-2 CONNECTOR, 180 6261071 2DEGREE UNION

7-311112017-45 170-4493 23869-2 CONNECTOR ELBOW 6261073 1

* CAGE Code element** CAGE Code element

5-70

TM 43-0001-39



Standard.Refer to aircraft subsystem.

Use:

To provide an interconnecting explosivemedia to the canopy severance assemblies ofthe crew compartments in the EmergencyCanopy Removal System of the AH-64 series hel-icopter.

Description:

Major components of the SMDC Assemblyare threaded fittings, seals, washers, inner andouter ferrules, loaded booster shell, and silversheathed mild detonating cord.

Functioning:

Upon actuation of the system by armingand firing any one of the three armed/firing ini-tiators, a detonation wave is received via thejunction manifold and is boosted by the loadedbooster shell. The stimuli from the booster actu-

ates the HNS within the SMDC assembly to theadapter of the canopy severance assemblies.

Tabulated Data:

NSN . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DODIC ---------------------------Drawing number --------------CAGE Code and

part number -----------------

Item Weight --------------------Dimensions ---------------------Diameter ------------------------Length ---------------------------Method of actuation ---------

Body Material ------------------

1377-01-170-5244MS80841AS42547

7-311112017-1751134-47

51.0 in.High order detona-tion waveSilver sheathed,high fine silver99.95%

Propellant/explosive material:Type ---------------------------- HNS, type I, grade

AWeight ------------------------- 0.002028 lb

5-71

TM 43-0001-39

Performance: Temperature Limits:


-65°F (-54°C)

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Shipping and Storage Data:Packaging:

Inner Container:Reference --------------------- MIL-B-117Type ---------------------------- Bag, sealedDimensions ------------------- 6 x 65 in,Items per package ---------- 1 eaWeight ------------------------- 0.31 lb




SIVE, HANDLECAREFULLY,KEEP AWAYFROM FIRE,

References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B

5-72

TM 43-0001-39




Use:


Description:


Functioning:


Tabulated Data:


part number -----------------


Body Material ------------------

1377-01-170-5245MS81841AS425-53

7-311112017-1551134-53

High order detona-tion waveSilver sheathed,high fine silver99.95%


AWeight ------------------------- 0.000529 lb

5-73

TM 43-0001-39

Performance:


-65°F (-54°C)

Packaging:


Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiber board boxDimensions ------------------- 0.9 x 0.65x 0.65 in,Weight ------------------------- 3.0 lbCube ---------------------------- 0.38 cu ft

Temperature Limits:

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65° F (-54°C)




References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

1.4

SCCLASS C EXPLO-SIVE. HANDLECAREFULLY,KEEP AWAYFROM FIRE,

5-74

TM 43-0001-39



Standard,Refer to aircraft subsystem.

Use:


Description:


Functioning:

Upon actuation of the system by armingand firing any one of the three armed/firing ini-tiators, a detonation wave is received via thejunction manifold and is boosted by the loadedbooster shell, The stimuli from the booster actu-

ates the HNS within the SMDC assembly to theadapter of the canopy severance assemblies,

Tabulated Data:


part number -----------------


Body Material ------------------

1377-01-170-5246MS82841AS425-51

7-311112017-1351134-51

29.0High order detona-tion waveSilver sheathed,high fine silver99.95%


AWeight ------------------------- 0.001587 lb

5-75

TM 43-0001-39

Performance:


-65°F (-54°C)

Temperature Limits:

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65° F (-54°C)


Inner Container:Reference --------------------- MIL-B-117Type ---------------------------- Bag, sealedDimensions ------------------- 6 x 45 in.Items per package ---------- 1 eaWeight ------------------------- 0.24 lb




SIVE. HANDLECAREFULLY.KEEP AWAYFROM FIRE.

References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

5-76

TM 43-0001-39




Use:

To provide an interconnecting explosivemedia to the canopy severance assemblies ofthe crew compartments in the EmergencyCanopy Removal System of the AH-64 series hel-icopter,

Description:

Major components of the SMDC Assemblyare threaded fittings, seals, washers, inner andouter ferrules, loaded booster shell, and silversheathed mild detonating cord,

Functioning:


ates the HNS within the SMDC assembly toadapter of the canopy severance assemblies.

the

Tabulated Data:

NSN . . . . . . . . . . . . . . . . . . . . . . . . .DODIC ---------------------------Drawing number --------------CAGE Code and

part number -----------------


Body Material ------------------

1377-01-170-5261MS83841AS425-45

7-311112017-2751134-45



AWeight ------------------------- 0.002601

5-77

TM 43-0001-39



-65°F (-54°C)

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)







References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

5-78

TM 43-0001-39




Use:


Description:


Functioning:



Tabulated Data:


part number -----------------


Body Material ------------------

1377-01-170-5262MS84841AS425-57

7-311112017-2551134-57



AWeight ------------------------- 0.001829 lb

5-79

TM 43-0001-39



-65°F (-54°C)

Packaging:


Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiber board boxDimensions ------------------- 3.56 x 1.90x .98 ftWeight ------------------------- 17.0 lbCube ---------------------------- 6.63 cu ft

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65° F (-54° C)




SIVE, HANDLECAREFULLY.KEEP AWAYFROM FIRE.

References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

5-80

TM 43-0001-39




Use:

To provide an interconnecting explosivemedia to the canopy severance assemblies ofthe crew compartments in the EmergentCanopy Removal System of the AH-64 series hel-icopter.

Description:


Functioning:



Tabulated Data:

NSN . . . . . . . . . . . . . . . . . . . . . DODIC ---------------------------Drawing number --------------CAGE Code and

part number -----------------


Body Material ------------------

1377-01-170-5263MS85841AS425-55

7-311112017-2351134-55



AWeight ------------------------- 0.000816 lb

5-81

TM 43-0001-39



-65°F (-54°C)

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C







References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

5-82

TM 43-0001-39




Use:


Description:


Functioning:



Tabulated Data:


part number -----------------


Body Material ------------------

1377~01-170-5264MS86841AS425-23

7-311112017-2151134-23


Propellant/explosive material:Type ---------------------------- HNS, type I,

AWeight ------------------------- 0.000529 lb

grade

5-83

TM 43-0001-39

Performance:


-65°F (-54°C)

Packaging:



Temperature Limits:

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)





References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

5-84

TM 43-0001-39




Use:


Description:


Functioning:

Upon actuation of the system by armingand firing any one of the three armed/firing ini-tiators, a detonation wave is received via thejunction manifold and is boosted by the loadedbooster shell, The stimuli from the booster actu-


Tabulated Data:


part number -----------------


Body Material ------------------

1377-01-170-5265MS87841AS425-49

7-311112017-1951134-49



AWeight ------------------------- 0.000772 lb

5-85

TM 43-0001-39

Performance:


-65°F (-54°C)

Temperature Limits:

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)







References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

5-86

TM 43-0001-39



Standard. Refer to aircraft subsystem.

Use:


Description:


Functioning:



Tabulated Data:

NSN --------------------- DODIC ---------------------------Drawing number --------------CAGE Code and

part number -----------------


Body Material ------------------

1377-01-186-9898MS88841AS425-35

7-311112017-2951134-35



AWeight ------------------------- 0.000506 lb

5-87

TM 43-0001-39



-65°F (-54°C)

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)







References:

TM 9-1377-200-20&PTM 55-1520-238-23TM 9-1300-385, App B.

5-88

TM 43-0001-39

CORD, ASSEMBLY, DETONATING, FLEXIBLE CONFINED (FCDC): (MS89)



Use:

To provide an interconnecting explosivemedia to the canopy severance assemblies ofthe crew compartment doors and windows,

Description:

Major components of the flexible confineddetonating cord (FCDC) are housing, threadedfittings, seals, charge case, Hexanitrostibene(HNS), lead sheathed assembly

Functioning:

When the armed/firing initiators are actu-ated, the FCDC lines receive a detonating stimu-lus via a junction manifold and transmits it tothe canopy severance assemblies in the crewcompartments.

Tabulated Data:


part number -----------------


Body Material ------------------

1377-01-170-5260MS896260906-5

7-311112017-4351135-35

9.45 in.High order detona-tion waveLead 6% antimonyalloy sheathed


BWeight ------------------------- 0.003024 lb

5-89

TM 43-0001-39


When initiated, the energy output of theFCDC shall be substantial enought to cause0.020 inch minimum diametrical swelling of thewitness cap threaded onto the remote end ofthe FCDC assembly.

Packaging:


Outer Container:Reference --------------------- PPP-B-1672Type ---------------------------- Fiber board boxDimensions ------------------- 1.0 x .66x .21 ftWeight ------------------------- 2.0 lbCube ---------------------------- 0.3 cu ft

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)





References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

5-90

TM 43-0001-39




Use:

To provide an interconnecting explosivemedia to the canopy severance assemblies ofthe crew compartment doors and windows,

Description:

Major components of the flexible confineddetonating cord (FCDC) are housing, threadedfittings, seals, charge case, Hexanitrostilbene(HNS), lead sheathed assembly.

Functioning:


Tabulated Data:

NSN - - - - - - - - - - - - - - - - -DODIC ---------------------------Drawing number --------------CAGE Code and

part number -----------------


Body Material ------------------

1377-01-186-9899MS906260906-1

7-311112017-3151135-1

15.0High order detona-tion waveLead 6% antimonyalloy sheathed


BWeight ------------------------- 0.004800 lb

5-91

TM 43-0001-39


When initiated, the energy output of theFCDC shall be substantial enough to cause0.020 inch minimum diametrical swelling of thewitness cap threaded onto the remote end ofthe FCDC assembly.

Packaging:



Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65° F (-54°C)





References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

5-92

TM 43-0001-39




Use:

To provide an interconnecting explosivemedia to the canopy severance assemblies ofthe crew compartment doors and windows.

Description:

Major components of the flexible confineddetonating cord (FCDC) are housing, threadedfittings, seals, charge case, Hexanitrostilbene(HNS), lead sheathed assembly.

Functioning:


Tabulated Data:

NSN -------------- ------DODIC ---------------------------Drawing number --------------CAGE Code and

part number -----------------


Body Material ------------------

1377-01-186-9900MS916260906-2

7-311112017-3351135-2

22.0High order detona-tion waveLead 6% antimonyalloy sheathed

Propellant/explosive material:Type ---------------------------- HNS, type I,

BWeight ------------------------- 0.007040 lb

grade

5-93

TM 43-0001-39

Performance:


Packaging:

Inner Container:Reference --------------------- MIL-B-117Type ---------------------------- Bag, sealedDimensions ------------------- 24x 12 in.Items per package ---------- 1 eaWeight ------------------------- 0.18 lb

Outer Container:Reference --------------------- PPP-B-1672Type ---------------------------- Fiber board boxDimensions ------------------- 1.1 x 1,1 x 0.30 ftWeight ------------------------- 3.0 lbCube ---------------------------- 0.5 cu ft

Temperature Limits:

Upper ----------------------------- +200°F (+93° C)Lower ----------------------------- -65°F (-54°C)




References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

1.4

SCCLASS C EXPLO-SIVE. HANDLECAREFULLY.KEEP AWAYFROM FIRE.

5-94

T M 4 3 - 0 0 0 1 - 3 9




Use:


Description:

Major components of the flexible confineddetonating cord (FCDC) are housing, threadedfitting, seals, charge case, Hexanitrostilbene(HNS), lead sheathed assembly.

Functioning:


Tabulated Data:


part number -----------------


Body Material ------------------

1377-01-186-9901MS926260906-7

7-311112017-3551135-7

15,95High order detona-tion waveLead 6% antimonyalloy sheathed


BWeight ------------------------- 0.005104 lb

5-95

TM 43-0001-39



Packaging:

Inner Container:Reference --------------------- MIL.B.117Type ---------------------------- Bag, sealedDimensions ------------------- 16x 12 in,Items per package ---------- 1 eaWeight ------------------------- 0.15 lb


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)





References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

5-96

TM 43-0001-39




Use:


Description:

Major components of the flexible confineddetonating cord (FCDC) are housing, threadedfittings, seals, charge case, Hexamtrostilbene(HNS), lead sheathed assembly.

Functioning:


Tabulated Data:

NSN ----------------------------- 1377-01-186-9902DODIC --------------------------- MS93Drawing number -------------- 6260906-4CAGE Code and

part number ----------------- 7-311112017-3751135-4

Item Weight --------------------Dimensions ---------------------Diameter ------------------------Length --------------------------- 15.0Method of actuation --------- High order detona-

tion waveBody Material ------------------ Lead 6’% antimony


Type ---------------------------- HNS, type I, gradeB

Weight ------------------------- 0.004800 lb

5-97

TM 43-0001-39

Performance:


Packaging:

Inner Container:Reference --------------------- MIL-B-117Type ---------------------------- Bag, sealedDimensions ------------------- 16x 12 in.Items per package ---------- 1 eaWeight ------------------------- 0.14 lb

Outer Container:Reference --------------------- PPP-B-1672Type ---------------------------- Fiber board boxDimensions ------------------- 1.5 x 1,0x 0.21 ftWeight ------------------------- 3.0 lbCube ---------------------------- 0.3 cu ft

Temperature Limits:

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65° F (-54°C)




References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

1.4

SCCLASS C EXPLO-SIVE. HANDLECAREFULLY.KEEP AWAYFROM FIRE.

5-98

TM 43-0001-39

CANOPY SEVERANCE ASSEMBLY FORWARD PANEL: (MS94)



Use:

An explosive device used in the AH-64 heli-copter emergency canopy severance system toprovide quick exit from, or access to the crewcompartments of the aircraft in an emergency

Description:

Major components of the canopy severanceassembly are charge retainer, charge holder,sleeve booster, initiation block, linear explosiveand nameplate.

Functioning:

Upon actuation of the system by any one ofthe armed/firing initiators, a detonation wave is

received via the interconnecting FCDC andSMDC lines to the canopy severance assem-blies. The explosive force of the linear explo-sive charge is outward, thus severing the plasticpanels of the crew compartments.

Tabulated Data:

NSN -------------------------------DODIC ---------------------------Drawing number --------------CAGE Code and part

number ------------------------

Item weight ---------------------Dimensions ----------------------Diameter -------------------------Length ----------------------------Method of actuation ----------

Body Material ------------------

1377-01-184-6112MS946260965-1

7-311112017-551188-1

High order detona-tion waveLead 6% antimonyalloy sheathed

Change 2 5-99

TM 43-0001-39

Propellant/ExplosiveMaterial:Type ---------------------------- HNS, type II, grade

Weight -------------------------- 0.000269 lb

Performance:

Minimum detonationvelocity ------------------------- 6050 meters/sec at

-65°F (-54°C)

Packaging:

Inner Container:Reference ---------------------- MIL-B-117Type ---------------------------- Bag, sealedDimensions ------------------- 85 x 45 m.Items per package ---------- 1 eaWeight -------------------------- 1.83 lb

Outer Container:Reference ---------------------- PPP-B-636Type ---------------------------- Fiberboard boxDimensions ------------------- 6.65 x 2.56x 0.98 ft

Weight -------------------------- 50.0 lbCube ---------------------------- 16.67 cu ft

Temperature Limits:

Upper ----------------------------- +200°F (+93°CLower ----------------------------- -65°F (-54°C)


Quantity distance class ------ 1.4Storage compatibilitygroup . . . . . . . . . . . . . . . . . . . . . . . . SDOT shipping class ----------- CDOT designation -------------- CLASS C EXPLO-

SIVE, HANDLECAREFULLY,KEEP AWAYFROM FIRE

References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B

5-100 Change 2

TM 43-0001-39

CANOPY SEVERANCE ASSEMBLY REAR (AFT) PANEL: (MS95)



Use:

An explosive device used in the AH-64 heli-copter emergency canopy severance system toprovide quick exit from, or access to the crewcompartments of the aircraft in an emergency.

Description:

Major components of the canopy severanceassembly are charge retainer, charge holder,sleeve booster, initiation block, linear explosiveand nameplate.

Functioning:

Upon actuation of the system by any one ofthe armed/firing initiators, a detonation wave is

received via the interconnecting FCDC andSMDC lines to the canopy severance assem-blies. The explosive force of the linear explo-sive charge is outward, thus severing the plasticpanels of the crew compartments.

Tabulated Data:

NSN -------------------------------DODIC ---------------------------Drawing number --------------CAGE Code and part

number ------------------------

Item weight ---------------------Dimensions ----------------------Diameter -------------------------Length ----------------------------Method of actuation ----------

Body Material ------------------

1377-01-184-6113 MS956260965-3

7-311112017-751390-1


Change 2 5-101

TM 43-0001-39

Propellant/ExplosiveMaterial:Type ---------------------------- ENS, type II, grade

Weight -------------------------- 0.004079 lb

Performance:

Minimum detonationvelocity ------------------------- 6050 meters/see at

-65°F (-54°C)

Packaging:

Inner Container:Reference ---------------------- MIL-B-117Type ---------------------------- Bag, sealedDimensions ------------------- 60 x 45 in.Items per package ---------- 1 eaWeight -------------------------- 1.66 lb

Outer Container:Reference ---------------------- PPP-B-636Type ---------------------------- Fiberboard boxDimensions ------------------- 4.65 x 3.4x 0.94 ft

5-102 Change 2

Weight -------------------------- 50.0 lb---------------------------- 14.85 cu ft

Temperature Limits:

Upper ----------------------------- +200°F (+93°CLower ----------------------------- -65°F (-54°C)


Quantity distance class ------ 1.4Storage compatibility


SIVE, HANDLECAREFULLY,KEEP AWAYFROM FIRE

References:

TM 9-1377 -200-20&PTM 55-1520-238-23TB 9-1300-385, App B

*U.S. GOVERNMENT PRINTING OFFICE: 1994- 546.043/00706

PIN 058915-002

TM 43-0001-39

CANOPY SEVERANCE ASSEMBLY REAR (AFT) PANEL: (MS96)



Use:


Description:

Major components of the canopy sever-ance assembly are: charge retainer, chargeholder, sleeve booster, initiation block, linearexplosive and nameplate.

Functioning:

Upon actuation of the system by any oneof the armed/firing initiators, a detonationwave is received via the interconnecting FCDCand SMDC lines to the canopy severance assem-blies, The explosive force of the linear explo-

sive charge is outward, thus severing the plasticpanels of the crew compartments.

Tabulated Data:


part number -----------------


Body Material ------------------

1377-01-185-8908MS96626095-4

7-311112017-1151391-1


Propellant/explosive material:Type ---------------------------- HNS, type II grade

BWeight ------------------------- 0.003814 lb

5-103

TM 43-0001-39


Minimum detonationvelocity ------------------------ 6050 meters/sec at

-65°F (-54°C)

Upper ----------------------------- +200oF (+93oC)Lower ----------------------------- -65°F (-54°C)



Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiber board boxDimensions ------------------- 4.35 x 3.27 x .94 ftWeight ------------------------- 50.0 lbCube ---------------------------- 13.4 cu ft




References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

5-104

TM 43-0001-39

CANOPY SEVERANCE ASSEMBLY FORWARD PANEL: (MS97)



Use:


Description:

Major components of the canopy sever-ance assembly are: charge retainer, chargeholder, sleeve booster, initiation block, linearexplosive and nameplate.

Functioning:

Upon actuation of the system by any oneof the armed/firing initiators, a detonationwave is received via the interconnecting FCDCand SMDC lines to the canopy severance assem-blies. The explosive force of the linear explo-

sive charge is outward, thus severing the plasticpanels of the crew compartments.

Tabulated Data:

NSN ----------------------------- 1377-01-187-4477DODIC --------------------------- MS97Drawing number -------------- 6260965-2CAGE Code and

part number ----------------- 7-311112017-951389-1

Item Weight --------------------Dimensions ---------------------Diameter ------------------------Length ---------------------------Method of actuation --------- High order detona-



Type ---------------------------- HNS, type II, gradeB

Weight ------------------------- 0.000269 lb

5-105

TM 43-0001-39



-65°F (-54°C)

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Shipping and Storage DataPackaging:


Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiber board boxDimensions ------------------- 6.19 x 2.48 x .94 ftWeight ------------------------- 50.0 lbCube ---------------------------- 14.4 cu ft




References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

5-106

TM 43-0001-39

ARMING/FIRING INITIATOR JUA-59: (MT06)



Use:

A mechanically actuated detonator-type ini-tiator used to actuate the emergency canopy sev-erance system on the AH-64 helicopter.

Description:

The arming/firing initiator is a mechani-cally actuated percussion-type detonator consist-ing of a body handle assembly, firing pin, M42primer, a demolition transfer charge assembly,seals and a fitting port.

Functioning:

The initiator handles are turned andpushed to actuate the initiators. The handlescan be rotated in either direction 90° to armthe initiator. As the handle is pushed, the

spring behind the firing pin is compressed. At0.3 in. (0.76 cm) fo travel, lock balls release thefiring pin, and it strikes the primer. Theprimer ignites the lead azide transfer charge,which in turn ignites the main charge of HNS.

Tabulated Data:

NSN ----------------------------- 1377-01-269-6496DODIC --------------------------- MT06Drawing number -------------- 6260964CAGE Code and

part number ----------------- 17610/51207-3Item Weight --------------------Dimensions --------------------- 1.875 in.Diameter ------------------------ 5.4 in.Length ---------------------------Method of actuation --------- MechanicalBody Material ------------------ SteelPropellant/explosive material:

Type ---------------------------- HNS, type I, gradeA

Weight ------------------------- 0.000269 lb

5-107

TM 43-0001-39



-65°F (-54°C)

Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)







References:

TM 9-1377-200-20&PTM 55-1520-238-23TB 9-1300-385, App B.

5-108

TM 43-0001-39

INERT CONNECTORS


Use:

Used in the AH-64 series helicopter can-opy release system as detonation transfermedia between between system assemblies, andas a means to secure the assemblies to the air-craft structure.

Description:

Three types of inert connectors are usedas detonation transfers in the system: the tee,the elbow, and the union.

Tabulated Data:

CONNECTOR, IN-LINE, UNION

NSN ----------------------------- 1377-01-170-5321Drawing no. -------------------- 6261071CAGE Code and part

no. ----------------------------- 7-311112017-4121601-2

Quantity per aircraft -------- 2

CONNECTOR, ELBOW

NSN . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Drawing no. --------------------CAGE code and part

no. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Quantity per Aircraft --------

CONNECTOR, TEE

NSN -----------------------------Drawing no. --------------------CAGE Code and part

no. --------------- -----------------

Quantity per aircraft --------

Service Life:

1377-01-170-53196261073

7-311112017-4523869-21

1377-01-170-53196261072

7-311112017-321738-35

INERT - Item is assembly of metal partonly. Replacement is determined by “OnCondition” (OC), after inspection for visiblewear or defect.

5-109 (5-110 blank)

TM 43-0001-39

CHAPTER 6

IMPULSE CARTRIDGES

6-1 General These cartridges shall be used only for their des-ignated application.

a. The Impulse Cartridges described inthis chapter have a wide range of application,

b. The Impulse Cartridges listed in this

characteristics, and physical appearances.chapter are grouped by their method of initia-tion; (1) electrical and (2) percussion.

6-1 (6-2 blank)

TM 43-0001-39

CARTRIDGE, IMPULSE, MARK 19 Mod 0: (MO12)

Type Classification

Refer to Aircraft Subsystem.

Use:

Used as the power source in storesrelease/ejector systems on aircraft.

Description:

This is an electrically initiated, case-grounded, screw-in type cartridge, consisting ofa body, Mark 11 Mod 0 ignition element, hollowmetal plug and main charge, The open end iscrimped over a sealing disc. The electrode ofthe ignition element is separated from the bodyby an insulator. A hollow metal plug isthreaded inside the body, between the igniterassembly and the propellant. The cartridge islocated in the firing breech of the mechanism itis to operate.

Functioning:

When the cartridge is fired, the resultinggas pressure operates the store release/ejectormechanism.

Tabulated Data:


part number -----------------Item weight ---------------------Diameter ------------------------

Length ---------------------------

Method of actuation ---------

1377-00-793-9926MO122164465

(10001) LD4197000.038 lb (0.017 kg)0.805 in.(2.045 cm)1.471 in.(3.736 cm)Electrical 5amperes

6-3

TM 43-0001-39

Body material ------------------ Aluminum alloyPropellant/explosive material:

Type --------------------------- Smokeless powder,HPSK 5250.95

Weight ------------------------- 0.0021 lb (14.77grains)

Performance:

600 Explosive Power Rating


Upper ----------------------------- +160°F (+71°C)Lower ----------------------------- -65°F (-54°C)

Packaging:

Inner Container:Reference --------------------- PPP-P-291Type ---------------------------- Bag, heat sealedDimension -------------------- 2.25 wide x 2.062

depth in. (6.41wide x 5.24 depth)

Items per package ---------- 2

Weight ------------------------- 0.25 lbOuter Container:

Reference --------------------- PPP-C-1672Type ---------------------------- Fiberboard boxDimension -------------------- 1.54 x 1.04 x 0.27 ftWeight ------------------------- 2.00 lbCube ---------------------------- .464 cu ft



group --------------------------- SDOT shipping class ----------- CDOT designation -------------- Small Arms

Ammunition,Handle Carefully,Keep Fire Away

References:

TM 9-1377-200-20&PTM 55-1510-204-23TM 55-1510-213-23TB 9-1300-385, App B

6-4

TM 43-0001-39

CARTRIDGE, IMPULSE: (M162)



Use:

To actuate a helicopter hoist cable cutterto cut and release a steel hoist cable and itsload, in an emergency (CH-47).

Description:

The impulse cartridge is an electrically ini-tiated cartridge. The contact pin which extendsfrom the firing end of the cartridge case is con-

nected to a wire within the powder chamber.The other end of the wire is connected to the car-tridge case adjacent to the steel cutting punch.The design and contour of the cutting edge ofthe captive cutting punch is such that thepunch cuts and wedges the severed ends of thereeved portion of the hoist cable in the cutter toprevent whiplash.

The cartridge is oriented to the correctposition in the cable cutter by a flat surface onthe rim of the cartridge case. This flat surfaceensures that the captive cutting punch strikesthe anvil of the cable cutter and wedges thereeved end of the hoist cable.

6-5

TM 43-0001-39

Functioning:

When the cable cutter switch is operated,electrical current initiates the cartridge in thecable cutter. The expanding gas from the car-tridge forces the punch against one side of thecable as the other side of the hoist cable isforced against the anvil in the cable cutter. Thecutting edge of the punch severs and releasesthe cable and its load from the hoist. The cut-ting punch also secures the reeved end of thehoist cable in the cable cutter. thus preventingwhiplash.

Tabulated Data:

NSN -------------------------------DODIC ---------------------------Drawing number --------------Vendor (CAGE Code) and

part number -----------------Item weight ---------------------Diameter ------------------------Length ---------------------------Method of actuation ---------

Body material ------------------

1377-00-999-7463M1622518426

(40912) MSA967130.04 lb (0.02 kg)0.500 in. (1.27 cm)2.109 in. (5.36 cm)Electrical 5amperesBrass

Propellant/explosive material:Type ---------------------------- Double baseWeight ------------------------- 0.0003 lb (2.10

grains)

Performance:


Upper ----------------------------- +160°F (+71°C)Lower ----------------------------- -65°F (-54°C)

Packaging:


Dimensions -------------------

Items per package ----------Outer Container:

Reference ---------------------Type ----------------------------Dimensions -------------------

Weight -------------------------Cube ----------------------------

MIL-C-10464Type 1 hermeti-cally sealed metalcontainer2.625 x 2.625 × 1.5in.2

PPP-C-1672Fiberboard box17 x 12 x 9 in.(43.18 x 30.48 x22.86 cm)2 lb0.464 cu ft



group --------------------------- SDOT shipping class ----------- CDOT designation -------------- Small Arms

Ammunition, ClassC Explosive,Handle Carefully,Keep Fire Away

References:

TM 9-1377-200-20&PTM 55-1520-209-23TM 55-1520-227-23TB 9-1300-385, App B

6-6

TM 43-0001-39

CARTRIDGE, IMPULSE: ARD-863-1 (M189)



Use:

For external stores ejection on the AH-1series helicopter.

Description:

The ARD-863-1 Impulse Cartridge is astandardized store ejection and release car-

tridge and consists of a cylindrical aluminumalloy case and ignition element (electrode,bridgewire, and ignition charge) and a separa-tion disc. The CCU-44/B Impulse CartridgeNSN-1377-01-033-2622 (MD66) is a suitable sub-stitute for the ARD-863-1 (M189).

Functioning:

Upon receipt of an electrical signal the igni-tion element is fired and the resulting gas pres-sure ignites the main charge. When sufficientpressure is developed, the closure disc rupturesand the released gas pressure actuates therelease/ejector mechanism.

6-7

TM 43-0001-39

Tabulated Data:

NSN ----------------------------- 1377-01-057-0686DODIC --------------------------- M189Drawing number -------------- N/AVendor (CAGE Code) and

part number ----------------- (80236) ARD-863-1(79495) P7911-2

Item weight ---------------------Diameter ------------------------ 1.075 in.

(2.731 cm)Length --------------------------- 1.03 in. (2.616 cm)Method of actuation --------- Electrical 5

amperesBody material ------------------ AluminumPropellant/explosive material:

Type ---------------------------- Double base, 2.75gm BoosterCharge, 1.15 gm

Weight ------------------------- 0.0090 lb (63grains)

Performance:


Upper -----------------------------Lower -----------------------------

Packaging:


+160°F (+71°C)-65°F (-54°C)

MIL-C-10464Type 1 hermeti-cally sealed metalcontainer


Outer Container:Reference ---------------------Type ----------------------------Dimensions -------------------

Weight -------------------------Cube ----------------------------

3.5 x 3 (dia)80.188 lb(0.0853 kg)

PPP-B-636Fiberboard box8.25 x 8.25 x 14.5in. (21 x 21 x36.82 cm)2 lb (0.9072 kg)0.57 cu ft




References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-237-23TM 55-1520-236-23TB 9-1300-385, App B

1.4

CCSmall ArmsAmmunition, ClassC Explosive,Handle Carefully,Keep Fire Away

6-8

TM 43-0001-39



Refer to Aircraft Subsystem.The M253 Impulse Cartridge consists of a

Use: steel case, two electrodes, bridgewire, ignition

Used in the Holex cable cutter on theelement, main charge, and closure assembly.

Army CH-54A helicopter cargo hoist cable sys-The M253 is sometimes referred to as the explo-

tem.sive bolt.

6-9

TM 43-0001-39

Functioning:

Upon receiving an electric current, thebridgewire attached to the electrical pins heatsand ignites the primer. The primer in turnignites the main charge. The pressure devel-oped by the main charge propels the cutterblade with sufficient force to sever the mainhoist cable, a 7/8-inch (2.22 cm) special steelcable.

Tabulated Data:

NSN ----------------------------- 1377-00-878-6510DODIC --------------------------- M253Drawing number --------------Vendor (CAGE Code) and

part number ----------------- (10640) R 4181-1Item weight ---------------------Diameter ------------------------ 1 in. (2.54 cm)Length --------------------------- 2.62 in. (6.67 cm)Method of actuation --------- ElectricalBody material ------------------ SteelPropellant/explosive material:

Type ---------------------------- HI TEMPWeight ------------------------- 0.004206 lb (29.442

grains)

Performance:


Upper ----------------------------- +160°F (+71°C)Lower ----------------------------- -65°F (-54°C)

Packaging:

Inner Container:Reference --------------------- MIL-B-117Type ---------------------------- Barrier bagDimensions ------------------- 8 x 5 in.Items per package ---------- 1Weight ----------------------------- 0.25 lb

Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiberboard boxDimensions ------------------- 1.6 x 1.05 x 0.30 ftWeight ------------------------- 2 lbCube ---------------------------- 0.464 cu ft




References:

TM 9-1377 -200 -20&PTM 55-1520-209-23TM 55-1520-227-23TB 9-1300-385, App B

1.4

SCExplosive ReleaseDevice, Class CExplosive, HandleCarefully, KeepFire Away

6-10

TM 43-0001-39

CARTRIDGE, IMPULSE, MARK 104 Mod 0: (M291)


ATC-S LCC-A.Refer to Aircraft subsystem.

Use:

To actuate a telescoped catapult EjectionSeat Trainer Device. The device is used totrain pilots and crew members on procedures tobe followed when ejecting from an aircraft dur-ing an emergency.

NOTE

Impulse cartridges Mark 103 Mod 0,Mark 104 Mod 0 and Mark 3 Mod 1 areidentical in general appearance, diame-ter, and length. Each of these threetypes of cartridges is designed for a differ-ent purpose and contains a different quan-tity of propellant. Impulse cartridgeMark 104 Mod 0 shall be used only in thecatapult of the ejection seat trainerdevice for which it was designed.

6-11

TM 43-0001-39

Description

The M291 Mark 104 Mod 0 ImpulseCartridge case has a cup-type case crimped overa head with an O-ring gasket for sealing. A lac-quer sealed 50M percussion primer is recessedin the head. The steel igniter tube is screwedinto the head and separated from the primer by abrass washer. A steel plug is screwed into oneend of the igniter tube and is staked to a disc-shaped aluminum trap having holes for theescape of the propellant gases.

Functioning

To operate the catapult, the trainee,seated in the ejection seat of the trainingdevice, reaches up with both hands and pullsthe handle of the face curtain at the top of theseat. Movement of the curtain pulls a cablewhich releases a spring-loaded firing pin at thetop of the catapult. Firing of the cartridgebuilds up pressure in the catapult, thrustingthe seat and occupant upward along the railswith a minimum of 6 g’s, simulating the effectof ejecting from an aircraft. The seat deceler-ates to a stop at a height of less than 20 feetand before reaching the top of the tower.

Tabulated Data:

NSN --------------------------- -----DODIC ---------------------------Drawing number --------------Vendor (CAGE Code) and


1377-00-707-0590M2911863079

(10001) LD491831

2.06 in. (5.232 cm)5.42 in. (13.77 cm)Percussion primerAluminum

Propellant/explosive material:Type ---------------------------- Black powder, HES

5250Weight ------------------------- 0.0705 lb (493.5

grains)

Performance:

18900 ft-lb Explosive Power Rating


Upper -----------------------------Lower -----------------------------

Packaging


Dimensions -------------------

Items per package ----------Outer Container:

Reference ---------------------Type ----------------------------Dimensions -------------------

Weight -------------------------Cube ----------------------------

+160°F (+71°C)-65°F (-54°C)

MIL-C-10464Type I hermetical-ly-sealed metalcontainer6.0 x 2.532 in dia(15.24 x 6.432 cmdia)1

PPP-B-621Wood box13.375 x 9.0 x 7.25in. (33.97 x 22.86 x18.42 cm)13 lb (5.897 kg)0.5 cu ft




References:

TM 9-1377-200-20&PTB 9-1300-385, App B

1.4

CCSmall ArmsAmmunition,Handle Carefully,Keep Fire Away

6-12

TM 43-0001-39

CARTRIDGE SET, IMPULSE, REDUCED CHARGE, PRIMARY: (M397)



Use:

The reduced charge cartridge set is in theMartin-Baker ejection seat and consists of onereduced charge primary catapult cartridge andtwo secondary catapult cartridges which, whenfired in sequence, provide recoil forces and ballis-tic gases sufficient to eject the seat and its occu-pant from the aircraft in an emergency.

Description:

Components of the reduced charge pri-mary catapult cartridge are copper disc, andbrass and rubber washers, metal case, and a per-cussion cap primer. Components of each of thetwo secondary catapult cartridges are brasscover with a 0.75-inch hole covered with a0.003-inch thick copper disc, rubber sealingring, and brass case. The secondary cartridgesrequire no primer or booster.

Functioning:

The ejection process is actuated when theoccupant of the ejection seat pulls a fabricblind, to which a cable is attached, down overhis face. This action causes the cable to with-

draw a sear from the firing mechanism of theejection gun which releases a spring-loaded fir-ing pin. Movement of the firing pin initiatesthe percussion primer of the primary catapultcartridge; flame then passes through two ventopenings, igniting the booster, which ignites themain charge of the primary catapult cartridge.

When the reduced charge primary cata-pult cartridge fires, recoil pressure forces theinner tube to cam the springloaded plunger outof the seat locking latch window. This latchretains the ejection seat in the aircraft.

Inner and intermediate tubes of the ejec-tion gun rise together, raising the ejection seataway from the floor of the cockpit. After 14inches of movement, a port in the outer tube isuncovered, exposing the lower secondary cata-pult cartridge at the upper half of the barrel.After a total movement of 39.35 inches, theintermediate tube is stopped by a flange. Thesefirings eject the top unit of the barrel (togetherwith the seat and occupant) from the cockpit;the two extended telescoping units remainattached to the floor of the aircraft.

6-13

TM 43-0001-39

CARTRIDGE SET, IMPULSE, REDUCED CHARGE, PRIMARY: M397

6-14

TM 43-0001-39

Tabulated Data

NSN --------------------------------DODIC ---------------------------Drawing number --------------Vendor (CAGE Code and

part number -----------------

Item weight ---------------------

Diameter ------------------------

Length ---------------------------


Body material ------------------

1377-00-845-5242M3972519696

(MBEU) 26434-1 (1ea) (MBEU)29434-2 (2 ea)0.03164 lb(0.01435 kg)Primary 1.843 in.(4.681 cm)Secondary 3.27 in.(8.306 cm)Primary 2.574 in.(6.538 cm)Secondary 0.610 in.(1.549 cm)Primary - percus-sion primer;Secondary - pres-sure and heat fromprimaryBrass

Propellant/explosive material:Type ---------------------------- Nitrocellulose,

black powderWeight ------------------------- 0.0815 lb (570.5

grains)

Performance:


Upper ----------------------------- +160°F (+71°C)Lower ----------------------------- -65°F (-54°C)

Packaging:


Dimensions -------------------


MIL-P-116Type IHermetically seal-ed metal container3.27 x 3.27 x 3 in.(8.306 x 8.306 x7.62 cm)1 set0.5 lb (0.227 kg)




References:

TM 9-1377-200-20&PTM 55-1510-204-23TM 55-1510-213-23TB 9-1300-385, App B

1.4

SCEXPLOSIVEPOWER DEVICE,CLASS C,HANDLECAREFULLY,KEEP FIRE AWAY

6-15 (6-16 blank)

TM 43-0001-39

CARTRIDGE, IMPULSE DROGUE: (M507)



Use:

Used in a drogue gun on the Martin-Baker ejection seat to automatically operate thegun which releases two drogue parachutes afterthe seat and occupant are ejected from the air-craft in an emergency escape.

Description:

Components of the drogue impulse car-tridge are: metal case, percussion cap primer,brass disc, and neoprene washer. The primer isencased in tinfoil and requires no anvil. Ananvil is machined into the primer cavity of thecase.

Functioning:

When the ejection catapult ejects the seatand occupant free of the aircraft, a trip rodattached to the bulkhead removes a sear pinfrom the drogue gun.

When the sear has been pulled, and amechanically induced delay time (determinedby sear series) has expired, the percussion capin the cartridge is fired by a blow from the fir-ing pin actuated by a compression spring.When the percussion cap fires, the gaseousflame is forced through two vents leading to thepowder chamber, igniting the main charge. Theresultant gases expand and force a piston mem-ber out of the top of the drogue gun. As the pis-ton leaves the gun, a shackle attached to thetop of the piston and to a drogue withdrawalline, pulls out an 18-inch controller drogue (par-achute) and a 60-inch stabilizer drogue from astowage compartment at the top of the seat.

Tabulated Data:

NSN --------------------------

DODIC ---------------------------Drawing number --------------Vendor (CAGE Code and

part number -----------------Item weight ---------------------

1377-00-883-89971377-00-960-0453M5072520002

(MBEU) 7536-10.0922 lb (0.042kg)

6-17

TM 43-0001-39

Diameter ------------------------ 0.705 in. (1.791cm)

Length --------------------------- 2.420 in. (6.147cm)

Method of actuation --------- Percussion primerBody material ------------------ BrassPropellant/explosive material:

Type ----------------------------Weight -------------------------

Performance:


Upper ----------------------------- +160°F (+71°C)Lower ----------------------------- -65°F (-54°C)

Packaging:

Inner Container:Reference --------------------- MIL-C-10464Type ---------------------------- Type I

Hermetically seal-ed metal container

Dimensions ------------------- 2.062 x 2.2 in. diaItems per package ---------- 4Weight ------------------------- 0.167 lb (0.076 kg)

Outer Container:

Reference --------------------- PPP-B-621Type ---------------------------- Wood boxDimensions ------------------- 9.75 x 5.688 x

3.313 in (24,765 x14.46 x 8.415 cm)

Weight ------------------------- 3 lb (31.361 kg)Cube ---------------------------- 0.1 cu ft



group --------------------------- CDOT shipping class ----------- CDOT designation -------------- SMALL ARMS

AMMUNITION,CLASS CEXPLOSIVE,HANDLECAREFULLY,KEEP FIRE AWAY

References:

TM 9-1377-200-20&PTM 55-1510-204-23TM 55-1510-213-23TB 9-1300-385, App B

6-18

TM 43-0001-39

CARTRIDGE, IMPULSE, GUILLOTINE: (M520)



Use:

Used in the guillotine firing unit on someMartin-Baker Mark 5 series and some Mark 6series ejection seats to furnish gas pressure foractuation of the parachute withdrawal line guil-lotine.

Description:

Components of the guillotine cartridgeare: metal case, guillotine cartridge cap anddisc, a paper disc, and percussion cap primer.

The primer is encased in tin foil andrequires no anvil. An anvil is machined intothe primer cavity of the case. The primer isforce-fitted into the cartridge case to ensure con-tact between the tin foil and the anvil point.The percussion cap is sealed in the head of thecase with dark purple lacquer.

6-19

TM 43-0001-39

Functioning:

When the manual override lever of the ejec-tion seat is operated, the sear is withdrawnfrom the guillotine firing unit and the firing pinmoves under strong spring pressure to strikethe percussion cap of the cartridge. The gas gen-erated from the fired cartridge is fed via a stain-less steel pipe and flexible hose to theguillotine. When actuated, the guillotine seversthe nylon parachute withdrawal line.

Tabulated Data:

NSN ----------------------------- 1377-00-883-8998DODIC --------------------------- M520Drawing number -------------- 2519698Vendor (CAGE Code and

part number ----------------- (U1604) 16650-1Item weight --------------------- 0.135 lb (0.062 kg)Diameter ------------------------ 0.800 in. (2.03 cm)Length --------------------------- 1.600 in. (4.1 cm)Method of actuation --------- Percussion primerBody material ------------------ AluminumPropellant/explosive material:

Type ---------------------------- Nitrocellulose, gunpowder

Weight ------------------------- 0.00352 lb (24.64grains)

Performance:

1410 ft-lb Explosive Power Rating


Upper ----------------------------- +160°F (+71°C)Lower ----------------------------- -65°F (-54°C)

Packaging:




MIL-C-10464Type IHermetically seal-ed metal container2.63 x 2.63 x 3 in.20.30 lb

PPP-B-1672Fiberboard box1.54 x 1.04 x 0.35 ft3 lb (1.361 kg)0.11 cu ft



group --------------------------- CDOT shipping class ----------- CDOT designation -------------- Small Arms

Ammunition,Handle Carefully,Keep Fire Away

References:

TM 9-1377-200-20&PTM 55-1510-204-23TM 55-1510-213-23TB 9-1300-385, App B

6-20

TM 43-0001-39




Use:

Used in the CH-54B helicopter to sever a7/8-inch (2.22 cm) diameter stainless steel hoistcable.

Description:

The M657 is used in the cable cutter NSN:1377-00-178-8416. Two cutters are used in theCH-54B helicopter. The cartridge consists of anignition element, body, and output charge. Theignition element has an initiator body four-pinelectrical connector, two bridgewires and asleeve with a closure disc. The cartridge bodyhouses the ignition element and output charge.A closure disc hermetically seals the outputcharge within the cavity of the cartridge body.

Functioning:

Firing of the electrically initiated car-tridge produces gas pressure to overcome thesheer pin. The cutter blade is driven onto theanvil cutting the cable that passes through thecutter body.

Tabulated Data:

NSN ----------------------------- 1377-00-168-5802DODIC --------------------------- M657Drawing number --------------Vendor (CAGE Code) and

part number ----------------- (22567) 300051-1Item weight ---------------------Diameter ------------------------ 2 in. (5.08 cm)Length --------------------------- 1.65 in. (4.17 cm)Method of actuation --------- ElectricalBody material ------------------ Steel

6-21

TM 43-0001-39

Propellant/explosive material:Type ---------------------------- High Temperature

Smokeless PowderWeight ------------------------- 0.0038 lb

Performance:

Temperature Limits:

Upper ----------------------------- +165°F (+74°C)Lower ----------------------------- -65°F (-54°C)

Packaging:

Inner Container:Reference --------------------- MIL-C-10464Type ---------------------------- Type I hermetically

sealed metal con-tainer

Dimensions ------------------- 8 x 6 in.Items per package ---------- 1Weight ------------------------- 1 lb

Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiberboard boxDimensions -------------------Weight ------------------------- 2.50 lbCube ---------------------------- 0.560 cu ft



group --------------------------- SDOT shipping class ----------- CDOT designation -------------- CLASS C

EXPLOSIVE,HANDLECAREFULLY,KEEP FIRE AWAY

References:

TB 9-1300-385, App B.

6-22

TM 43-0001-39

CARTRIDGE, IMPULSE, CCU-92/A: (MJ21)



Use:

CCU-92/A is used as the power source forthe TCU-3/A Thruster.

Description:

The impulse cartridge CCU-92/A is electri-cally initiated and consists of cylindrical alumi-num body loaded phenolic spacer, main charge,aluminum closure disc. Four insulated contactpins complete the internal electrical circuitthrough two separate bridgewires.

Functioning:

Upon receipt of firing current the bridge-wires are fired which in turn fires the main

charge that supplies the gas pressure for theTCU-3/A Thruster.

Tabulated Data:



1377-01-211-7211MJ211512AS121

(01276) FE7590-95

0.572 in. (1.45 cm)0.88 in. (2.24 cm)ElectricalAluminum

Propellant/explosive material:Type ----------------------------Weight -------------------------

Black powder0.00052 lb (3.64grains)

6-23

TM 43-0001-39

Performance:

Temperature Limits:

Upper ----------------------------- +200°F (+93.4°C)Lower ----------------------------- -65°F (-54°C)

Packaging:

Inner Container:Reference --------------------- MIL-C-10464Type ---------------------------- Type I heretically


Dimensions -------------------Items per package ---------- 1Weight -------------------------

Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiberboard boxDimensions -------------------



group --------------------------- CDOT shipping class ----------- CDOT designation -------------- Class C Explosive,

Handle Carefully,Keep Fire Away

References:

TB 9-1300-385, App B.

6-24

TM 43-0001-39

CARTRIDGE, IMPULSE, M796: (MD73)


ATC-S LCC-A.Refer to Aircraft Subsystem.

Use:

Power source for the M1 chaff cartridge ofthe M206 flare cartridge on a one to one matchwhich is used in the M130 dispenser pod on vari-ous aircraft.

Description:

The M796 cartridge consists of an alumi-num case, header assembly, igniter charge,booster charge, output charge, closure disc andclosure washer.

Functioning:

The impulse cartridge is fired electrically.The resulting hot ballistic gases developed bythe impulse cartridge ignite the flare pellet caus-ing the piston to expel the flare pellet from thecase.

Tabulated Data:

NSN - - - - - - - - - - - - - - - - - - - - - - - - --DODIC ---------------------------Drawing number --------------Vendor (CAGE Code) and


1377-01-049-6365MD739311660

(14083) 93116600.278 lb (0.126 kg)0.625 in. (1.59 cm)0.50 in. (1.40 cm)ElectricalAluminum

Propellant/explosive material:Type ---------------------------- HPC 1, M1911Weight ------------------------- 0.0088 lb (61.6

grains)

Performance:


Upper ----------------------------- +160°F (+71°C)Lower ----------------------------- -65°F (-54°C)

6-25

TM 43-0001-39

Packaging:

Inner Container:Reference --------------------- MIL-C-10464Type ---------------------------- Type I,

Hermeticallysealed metal con-tainer

Dimensions -------------------Items per package ---------- 60Weight ------------------------- 1.67 lb (0.758 kg)

Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiberboard boxDimensions -------------------Weight ------------------------- 60 lb (27.22 kg)


Quantity distance class ----- 1.4

Storage compatibilitygroup --------------------------- S

DOT shipping class ----------- CDOT designation -------------- ELECTRICAL

SQUIB, CLASS CEXPLOSIVE,HANDLECAREFULLY,KEEP FIRE AWAY

References:

TM 9-1377-200-20&PTM 9-1095-206-13&PTB 9-1300-385, App B.

6-26

TM 43-0001-39

CARTRIDGE, IMPULSE, CCU-44/B: (MD66)

CASE



Use:

Utilized as a power source for the ejectionof stores from aircraft/helicopter missile launch-ers and bomb racks. This cartridge is a suitablesubstitute for the ARD-863-1, M189.

Description:

The CCU-44/B cartridge is an electricallyinitiated cartridge installed in the firing cham-

ber of the ejection mechanism of a missilelauncher or bomb rack. The cartridge consistsof a case, electrode, ignition element, maincharge, and cap closure assembly.

Functioning:

Upon receipt of firing current the ignitionelement is fired and the resulting gas pressureignites the main charge. When sufficient pres-sure is developed, the cup closure assembly rup-tures and the released gas pressure actuatesthe release/ejector mechanism.

6-27

TM 43-0001-39

Tabulated Data:

NSN -----------------------------

DODIC ---------------------------Drawing Number -------------Vendor (CAGE Code) and

part number -----------------Item weight ---------------------Diameter ------------------------

Length ---------------------------


Body material ------------------

1377-01-063-31611377-01-063-31641377-01-063-3165MD66(53711)

51848500.086 lb (0.04 kg)1.555 in.(2.934 cm)1.155 in.(2.934 cm)Electrical 10amperesAluminum alloy

Propellant/explosive material:Type ---------------------------- Double Base Nitro

CelluloseWeight ------------------------- 0.01014 lb (70.98

grains)

Performance:


Upper ----------------------------- +225°F (+107°C)Lower ----------------------------- -65°F (-54°C)

Packaging:



Dimensions -------------------


Outer Container:Reference ---------------------Type ----------------------------Dimensions -------------------Weight -------------------------Cube ---------------------------

4.13 x 6.19 in. dia(10.49 x 15.723 cmdia)NSN 1377-01-063-3161 = 60NSN 1377-01-063-3164 = 80NSN 1377-01-063-3165 = 10

PP-B-1672Class II STYLE D2 x 1.33 x 0.35 ft10 lb0.78 cu ft



group --------------------------- CDOT shipping class ----------- CDOT designation -------------- SMALL ARMS

AMMUNITION,CLASS CEXPLOSIVE,HANDLECAREFULLY,KEEP FIRE AWAY

References:

TM 9-1377-200-20&PTB 9-1300-385, App B

6-28

TM 43-0001-39

CHAPTER 7

INITIATORS/DETONATORS(ARMING/FIRING MECHANISMS)

7-1. General

Initiators are explosive devices that use bal- waves to start a chain of events or functionslistic gas pressure or high order detonation within a system.

7-1 (7-2 blank)

TM 43-0001-39

ARMING/FIRING MECHANISM: P/N 813633-4



Use:

A detonator-type mechanism used in theAH-1 series helicopter to actuate the canopyremoval system.

NOTE

Arming/Firing Mechanism PN 813633-4to be replaced by 3W84, 1377-01-234-0667.

Description:

The armed/firing mechanism is a manu-ally operated percussion-type detonator assem-bly consisting of a body, handle assembly, firingpin, compression spring, a demolition trans-fer/charge assembly quick release pin, seals,fittings, and attaching hardware.

There are three armed/firing mechanismsin the system, one each at the pilot’s and gun-ner’s stations and one in the fuselage nose forexternal access by rescue personnel.

Functioning:

To actuate the system, the handle of thearmed/firing mechanism is rotated 90 degreescounterclockwise to arm and pulled to fire aprimer charge initiating a detonation wavewhich is transmitted through the system to deto-nate all four window cutting assemblies.

Tabulated Data:

NSN ----------------------------- 1377-00-410-8265DODIC ---------------------------Drawing number -------------- 813633-4Vendor (CAGE Code) and

part number ----------------- (97499) 209-030-711-37(06331) 813633-4

Item weight --------------------- 2.5 lb (1.134 kg)Width ----------------------------- 17 in. (17.8 cm)Height ---------------------------- 5 in. (12.7 cm)Length --------------------------- 12 in. (30.5 cm)Method of actuation --------- Manually operatedBody material ------------------ Aluminum alloyPropellant/explosive material:

Type ---------------------------- HNS, Type I, gradeB

Weight ------------------------- 0.000190 lb (1.33grains)

Body material --------------- Steel

7-3

TM 43-0001-39

Performance:


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C

Packaging:



Dimensions ------------------- 6 x 11.5 in.Items per package ---------- 1Weight ------------------------- 1lb

Outer Container:Reference --------------------- PPP-B-621Type ---------------------------- Wood boxDimensions ------------------- 1.6 x 1.1 ft

Weight ------------------------- 2.5 lbCube ---------------------------- 0.562 cu ft





References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TM 55-1520-236-23TM 55-1520-239-23TB 9-1300-385, App B

7-4

TM 43-0001-39

ARMING/FIRING MECHANISM: P/N 814033-101



Use:

A detonator-type mechanism used in theAH-1 series helicopter to actuate the canopyremoval system.

NOTE

Arming/Firing Mechanism PN 814033-101 to be replaced by 3W84, 1377-01-234-0667.

Description:

The armed/firing mechanism is a manu-ally operated percussion-type detonator assem-bly consisting of a body, handle assembly firingpin, compression spring, a demolition trans-fer/charge assembly quick release pin, seals,fittings, and attaching hardware.

There are three armed/firing mechanismsin the system, one each at the pilot’s and gun-ner’s stations and one in the fuselage nose forexternal access by rescue personnel.

Functioning:

To actuate the system, the handle of thearmed/firing mechanism is rotated 90 degreescounterclockwise to arm and pulled to fire aprimer charge initiating a detonation wavewhich is transmitted through the system to deto-nate all four window cutting assemblies.

Tabulated Data:

NSN ----------------------------- 1377-01-033-5088DODIC --------------------------- N/ADrawing number -------------- 814033-101Vendor (CAGE Code) and

part number ----------------- 116-416-1209-033-008-101

Item weight ---------------------Diameter ------------------------ 2.7 in. (6.86 cm)Length --------------------------- 7.9 in. (20.07 cm)Method of actuation --------- ManualBody material ------------------ SteelPropellant/explosive material:

Type ---------------------------- HNSWeight ------------------------- 0.000190 lb (1.33

grains)

7-5

TM 43-0001-39

Performance:


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65°F (-54°C)

Packaging:



Items per package ---------- 1Weight ------------------------- 1 lb

Outer Container:Reference --------------------- PPP-621Type ---------------------------- Wood boxDimensions ------------------- 1.6 x 1.1 x 0.4 ftWeight ------------------------- 2.5 lbCube ---------------------------- 0.562 cu ft





References:

TM 9-1377-200-20&PTM 55-1520-221-23TM 55-1520-234-23TM 55-1520-236-23TM 55-1520-239-23TB 9-1300-385, App B

7-6

TM 43-0001-39

CHAPTER 8

ROCKET MOTORS/CATAPULTS

8-1. General seat and its occupant from the aircraft in anemergency situation.

a. Rocket Motors and Rocket Catapultsare explosive devices used in various aircraft b. This chapter contains technical data,egress systems to assist or propel the ejection use, and description of rocket motors/rocket cat-

apults.

8-1 (8-2 blank)

TM 43-0001-39

ROCKET MOTOR: (M447)



Use:

To provide stabilization and improved tra-jectories of the seat escape system.

Description:

The M119 tip-off compensation rocketmotor is designed for use in the Grumman OV-1 Mohawk airplane on the MD-S5 seat system.The unit provides sufficient energy to stabilizethe ejection seat in the correct attitude toinsure drogue chute deployment in the opti-mum direction.

The M119 rocket motor is trunnionmounted under the seat. The nozzle is orientedin a down position. A steel wire lanyard isthreaded into the firing mechanism andattached to the cable dispenser which isattached to the aircraft bulkhead.

After the lanyard is connected, the safetypin is removed from the firing mechanism.Once the escape system is actuated, the lanyardautomatically triggers the firing mechanismand initiates the igniter assembly which, inturn, ignites the propellant grain which pro-vides the additional propulsion to the seat.

Performance:

Rocket Motor Performance

Parameter-65 to -70°F

Min Max+65 to +75°F +160 to +165°F

Min Max Min Max

Peak Thrust (lb) 1200 1800 1500 2300 1700 2700

Total Impulse (lb-sec) 370 430 370 430 370 430

Action Time (sec) 0.280 0.420 0.230 0.350 0.180 0.320

Burning Time (sec) 0.220 0.310 0.180 0.270 0.140 0.250

Ignition Delay Time (sec) 0.000 0.015 0.000 0.015 0.000 0.015

8-3

TM 43-0001-39


Upper ----------------------------- +160°F (+71°C)Lower ----------------------------- -65°F (-54°C)

Tabulated Data:

NSN ----------------------------- 1377-00-244-1578DODIC --------------------------- M447Drawing number -------------- 11740301Vendor (CAGE Code)

and part number ----------- (51998) 1044-2Item weight --------------------- 6.36 lb (2.9 kg)Diameter ------------------------ 4.202 in. (10.67

cm)Length --------------------------- 13.3 in. (33.78 cm)Method of actuation --------- MechanicalBody material ------------------ 4130 steel and alu-

minum alloyPropellant/explosive material:

Type ---------------------------- High-density car-boxy terminatedpolybutadiene,N-53 (U) MIL-P-82676

Weight ---------------------------- 2.56 lb (17920grains)

Packaging:

Inner Container:Reference --------------------- PPP-B-636

Type ---------------------------- FiberboardDimensions ------------------- (34.1 x 13.2 x 8.1

cm)Items per package ---------- 1 eaWeight ------------------------- 8 lb

Outer container:Reference --------------------- PPP-B-621Type ---------------------------- Wood boxDimensions ------------------- 17 x 12-1/16 x 4-

11/16 in. ((43.2 x30.6 x 12 cm)

Weight ------------------------- 13 lbCube ---------------------------- 1.639 cu ft



group --------------------------- F DOT shipping class ----------- BDOT designation -------------- CLASS B


References:

TM 9-1377-200-20&PTM 55-1510-204-23TM 55-1510-213-23TB 9-1300-385, App B

8-4

TM 43-0001-39

CHAPTER 9

THRUSTERS

9-1. Generalb. The basic parts of a thruster consist

a. A thruster is a component part of an of a firing mechanism, cartridge, chamber andaircraft escape system or aerial delivery system, piston. The main purpose of a thruster is towhich is used to accomplish a certain task prior impart a thrust to a known load or oppose ato implementing the final phases of escape, for force through a given travel (stroke).crewmen from a disable aircraft, or separationof the components of an aerial delivery system.

9-1 (9-2 blank)

TM 43-0001-39

THRUSTER, CARTRIDGE ACTUATED, TCU-1/B: (MF24)


Type III A Release by Navy.

STD LCCA

Use:

Used on the high speed aerial delivery sys-tem and receives its ballistic power from theCCU-57/B Delay Cartridge.

Note

TCU-1/B replaces XM5 thruster.

Description:

The TCU-1/B thruster consists of a car-tridge (CCU-57/B), firing mechanism, body pis-ton assembly, front and rear brackets andsafety pin.

Functioning:

When the CTU-2/A container is releasedfrom the aircraft, an attached lanyard from the

aircraft initiates the CCU-57/B cartridge. Afterthe 0.4 second time delay, the TCU-1/B thrusterreleases a tail cone which houses a recovery par-achute. The aerodynamic load on the tail conethus serves to deploy the parachute.

Tabulated Data:

NSN ----------------------------- 1377-01-075-6433DODIC --------------------------- MF24Drawing number -------------- 5184910Vendor (CAGE Code) and

part number ----------------- 5184910Item weight --------------------- 1.36 lb (0.62 kg)Diameter ------------------------Length --------------------------- 9.0 in. (22.86 cm)Method of actuation --------- ManualBody material ------------------ SteelPropellant/explosive material:

Type ----------------------------

Weight -------------------------

Black powder andHES 58080.0025 lb (17.5grains)

9-3

TM 43-0001-39

Performance:

Delay time ---------------------- 0.4 sec +0.1Minimum stroke1.5 in. (3.81 cm)


Upper ----------------------------- +200°F (+93°C)Lower ----------------------------- -65F0 (-54°C)

Packaging:

Inner Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiberboard boxDimensions ------------------- 10-3/16 x 2-1/2 x 2-

1/2 in. (25.9 x 6.4 x6.4 cm)

Items per package ---------- 1Weight ------------------------- 1.6 lb (0.73 kg)

Outer Container:Reference --------------------- PPP-B-621Type ---------------------------- Wood Box

Dimensions ------------------- 19 x 12-3/16 x 11-7/8 in. (48.3 x 30.46x 30.16 cm)

Weight -------------------------Cube ---------------------------- 1.6 cu ft



group --------------------------- SDOT shipping class ----------- CDOT designation -------------- EXPLOSIVE

POWER DEVICE,CLASS CEXPLOSIVE,HANDLECAREFULLY,KEEP FIRE AWAY

References:

FM 10-547TM 9-1377-200-20&PTB 9-1300-385, App B

9-4

TM 43-0001-39

THRUSTER, CARTRIDGE ACTUATED, TCU-3/A: (MJ20)



Use:

UH-60 cargo hook release mechanism,Provides a power source to release the loadapplied to the 6,000 lb cargo hoist hook in theevent of an emergency.

Description:

The cartridge assembly for the cargo hookconsists of an aluminum body, a pressure car-tridge, piston, plug, washer, piston retainingring and O-rings.

Functioning:

The cargo hook cartridge assembly is firedelectrically by placing a switch in the crew com-partment to the release position. Ballistic gaspressure from the cartridge forces the pistonout of the body assembly thus mechanically oper-ating the release mechanism on the cargo hook.

Tabulated Data:

NSN ----------------------------- 1377-01-211-7212DODIC --------------------------- MJ20Drawing number -------------- 1512AS120

9-5

TM 43-0001-39

Vendor (CAGE Code) andpart number ----------------- (01270) FE 7590-

98Item weight --------------------- 0.21 lbDiameter ------------------------ 0.735 in. (1.867

cm)Length --------------------------- 253 in. (6.426 cm)Method of actuation --------- ElectricalBody material ------------------ AluminumPropellant/explosive material:

Type ---------------------------- SPWeight ------------------------- 0.00052 lb (3.64

grains)

Performance:


Upper -----------------------------Lower -----------------------------

Packaging:


+200°F (+93.4°C)-65°C (-54°C)

MIL-C-10464Hermeticallysealed metal con-tainer

Dimensions -------------------Item per package ----------- 1Weight -------------------------

Outer Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiberboard boxDimensions -------------------Weight -------------------------Cube ----------------------------




References:

TM 9-1377-200-20&PTM 55-1520-237-23TB 9-1300-385, App B

1.4

SCEXPLOSIVEPOWER DEVICE,CLASS CEXPLOSIVE,HANDLECAREFULLY,KEEP FIRE AWAY

9-6

TM 43-0001-39

THRUSTER, EXPLOSIVE ACTUATED: P/N 209-033-007-3



Use:

Used on the AH-E/F/P Helicopter.

Description:

The thruster is a steel manifold that trans-mits an explosive force from shielded mild deto-nating cord (SMDC) to a thruster piston.(Detonating cord provided at installation.)

Functioning:

Upon detonation of the SMDC the explo-sive force is applied to the piston driving it for-ward.

Tabulated Data:

NSN -----------------------------DODIC ---------------------------Drawing number --------------Vendor (CAGE Code) and

part number -----------------

Item weight ---------------------Diameter ------------------------Length ---------------------------Method of actuation ---------

1377-01-062-4196

820810

(97499) 209-033-007-30.37 lb0.88 in.4.78 in.ExplosivelyInitiated

Propellant/explosive material: None/InertType ---------------------------- N/AWeight ------------------------- N/A

9-7

TM 43-0001-39

Performance:


Upper ----------------------------- +200°F (+93.4°C)Lower ----------------------------- -65°C (-54°C)

Packaging:

Reference ------------------------ MIL-B-117Type ----------------------------- Heat sealedDimensions --------------------- 9 x 6 in.Weight ---------------------------- 0.6 lbCube ----------------------------- 0.30 cu ft


Quantity distance class -----

Storage compatibilitygroup ---------------------------

DOT shipping class -----------DOT designation --------------

References:

TB 9-1300-385, App B

9-8

TM 43-0001-39

CHAPTER 10

MISCELLANEOUS ITEMS

10-1. General and Propellant Actuated Devices (PADs)described in the other chapters of this manual.

a. The items listed in this chapter havecharacteristics which set them apart from the b. Some of the items described in thisCartridges, Cartridge Actuated Devices (CADs) chapter are part of a kit or component and will

refer to the data sheet on such items.

10-1 (10-2 blank)

TM 43-0001-39

REFIRE KIT: 073-3831



Use:

The refire kit is used to rebuild the cablecutter on UH-1 and UH-60.

Description:

The refire kit consists of a cartridge assem-bly, shear pin, anvil, cutter, and two O-rings.

Functioning:

The Refire Kit is used to reload the UH-1and UH-60 Cable Cutter.

Tabulated Data:

NSN ----------------------------- 1377-01-073-3831DODIC ---------------------------Drawing number --------------

Vendor (CAGE Code) andpart number -----------------

Item weight ---------------------Diameter ------------------------Length ---------------------------Method of actuation ---------Body material ------------------

(22567) K303104-1(82402) 42277E182

4.0 in. (10.16 cm)6.0 in. (15.24 cm)ElectricalAluminum

Propellant/explosive material:Type ---------------------------- Dupont bullseye

black powderWeight ------------------------- 0.000243 lb (1,7

grains)

Performance:


Upper ----------------------------- + 165°F (+74° C)Lower ----------------------------- -65°F (-54°C)

10-3

TM 43-0001-39

Packaging:

Inner Container:Reference --------------------- PPP-B-636Type ---------------------------- Fiberboard boxDimensions -------------------Items per packageWeight ------------------------- 0.3 lb

Outer Container:Reference --------------------- PPP-B-621Type ---------------------------- Wood boxDimensions ------------------- 1.6 x 1.1 x 0.4 ftWeight ------------------------- 2.5 lbCube ---------------------------- 0.560 cu ft



group --------------------------- SDOT shipping class ----------- CDOT designation -------------- EXPLOSIVE

POWER DEVICE,HANDLECAREFULLY,KEEP FIRE AWAY

References:

TB 9-1300-385, App B.

10-4

TM 43-0001-39

PIN PULLER, EXPLOSIVE ACTUATED P/N 816984



Use:

The pin puller is used in the AH-1 canopyremoval system(s).

Description

The Pin Puller is a steel manifold thattransmits an Explosive Force from shieldedmild detonating cord (SMDC) to a puller posi-tion.

Functioning:

Upon detonation of the SMDC, the explo-sive force is applied to the piston. Movement ofthe piston pulls the pin that retains the canopy.

Tabulated Data:

NSN ----------------------------- 1377-01-037-4091DODIC ---------------------------Drawing number -------------- 816984Vendor (CAGE Code) and

part number ----------------- (06331) 816984Item weight ---------------------Diameter ------------------------ 1.5 in. (3.81 cm)Length --------------------------- 2.25 in. (5.72 cm)Method of actuation --------- Explosively actu-

atedBody Material ------------------ SteelPropellant/explosive

material ----------------------- Not loaded - inert.

Performance:


Upper ----------------------------- +200°F (+93.4°C)Lower ----------------------------- -65°F (-54°C)

10-5

TM 43-0001-39

PIN PULLER, EXPLOSIVE ACTUATED: P/N 816984

Packaging:Shipping and Storage Data:

Inner Container:Reference --------------------- MIL-B-117Type ---------------------------- Type I, class BDimensions ------------------- 4 x 6 in.Items per package ---------- 1Weight ------------------------- 0.5 lb

Outer Container:Reference --------------------- SPI (AMOP-01-

037-4091)Type ----------------------------Dimensions ------------------- 0.6 x 0.5x 0.2 ftWeight ------------------------- 0.5 lbCube ---------------------------- 0.046 cu ft

Quantity distance class ----- N/AStorage compatibility

group --------------------------- N/ADOT shipping class ----------- N/ADOT designation -------------- N/A

References:

TM 9-1377-200-20&PTM 55-1520-236-23TB 9-1300-385, App B.

10-6

TM 43-0001-39

CARTRIDGE ASSEMBLY, CARGO HOOK: PY58



Use:

UH-60 cargo hook release mechanism.Provides a power source to release the loadapplied to the 8,000 lb cargo hoist hook in theevent of an emergency.

NOTE

To be replaced by CCU-921A ImpulseCartridge MJ21 1377-01-211-7212

Description:

The cartridge assembly for the cargo hookconsists of an aluminum body, a pressure car-tridge, piston, plug, washer piston retainingring and O-rings.

Functioning:

The cargo hook cartridge assembly is firedelectrically by actuating a switch in the crew

compartment to the release position. Ballisticgas pressure from the cartridge forces the pis-ton out of the body assembly thus mechanicallyoperating the release mechanism on the cargohook.

Tabulated Data:

NSN ----------------------------- 1377-01-149-5917DODIC --------------------------- PY58Drawing number -------------- FE7590-65Vendor (CAGE Code) and

part number ----------------- (01276) FE7590-65Item weight ---------------------Diameter ------------------------ 0.75 in. (1.91 cm)Length --------------------------- 2.36 in. (5.99 cm)Method of actuation --------- ElectricalBody material ------------------ AluminumPropellant/explosive material:

Type ----------------------------Weight -------------------------

10-7

TM 43-0001-39

Performance:


Upper ----------------------------- N/ALower ----------------------------- N/A

Packaging:





group -------------------------- CDOT shipping class ----------- CDOT designation -------------- Explosive Power

Device, Class CExplosive, HandleCarefully KeepFire Away.

References:

TM 9-1377-200-20&PTM 55-1520-237-23TB 9-1300-385, App B

10-8

TM 43-0001-39

APPENDIX A

REFERENCE PUBLICATIONS

A-1. Army Regulations

Army Safety Program . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AR 385.10System Safety Engineering and Management . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AR 385-16Accident Reporting and Records . . . . . . . . . . . . . . . . ,. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AR 385-40Ammunition and Explosive Safety Standards .... .. . . . . . .. . . . . . . . . . . . . . . . . . . AR 385-64Identification of Inert Ammunition and Ammunition Components . . . . . . . . . AR 385-65Reporting of Transportation Discrepancies in Shipments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AR 55-38Worldwide Ammunition Reporting System (WARS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AR 700-22Ammunition Stockpile Reliability Program . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AR 702-6Type Classification/Reclassification of Army Material . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AR 71-6Report of Item and Packaging Discrepancies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AR 735-11-2Malfunctions Involving Ammunition and Explosives . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AR 75-1Hazardous Item Contracts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . ... DARCOM-R 385-17Determination and Assignment of Ammunition and Explosives

Hazard (classifications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DARCOM-R 385-21Safety Manual .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DARCOM 385Safety Manual . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DARCOM 385-100

A-2. Technical Manuals

The Army Maintenance Management System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Operator’s Aviation Unit Maintenance and Aviation Intermediate

Maintenance Manual Repair Parts and Special Tools List(Incl RPSTL) Dispenser, General Purpose Aircraft: M130 . . . . . . . . . . . . . . . . . . . . .

Ammunition, General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Ammunition and Explosive Standards ., . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Ammunition Maintenance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..Organizational and Maintenance Manual (Incl RPSTL) Cartridges,

Cartridge Actuated Devices and Propellant Actuated Devices.Aviation Unit and Intermediate Maintenance Manual:

Army Models OV-1B/OV-1C Aircraft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Aviation Unit and Intermediate Maintenance Manual:

Army Models OV-1D/RV-1D Aircraft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Aviation Unit and Aviation Intermediate Maintenance Manual:

Army Model CH-47A Helicopter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Aviation Unit and Intermediate Maintenance Instructions:

Army Model UH-1D/H/V/EH-1H Helicopters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Aviation Unit and Intermediate Maintenance Instructions:

CH-54A Helicopter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . .Aviation Unit and Intermediate Maintenance Instructions:

Army Model UH-1C/M Helicopters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

DA PAM 738-750

TM 9-1095-206-13&PTM 9-1300-200TM 9-1300-206TM 9-1300-250

TM 9-1377-200-20&P

TM 55-1510-204-23

TM 55-1510-213-23

TM 55-1520-209-23

TM 55-1520-210-23

TM 55-1520-217-23

TM 55-1520-220-23

A-1

TM 43-0001-39

]Aviation Unit and Aviation Intermediate Maintenance Manual:Army Model AH-1G and AH-1Q Helicopters .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TM 55-1520-221-23

Aviation Unit and Aviation Intermediate Maintenance Manual:Army Model CH-47B and CH-47C Helicopters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TM 55-1520-227-23

Avum and Avim Maintenance Manual: AH-1S (MOD) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TM 55-1520-234-23Aviation Unit and Intermediate Maintenance Manual:

Army Model AH-IS (PROD), AH-IS (ECAS) and AH-1S(Modernized COBRA) Helicopters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TM 55-1520-236-23

Aviation Unit and Intermediate Maintenance Wiring DataManual for UH-60A Helicopter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TM 55-1520-237-23

Aviation Unit and Intermediate Maintenance Repair Parts andSpecial Tools List (Incl Depot Maintenance RPSTL) forHelicopter, Attack, AH-1S (Modernized COBRA) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TM 55-1520-239-23

Aviation Unit and Aviation Intermediate Maintenance Manual:CH-47D Helicopter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TM 55-1520-240-23

A-3. Technical Bulletins

Department of Defense Explosive Hazard Classification Procedures. . . . . . . . . . . . TB 700-2Munitions Suspended or Restricted . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TB 9-1300-385-1Munition Permanently Suspended or Restricted . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TB 9-1300-385-2

A-4. Supply Catalogs

DOD Consolidated Ammunition Catalog. . . . . . . . . . . . . . . . . . . . . . SB 708-4

A-5. Blank Forms

Recommended Changes to Publications and Blank Forms . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DA Form 2028Ammunition Condition Report . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DA Form 2415Accident Report . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DA form 285Discrepancy in Shipment Report . . . . . . . . . . . . . . . .. . . . . . . . .. SF 361Packaging and Improvement Report . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SF 364

A-6. Navy Publications

Ordnance Safety Precautions, Their Origin and Necessity. . . . . . . . . . . . . . . . . . . . . .OP 1014Index to Navy Ammunition Stocks, Cartridges and Cartridge

Actuated Devices. . . . . . . . . . . . . . . . . . . . . . . . . . . .TW010-AA-ORD-010Navy Transportation Safety Handbook. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OP 2165United States Navy Ordnance Safety Precautions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OP 3347Ammunition Afloat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OP 4Ammunition and Explosives Ashore . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OP 5

A-2

TM 43-0001-39

APPENDIX B

CAD/PAD AIRCRAFT/HELICOPTER/EQUIPMENTCROSS REFERENCE

CAD/PAD

Arm-Fire InitiatorCartridge, Aricraft Fire ExtinguisherCartridge, Aircraft Fire ExtinguisherCartridge, Aircraft Fire ExtinguisherCartridge, Aircraft Fire Extinguisher

Cartridge, Aircraft Fire Extinguisher

Cartridge, Aircraft Fire ExtinguisherCartridge, Assembly Cargo HookCartridge, Assembly Cargo HookCartridge, DelayCartridge, Delay

Cartridge, DelayCartridge, ImpulseCartridge, ImpulseCartridge, Impulse

Cartridge, ImpulseCartridge, ImpulseCartridge, ImpulseCartridge, ImpulseCartridge, ImpulseCartridge, ImpulseCartridge, ImpulseCartridge, ImpulseCartridge, ImpulseCartridge, ImpulseCartridge, ImpulseCartridge, ImpulseCartridge, Set, ImpulseCartridge, ImpulseConnector, Inline (Inert)

Cord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, Detonating

NSN

1377-01-033-50881377-00-087-71031377-00-756-13841377-00-824-58581377-00-930-9390

1377-01-113-85301377-01-263-36271377-01-185-26221377-01-115-37111377-01-149-59171377-00-774-72591377-00-958-1048

1377-01-084-60641377-00-168-58021377-00-253-44361377-00-585-9291

1377-00-707-05901377-00-793-99261377-00-805-92811377-00-878-65101377-00-883-89971377-00-883-89981377-00-999-74631377-01-049-63651377-01-057-06861377-01-063-31611377-01-063-31641377-01-063-31651377-01-211-72111377-00-845-52421377-00-062-4195

1377-00-409-10981377-00-409-10991377-00-409-11001377-00-410-82661377-00-410-82711377-00-410-82891377-00-410-82971377-01-032-10471377-01-032-10481377-01-032-1049

APPLICATION

AH-E/F/P (Cobra)

CH-47 (Chinook)

OV-1 (Mohawk)CH-47 (Chinook)AH-1 (Cobra)UH-60A (Blackhawk)

UH-60A (Blackhawk)UH-60A (Blackhawk)

20 sec delayCargo ParachuteTCU-1/B ThrusterCH 54B

AH-S(MOD) E/F/P (Cobra)AH-1S/MOD EAH-1S/MOD FAH-1S/MOD P

OV-1A (Mohawk)

OV-1 (Mohawk)OV-1 (Mohawk)

UH-60A (Blackhawk)UH-60A (Blackhawk)UH-60A (Blackhawk)UH-60A (Blackhawk)TCU-3/A ThrusterOV-1 (Mohawk)AH-1E/F/P (Cobra)AH-1S/MOD EAH-1S/MOD FAH-1S/MOD PAH-1S (MOD)AH-1S (MOD)AH-1S (MOD)AH-1S (MOD)AH-1S (MOD)AH-1S (MOD)AH-1S (MOD)AH-1 E/F/P (Cobra)AH-1 E/F/P (Cobra)AH-1 E/F/P (Cobra)

B-1

TM 43-0001-39

CAD/PAD

Cord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCutter AssemblyCutter, Cartridge ActuatedCutter, Cartridge ActuatedCutter, Reef Line

Cutting AssemblyCutting AssemblyCutting AssemblyCutting AssemblyFiring MechanismInterconnecting LineJunction Manifold (Inert)Junction Manifold (Inert)Junction Manifold (Inert)Pin Puller, ExplosiveRefire KitRocket MotorThruster, Cartridge Actuated

Thruster, Cartridge ActuatedThruster, Explosive

NSN

1377-01-032-10501377-01-032-32791377-01-032-32801377-01-032-32831377-01-032-32861377-01-035-41241377-01-037-40901377-01-037-40931377-01-037-40941377-01-037-40951377-01-037-40961377-01-037-92371377-01-064-49271377-00-412-43771377-01-087-51661377-00-060-0885

1377-00-106-77731377-00-409-10951377-00-409-10961377-00-409-10971377-00-410-82651377-01-100-17181377-00-409-11011377-00-410-82281377-01-037-40921377-01-037-40911377-01-073-38311377-00-244-15781377-01-075-6433

1377-01-211-72121377-01-062-4196

APPLICATION

AH-1 E/F/P (Cobra)AH-1 E/F/P (Cobra)AH-1 E/F/P (Cobra)AH-1 E/F/P (Cobra)AH-1 E/F/P (Cobra)AH-1 E/F/P (Cobra)AH-1 E/F/P (Cobra)AH-1 E/F/P (Cobra)AH-1 E/F/P (Cobra)AH-1 E/F/P (Cobra)AH-1 E/F/P (Cobra)AH-1 E/F/P (Cobra)UH-1 (Iroquois)CH-54 (Tarhe)

High Speed AerialDeliver, CTU-2AAH-1S (MOD) (Cobra)AH-1S (MOD) (Cobra)AH-1S (MOD) E/F/P (Cobra)AH-1S (MOD) (Cobra)AH-1S (MOD) E/F/P (Cobra)AH-1S (MOD) (Cobra)AH-1S (MOD) (Cobra)AH-1S (MOD) (Cobra)AH-1 E/F/P (Cobra)AH-1 E/F/P (Cobra)UH-1 (Iroquois)OV-1 (Mohawk)High Speed AerialDelivery, CTU-2AUH-60A (Blackhawk)AH-1E/F/P (Cobra)

B-2

TM 43-0001-39

Figure B-1. Designation of Rotary Wing Army Aircraft (sheet 1 of 2).

B-3

TM 43-0001-39

Figure B-1. Designation of Rotary Wing Army Aircraft (sheet 2 0f 2).

B-4

TM 43-0001-39

Figure B-2. Designation of Fixed Wing Army Aircraft (sheet 1 of 2).

B-5

TM 43-0001-39

Figure B-2. Designation of Fixed Wing Army Aircraft (sheet 2 of 2).

B-6

Type - AircraftEquipment

AH-IS (MOD)

AH-1 E/F/P

AH-1 E/F/P

AH-64

TM 43-0001-39

APPENDIX C

AIRCRAFT/HELICOPTER/EQUIPMENT TO CAD/PADCROSS-REFERENCE

CAD/PAD

Cartridge, ImpulseCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCutting, AssemblyCutting, AssemblyCutting, AssemblyCutting, AssemblyFiring MechanismJunction Manifold (Inert) CrossJunction Manifold (Inert) Tee

Cartridge, ImpulseConnector, InlineCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingJunction, Manifold (Inert) InlinePin Puller, ExplosiveThruster, Explosive

Cord, DetonatingInitiator, Arm-Fire

Connector, ElbowConnector, UnionConnector, TeeCord, DetonatingCord, DetonatingCord, DetonatingCord, Detonating

NSN

1377-00-585-92911377-00-409-10981377-00-409-10991377-00-409-11001377-00-410-82221377-00-410-82661377-00-410-82711377-00-410-82891377-00-410-82971377-00-106-77731377-00-409-10951377-00-409-10961377-00-409-10971377-00-410-82651377-00-409-11011377-00-410-8228

1377-00-585-92911377-01-062-41951377-01-032-10471377-01-032-10481377-01-032-10491377-01-032-10501377-01-032-32791377-01-032-32801377-01-032-32831377-01-032-32861377-01-035-41241377-01-037-40901377-01-037-40931377-01-037-40941377-01-037-40951377-01-037-40961377-01-037-92371377-01-037-40921377-01-037-40911377-01-062-4196

1377-01-100-17181377-01-033-5088

1377-01-170-44931377-01-170-53211377-01-170-53191377-01-186-98991377-01-186-99001377-01-186-99011377-01-186-9902

DODIC

M189MD18MD16MS50

MS47MD15MS48MD17MD35MD34MD33MD36———

M189

MS76MS77MS78MS79MS60MS61MS59MS58MS51MS53MS57MS56MS55MS54MS52———

MS62—

——

MS90MS91MS92MS93

C-1

TM 43-0001-39

Type - AircraftEquipment

Cargo Parachute

CH-46, CH-47

CH-47

CH-54

CTU-2/A, TCU-1/B

OV-1

UH-1

UH-60

CAD/PAD

Cord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCord, DetonatingCutting AssemblyCutting AssemblyCutting AssemblyCutting AssemblyInitiator, Mechanical

Cartridge, Delay

Cartridge, Aircraft FireExtinguisher


Cartridge, Impulse

Cartridge, ImpulseCutter, Cartridge Actuated

Cartridge, DelayCutter, Reef LineThruster, Cartridge Actuated


Cartridge, ImpulseCartridge, ImpulseCartridge, ImpulseCartridge Set, ImpulseRocket MotorParts Kit, Cutter

Parts Kit, CutterRefire Kit


Cartridge, Pressure Cargo HookCartridge, Impulse ARD 863-1Cartridge, Aircraft Fire

ExtinguisherCartridge, Impulse CCU-44/B

NSN

1377-01-170-52601377-01-170-52451377-01-170-52461377-01-170-52441377-01-170-52651377-01-170-52641377-01-170-52631377-01-170-52621377-01-170-52611377-01-186-98981377-01-184-61121377-01-184-61131377-01-187-44771377-01-185-89081377-01-269-6496

1377-00-958-1048

1377-00-756-1384

1377-00-930-9390

1377-00-999-7463

1377-00-168-58021377-00-412-4377

1377-01-084-60461377-00-060-08851377-01-075-6433

1377-00-930-9390

1377-00-793-99261377-00-883-89971377-00-883-89981377-00-845-52421377-00-244-15781377-00-011-9082

1377-00-011-90821377-01-073-3831

1377-01-113-8530

1377-01-115-37111377-01-057-06861377-01-263-3627

1377-01-063-3164

DODIC

MS89MS81MS82MS80MS87MS86MS85MS84MS83MS88MS94MS95MS97MS96MT06

M308

M182

M193

M162

M657M554

MF35M500MF24

M012M507M520M397M447

M189MT20

MD66

C - 2

TM 43-0001-39

APPENDIX D

CAD/PAD INDEX BY DODIC

DODIC NOMENCLATURE PAGE

M162M182M189M193M232M253M291M308M397M447M500M507M520M554M657M721MD15MD16MD17MD18MD33MD34MD35MD36MD66MD73MF24MF35MF90MF92MH88MH92MJ20MJ21MO12

Cartridge, ImpulseCartridge, Aircraft Fire ExtinguisherCartridge, Impulse ARD 863-1Cartridge, Aircraft Fire ExtinguisherCartridge, Aircraft Fire ExtinguisherCartridge, ImpulseCartridge, ImpulseCartridge, Delay M252Cartridge Set, Impulse ReducedRocket Motor M119Cutter, Reef Line M21Cartridge, Impulse DrogueCartridge, Impulse GuillotineCutter, Cartridge ActuatedCartridge, ImpulseCartridge, DelayCord, Detonating (FCDC)Cord, Detonating (FCDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cutting Assembly (WCA)Cutting Assembly (WCA)Cutting Assembly (WCA)Cutting Assembly, (WCA)Cartridge, ImpulseCartridge, ImpulseThruster, Cartridge ActuatedCartridge, Delay CCU-57/BCartridge, ImpulseCartridge, ImpulseCartridge, DelayCartridge, Aircraft Fire ExtinguisherThruster, Cartridge ActuatedCartridge, Impulse CCU-92/ACartridge, Impulse Mk 19 Mod 0

6-52-36-72-52-76-96-114-76-138-33-36-176-193-56-21See 20 & P5-95-115-135-155-175-195-215-236-276-259-34-3See 20 & PSee 20 & P4-52-99-56-236-3

D-1

TM 43-0001-39

DODIC NOMENCLATURE PAGE

MS47 Cord, Detonating (SMDC) 5-25MS48 Cord, Detonating (SMDC) 5-27MS49 Cord, Detonating (SMDC) 5-29MS50 Cord, Detonating (SMDC) 5-31MS51 Cord, Detonating (SMDC) 5-33MS52 Cord, Detonating (SMDC) 5-35MS53 Cord, Detonating (SMDC) 5-37MS54 Cord, Detonating (SMDC) 5-39MS55 Cord, Detonating (SMDC) 5-41MS56 Cord, Detonating (SMDC) 5-43MS57 Cord, Detonating (SMDC) 5-45MS58 Cord, Detonating (SMDC) 5-47MS59 Cord, Detonating (SMDC) 5-49MS60 Cord, Detonating (SMDC) 5-51MS61 Cord, Detonating (SMDC) 5-53MS62 Cord, Detonating (SMDC) 5-55MS76 Linear Explosive Assembly (LEA) 5-57MS77 Linear Explosive Assembly (LEA) 5-59MS78 Linear Explosive Assembly Window (WCA) 5-61MS79 Linear Explosive Assembly Window (WCA) 5-63MS80 Cord, Detonating (SMDC) 5-71MS81 Cord, Detonating (SMDC) 5-73MS82 Cord, Detonating (SMDC) 5-75MS83 Cord, Detonating (SMDC) 5-77MS84 Cord, Detonating (SMDC) 5-79MS85 Cord, Detonating (SMDC) 5-81MS86 Cord, Detonating (SMDC) 5-83MS87 Cord, Detonating (SMDC) 5-85MS88 Cord, Detonating (SMDC) 5-87MS89 Cord, Detonating (FCDC) 5-89MS90 Cord, Detonating (FCDC) 5-91MS91 Cord, Detonating (FCDC) 5-93MS92 Cord, Detonating (FCDC) 5-95MS93 Cord, Detonating (FCDC) 5-97MS94 Canopy Severance Assembly Forward Panel 5-99MS95 Canopy Severance Assembly Rear Panel 5-101MS96 Canopy Severance Assembly Rear Panel 5-103MS97 Canopy Severance Assembly Forward Panel 5-105MT06 Arming/Firing Initiator 5-107MT20 Cartridge, Aircraft Fire Extinguisher 2-11MU02 Cutter, Cartridge Actuated 3-7MU03 Cutter, Assembly 3-9MU11 Cutter, Delay, Propellant Actuated MLU-58/B 3-11PY58 Cartridge Assembly Cargo Hook 10-7

D-2

TM 43-0001-39

APPENDIX E

CAD/PAD INDEX BY NSN

NSN 1377- NOMENCLATURE DODIC

00-087-532600-060-088500-087-710300-106-777300-168-580200-244-157800-253-553600-328-808000-409-109500-409-109600-409-109700-409-109800-409-109900-409-110000-409-110100-410-822200-410-822800-410-826500-410-826600-410-827100-410-828900-410-829700-412-437700-508-246400-585-929100-707-059000-756-138400-774-725900-793-992600-805-928100-824-585800-845-524200-878-651000-883-899700-883-899800-930-939000-958-104800-978-764400-999-746300-999-746501-032-104701-032-104801-032-104901-032-105001-032-327901-032-3280

Cutter Propellant Actuated Mk 20 Mod 0Cutter, Reef Line M21Cartridge Aircraft Fire ExtinguisherCutting Assembly Gunner’s Door WindowCartridge, ImpulseRocket MotorCartridge, ImpulseFiring MechanismCutting Assembly Gunner’s Canopy WindowCutting Assembly Pilot’s Canopy WindowCutting Assembly Pilot’s Door WindowCord, Detonating (SMDC)Cord, Detonating (FCDC)Cord, Detonating (SMDC)Junction, Manifold (Inert)Cord, Detonating (SMDC)Junction, Manifold (Inert)Armed/Firing MechanismCord, Detonating (SMDC)Cord, Detonating (FCDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cutter, Cartridge ActuatedCutter, Reef Line M21Cartridge, Impulse ARD-863-1Cartridge, Impulse MK 104 Mod 0Cartridge, Aircraft Fire ExtinguisherCartridge, DelayCartridge, Impulse MK 19 Mod 0Cartridge, ImpulseCartridge, Aircraft Fire ExtinguisherCartridge Set, Impulse Reduced ChargeCartridge, ImpulseCartridge, Impulse DrogueCartridge, Impulse GuillotineCartridge, Aircraft Fire ExtinguisherCartridge, DelayCutter, Cartridge ActuatedCartridge, ImpulseCartridge, ImpulseCord, Detonating (LSC)Cord, Detonating (LSC)Cord, Detonating Window Cutting AssemblyCord, Detonating Window Cutting AssemblyCord, Detonating (SMDC)Cord, Detonating (SMDC)

M648M500M232MD35M657M447MF90

MD34MD33MD36MD18MD16MS50—MS49——MS47MD15MS48MD17M554M500M189M291M182

MO12MF92M232M397M253M507M520M193M308MDO1

M162MS76MS77MS78MS79MS60MS61

E-1

TM 43-0001-39


01-032-328301-032-328601-032-508801-035-412401-037-409001-037-409101-037-409201-037-409301-037-409401-037-409501-037-409601-037-923701-049-636501-057-068601-060-853101-062-419501-062-419601-063-316101-063-316401-063-316501-064-492701-073-383101-075-643301-084-604601-087-516601-100-171801-113-853001-115-371101-141-902801-149-591701-185-262201-211-721101-170-449301-170-524401-170-524501-170-524601-170-526001-170-526101-170-526201-170-526301-170-526401-170-526501-170-531901-184-611201-184-611301-185-890801-186-989801-186-9899

Cord, Detonating (SMDC)Cord, Detonating (SMDC)Armed/Firing Mechanism P/N 814033-101Cord, Detonating (SMDC)Cord, Detonating (SMDC)Pin Puller ExplosiveJunction, Manifold (INERT)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cartridge, ImpulseCartridge, Impulse ARD 863-1Cord, Set DetonatingConnector, Inline (INERT)Thruster, Explosive P/N 209-033 -007-3Cartridge, Impulse, CCU-44/BCartridge, Impulse, CCU-44/BCartridge, Impulse, CCU-44/BCutter, Assembly; P/N FTL 3648-2Refire KitThruster, TCU-1BCartridge, Delay CCU-57/BCutter, Cartridge Actuated P/N 303104-1Cord, Detonating (SMDC)Cartridge, Aircraft Fire ExtinguisherCartridge Assembly Cargo HookCutter, Cartridge ActuatedCartridge Assembly Cargo HookCartridge Aircraft Fire ExtinguisherCartridge, Impulse CCU-92/AConnector, Elbow (Inert)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Connector, Tee (Inert)Cutting Assembly Gunner’s WindowCutting Assembly Pilot’s WindowCutting Assembly Pilot’s DoorCord, Detonating (SMDC)Cord, Detonating (FCDC)

MS59MS58

MS51MS53

—MS57MS56MS55MS54MS52MD73M189ME83

MD66MD66MD66MU03

MF24MF35MU02MS 62

MG51

MH92MJ21—MS80MS81MS82MS89MS83MS84MS85MS86MS87—MS94MS95MS96MS88MS90

E-2

TM 43-0001-39


01-186-9900 Cord, Detonating (FCDC) MS9101-186-9901 Cord, Detonating (FCDC) MS9201-186-9902 Cord, Detonating (FCDC) MS9301-187-4477 Cutting Assembly Gunner’s Door MS9701-263-3627 Cartridge, Aircraft Fire Extinguisher MT2001-269-6496 Initiator, Mechanical Actuated MT0601-288-0418 Cutter, Delay Propellant Actuated MU11

E-3 (E-4 blank)

TM 43-0001-39

APPENDIX F

CAD/PAD INDEX BY GOVERNMENT SOURCE DRAWING NUMBER

DWG NO. NOMENCLATURE PAGE

FE7590-651174030114195-118630792164465251842625185192519614251969625196982519707252000251848503904002051848585184910813633-4857AS300-1857AS300-2857AS300-3857AS300-4857AS400-1857AS400-2857AS500-1857AS500-288759788864789311660897899ARD-863-111-1-304342277E336814033-101816984820810251961451851076260906-16260906-26260906-46260906-56260906-762609646260965-2

Cartridge, Assembly Cargo Hook PY58 10-7Rocket Motor, M119, M447 8-3Cutter, Cartridge Actuated, M554 3-5Cartridge, Impulse Mk 104 Mod 9, M291 6-11Cartridge, Impulse Mk 19 Mod 0, M012Cartridge, Impulse, M162Cartridge, Aircraft Fire Extinguisher, M182Cartridge, Aircraft Fire Extinguisher, M193Cartridge Set, Impulse Reduced, M397Cartridge, Impulse Guillotine, M520

6-36-52-32-56-136-19

Cartridge; Aircraft Fire Extinguisher, M232Cartridge, Impulse Drogue, M507Cartridge, Impulse, CCU-44/B, MD66Cartridge, Aircraft Fire Extinguisher, MH92Cartridge, Delay CCU-57/B, MF35Thruster, Cartridge Actuated, TCU-1/B, MF24Arming/Firing MechanismCutting Assembly Pilot’s Door Window, MD36Cutting Assembly Gunner’s Canopy Window, MD35Cutting Assembly Gunner’s Canopy Window, MD34Cutting Assembly Pilot’s Canopy Window, MD33Cord, Detonating (SMDC), MD17Cord, Detonating (SMDC), MD18Cord, Detonating (FCDC), MD16Cord, Detonating (FCMC), MD15Cutter, Reef Line M21, M500Cartridge, Delay M252, M308Cartridge, Impulse M796, MD73Cartridge, Aircraft Fire Extinguisher, MT20Cartridge, Impulse M189Cutter, Assembly MU03Cutter, CTG Actuated MU02Arming/Firing MechanismPin Puller, Explosive Actuated (Inert)Thruster, Explosive ActuatedCTG, Aircraft Fire Extinguisher M193CTG, Delay CCU-89/B, MH88Cord, Detonating (FCDC) MS90Cord, Detonating (FCDC) MS91Cord, Detonating (FCDC) MS93Cord, Detonating (FCDC) MS89Cord, Detonating (FCDC) MS92Arming/Firing Initiator, MT06Canopy Severance Assembly, Forward Panel, MS97

2-76-176-272-94-39-37-35-235-215-195-175-135-155-115-93-34-76-252-116-73-93-77-510-59-72-54-55-915-935-975-895-955-1075-105

F-1

TM 43-0001-39

DWG NO. NOMENCLATURE PAGE

6260965-4 Canopy Severance Assembly, Rear Panel, MS96 5-1036260965-5 Canopy Severance Assembly Forward Panel, MS94 5-996260965-7 Canopy Severance Assembly Rear Panel, MS95 5-1016261062-1 Linear Explosive Assembly (LEA), MS76 5-576261062-3 Linear Explosive Assembly (LEA), MS77 5-596261062-7 Linear Explosive Assembly (LEA), Window MS79 5-636261063-9 Linear Explosive Assembly (LEA), Window MS78 5-616261071 Connector, Union 5-1096261072 Connector, Tee 5-1096261073 Connector, Elbow 5-1096261278 Cutter, Delay, Propellant Actuated MU11 3-11757AS400-17 Cord, Detonating (SMDC) MS48 5-27841AS425-23 Cord, Detonating (SMDC) MS86 5-83841AS425-35 Cord, Detonating (SMDC) MS88 5-87841AS425-45 Cord, Detonating (SMDC) MS83 5-77841AS425-47 Cord, Detonating (SMDC) MS80 5-71841AS425-49 Cord, Detonating (SMDC) MS87 5-85841AS425-51 Cord, Detonating (SMDC) MS82 5-75841AS425-53 Cord, Detonating (SMDC) MS81 5-73841AS425-55 Cord, Detonating (SMDC) MS85 5-81841AS425-57 Cord, Detonating (SMDC) MS84 5-79857AS101-1 Connector, Tee (Inert) 5-65857AS102-1 Connector, Cross Manifold (Inert) 5-65857AS103-1 Connector, In-Line (Inert) 5-65857AS400-15 Cord, Detonating (SMDC) MS47 5-25857AS400-21 Cord, Detonating (SMDC) MS49 5-29857AS400-25 Cord, Detonating (SMDC) MS50 5-31857AS400-105 Cord, Detonating (SMDC) MS51 5-33857AS400-107 Cord, Detonating (SMDC) MS52 5-35857AS400-109 Cord, Detonating (SMDC) MS53 5-37857AS400-111 Cord, Detonating (SMDC) MS54 5-39857AS400-113 Cord, Detonating (SMDC) MS55 5-41857AS400-115 Cord, Detonating (SMDC) MS56 5-43857AS400-117 Cord, Detonating (SMDC) MS57 5-45857AS400-119 Cord, Detonating (SMDC) MS58 5-47857AS400-121 Cord, Detonating (SMDC) MS61 5-53857AS400-123 Cord, Detonating (SMDC) MS60 5-51857AS400-125 Cord, Detonating (SMDC) MS59 5-49857AS400-127 Cord, Detonating (SMDC) MS62 5-551512AS105 CTG, Aircraft Fire Extinguisher, MH92 2-91512AS120 Thruster, CTG Actuated, TCU-3/A, MJ20 9-51512AS121 Cartridge, Impulse CCU-92/A, MJ21 6-231660AS200 CTG, Aircraft Fire Extinguisher, M232 2-71660AS300 CTG, Aircraft Fire Extinguisher, M182 2-3

F-2

TM 43-0001-39

APPENDIX G

CAD/PAD INDEX BY MANUFACTURER’S PART NUMBER

P/N

ARD 863-151848505184858FLT 3648-2K303104-1P7911-2R4181-1MSA 9671311-1-32914195-114398-1155468-91863079816986-3816987-103

51134-4751134-5351134-5151134-4551134-5751134-5551134-2351134-4951134-352519696303104-13090382442277E33651849107536-1813475-101813475-102813475-103813475-104813475-105813475-107813475-109813475-111

NOMENCLATURE

Cartridge, ImpulseCartridge, Impulse CCU-44/BCartridge, Delay CCU-57/BCutter AssemblyRefire KitCartridge, ImpulseCartridge, ImpulseCartridge, ImpulseCartridge, Delay M252Cutter, Cartridge ActuatedCartridge, Assembly Cargo HookCord, DetonatingCartridge, Impulse Mk 104 Mod 0Linear Explosive Assembly (LEA)Linear Explosive Assembly Window, (WCA)

Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cartridge Set ImpulseCutter, Cartridge ActuatedCartridge, Aircraft Fire ExtinguisherCutter, Cartridge ActuatedThruster, Cartridge ActuatedCartridge, Impulse DrogueCutting AssemblyCutting AssemblyCutting Assembly (WCA)Cutting Assembly (WCA)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)

DODIC

M189MD66MF35MU03

M189M253M162M308M554PY58

M291MS77MS78MS79MS80MS81MS82MS83MS84MS85MS86MS87MS88M397MU02MH92

MF24M507MD36MD35MD34MD33MS51MS52MS53MS54

PAGE

6-76-274-33-910-36-76-96-54-73-510-7

6-115-595-615-635-715-735-755-775-795-815-835-855-876-133-72-93-79-36-175-235-215-195-175-335-355-375-39

G-1

TM 43-0001-39

P/N

813475-113813475-115813475-117813475-119813475-123813475-125813475-15813475-17813475-19813475-21813475-25813475-27813592-3813592-4814033-101814280-101814280-1028142/80-103814280-104816984-107816986-1816986-393116601044-2FE7590-65FE5790-95FE7590-9816650-121602-221738-323869-251135-551135-151135-251135-751135-451188-151207-351389-151390-151391-1300051-1LDA419700

NOMENCLATURE

Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord, Detonating (SMDC)Cord Assembly, Detonating (FCDC)Cord, DetonatingArm Fire InitiatorCutting Assembly Pilot’s Door WindowCutting Assembly Gunner’s Door WindowCutting Assembly Gunner’s Canopy WindowCutting Assembly Pilot’s Canopy WindowPin Puller, ExplosiveLinear Explosive Assembly (LEA)Linear Explosive Assembly (LEA)Cartridge, Impulse M796Rocket MotorCTG Assembly Cargo HookCartridge, Impulse CCU-92/AThruster, CTG Actuated TCU-3/ACartridge, Impulse, GuillotineConnector, Union (Inert)Connector, Tee (Inert)Connector, Elbow (Inert)Cord, Detonating (FCDC)Cord, Detonating (FCDC)Cord, Detonating (FCDC)Cord, Detonating (FCDC)Cord, Detonating (FCDC)Canopy Severance Assembly Forward PanelArming/Firing InitiatorCanopy Severance Assembly Forward PanelCanopy Severance Assembly Rear PanelCanopy Severance Assembly, Rear PanelCartridge, ImpulseCartridge, Impulse MK 19 MOD 0

DODIC

MS55MS56MS57MS58MS60MS59MS47MS48MD17MS49MS50MD18MD16MD15

MD36MD35MD34MD33

MS76MS77MD73M447PY58MJ21MJ20M520

MS89MS90MS91MS92MS93MS94MT06MS97MS95MS96M657MO12

PAGE

5-415-435-455-475-515-495-255-275-135-295-315-155-115-97-55-235-215-195-1710-55-575-596-258-310-76-239-56-195-1095-1095-1095-895-915-935-955-975-995-1075-1055-1015-1036-216-3

G-2

TM 43-0001-39

P/N NOMENCLATURE DODIC PAGE

813475-121 Cord, Detonating (SMDC) MS61 5-53813475-127 Cord, Detonating (SMDC) MS62 5-55816984 Pin Puller, Explosive Actuated 10-5820810 Thruster, Explosive Actuated 9-72518519 CTG, Aircraft Fire Extinguisher M182 2-32519614 CTG, Aircraft Fire Extinguisher M193 2-52519707 CTG, Aircraft Fire Extinguisher M232 2-75185107 Cartridge, Delay CCU-89/B MH88 4-56261278 Cutter, Delay Propellant Actuated MU11 3-118875978 Cutter, Reef Line M21 M500 3-3897899 Cartridge, Fire Extinguisher MT20 2-11

G-3 (G-4 blank)

TM 43-0001-39

APPENDIX H

CAD/PAD INDEX BY NOMENCLATURE

NOMENCLATURE WITH ITEM IDENTIFIER(S)

Arm-Fire Initiator P/N 814033-101Arming/Firing Initiator JAU-59ACanopy Severance Assembly Forward Panel, MS94Canopy Severance Assembly Rear Panel, MS95Canopy Severance Assembly Rear Panel, MS96Canopy Severance Assembly, Forward Panel, MS97Cartridge, Aircraft Fire Extinguisher MH92Cartridge, Aircraft Fire Extinguisher M182Cartridge, Aircraft Fire Extinguisher M193Cartridge, Aircraft Fire Extinguisher M232Cartridge, Aircraft Fire Extinguisher MT20Cartridge Assembly Cargo Hook PY58Cartridge, Delay CCU-57/B, MF35Cartridge, Delay CCU-89/B MH88Cartridge, Delay M252, M308Cartridge, Impulse M162Cartridge, Impulse, ARD 836-1, M189Cartridge, Impulse, M253Cartridge, Impulse, Mk 104, Mod 0 M291Cartridge Set, Impulse, Reduce Charge Primary M397Cartridge, Impulse Drogue, M507Cartridge, Impulse Guillotine, M520Cartridge, Impulse, M657Cartridge, Impulse, CCU-44/B, MD66Cartridge, Impulse M796, MD73Cartridge, Impulse, CCU-92/A, MJ21Cartridge, Impulse, Mk 19 Mod 0 MO12Cord Assembly Detonating (FCDC) MD15Cord Assembly Detonating (FCDC) MD16Cord Assembly Detonating (SMDC) MD17Cord Assembly Detonating (SMDC) MD18Cord, Detonating (WCA) MD33Cord, Detonating (WCA) MD34Cord, Detonating (WCA) MD35Cord, Detonating (WCA) MD36Cord, Detonating (FCDC) MS89Cord, Detonating (FCDC) MS90Cord, Detonating (FCDC) MS91Cord, Detonating (FCDC) MS92Cord, Detonating (FCDC) MS93Cord, Detonating (SMDC) MS47Cord, Detonating (SMDC) MS48Cord, Detonating (SMDC) MS49

PAGE

7-55-1075-995-1015-1035-1052-92-32-52-72-1110-74-34-54-76-56-76-96-116-136-176-196-216-276-256-236-35-95-115-135-155-175-195-215-235-895-915-935-955-975-255-275-29

H-1

TM 43-0001-39

NOMENCLATURE WITH ITEM IDENTIFIER(S) PAGE

Cord, Detonating (SMDC) MS50 5-31Cord, Detonating (SMDC) MS51 5-33Cord, Detonating (SMDC) MS52 5-35Cord, Detonating (SMDC) MS53 5-37Cord, Detonating (SMDC) MS54 5-39Cord, Detonating (SMDC) MS55 5-41Cord, Detonating (SMDC) MS56 5-43Cord, Detonating (SMDC) MS57 5-45Cord, Detonating (SMDC) MS58 5-47Cord, Detonating (SMDC) MS59 5-49Cord, Detonating (SMDC) MS60 5-51Cord, Detonating (SMDC) MS61 5-53Cord, Detonating (SMDC) MS62 5-55Cord, Detonating (SMDC) MS80 5-71Cord, Detonating (SMDC) MS81 5-73Cord, Detonating (SMDC) MS82 5-75Cord, Detonating (SMDC) MS83 5-77Cord, Detonating (SMDC) MS84 5-79Cord, Detonating (SMDC) MS85 5-81Cord, Detonating (SMDC) MS86 5-83Cord, Detonating (SMDC) MS87 5-85Cord, Detonating (SMDC) MS88 5-87Cutter, Assembly P/N FTL 3648-2 MU03 3-9Cutter, Cartridge Actuated P/N 303104-1 MU02 3-7Cutter, Cartridge Actuated M554 3-5Cutter, Reef Line M21, M500 3-3Linear Explosive Assembly (LEA), MS76 5-57Linear Explosive Assembly (LEA), MS77 5-59Linear Explosive Assembly Window (WCA) 5-61Linear Explosive Assembly, Window (WCA) 5-63Tee Connector (Inert) 87AS101-2 5-65Tee Connector (Inert) 87AS102-1 5-65Pin Puller, Explosive Actuated, P/N 816984-107 10-5Refire Kit 10-3Rocket Motor M447 8-3Thruster, Cartridge Actuated, TCU-1B, MF24 9-3Thruster, Cartridge Actuated, TCU-3A, MJ20 9-5Thruster, Explosive Actuated, P/N 209-033-007-3 9-7

H-2



Chief of Staff

Official:



Distribution:

To be distributed in accordance with DA Form 12-34-E, block 0933, Requirements forTM 43-0001-39.

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