QR Structural Panel Fasteners - Arconic Structural Panel Fasteners Fairchild Fasteners Tridair...

QRStructural Panel Fasteners

The QR Strucutral Panel Fastener qualifies to MIL-F-22978 and meetsMS17731 and MS17732. The QR fastening system is lightweight, hasa small envelope and is fast operating. Most versions lock and unlockin less than two turns. Positive stud retention is featured. Flush orprotruding head styles and various recess configurations are avail-able. Optional stud hold-out grommet is available which providesbottom flush condition. Receptacle provides .020 inch minimum radialfloat. There are other QR Panel Fastener styles and types which arenot featured in this catalog; contact Fairchild Fasteners for details.

Tridair Products 64Fairchild Fasteners

Typical QR Fastening System:

The QR Fastening System has a high-strength-to-weight ratio.Quick operating, it locks and unlocks in less than two turns.Optional stud hold-out grommet is available which providesbottom flush condition.

Stud assembly is retained in retracted positionby sprint-loaded grommet and retaining ring.

Stud assembly is automatically ejeted freefrom sub-structure during unlocking cycle.

QR‘MS’ Version


Retaining RingStandard VersionFX10-1525

Material:18-8 Type 300 Series CRES perAMS 7245 or QQ-W-423.Heat Treat:Stressed relieved.Finish:Passivated per QQ-P-35.Weight:.033 lbs./100, approximate.

Installation Tool for FX10-1525 Retaining Ring:FX10-1530T

Material: Alloy SteelFinish: Black Oxide per MIL-C-13924

To Install FX10-1525 Retaining Ring:

1. Slide retaining ringonto mandrel (Figures Aand B).2. Slide handle ontomandrel (Figure C).

3. Place anvil on top side of panel to brace stud assembly.

Retaining RingOversize Version.FX10-1576

Material: 17-7Ph CRES per AMS 5528.Heat Treat: Rc 44-48.Finish: Passivated per QQ-P-35.Weight: .043 lbs./100, approximate.

Notes:1. Ring is designed to be used when hole in substructure is.391 or greater. See hole preparation on Page 69.2. FX10-1576 retaining ring is hand installed.

4. Align tool assembly onto studassembly and push on handle untilretaining ring is captivated to thestud assembly (Figures D and E).5. Remove tool.

QRStandard Version


Stud AssembliesFlush Head Style.FX10-1558-( )( ) Series

Protruding Head Style.FX10-1559-( )( ) Series

Material:Screw: 8740 Alloy Steel per MIL-S-6049.Grommet: 4140 Alloy Steel per MIL-S-5626.Spring: 17-7PH CRES per AMS 5673.

Heat Treat:Screw and Grommet: 160 K.S.I. minimum ultimate tensilestrength per MIL-H-6875.Spring: Condition CH900 per MIL-H-6875.

Finish:Screw and Grommet: Cadmium Plated per QQ-P-416, TypeII, Class 3.Spring: Passivated per QQ-P-35.

Specifications: See Page 2.

Notes:1. Anti-seize compound per MIL-A-907 applied to thread.2. For retaining ring information see Page 65.

How to Order:FX10 — 1558 — 4 P

Recess options:p = recess per MS9006,No. 10 sizeTS = recess per NAS1078,No. 10 size

Grip range: (see stud part numberselection Page 8 for grip rangerequirements)FX10-1558-4 = .361 to .430FX10-1559-4 = .326 to .395

Head style:FX10-1558 = Flush head styleFX10-1559 = Protruding head style

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QRStandard Version


Stud AssemblyFully Retractable Flush Head Style.FX10-15010-( )P Series

Material:Screw: 8740 Alloy Steel per MIL-S-6049.Grommet: 4140 Alloy Steel per MIL-S-5626.

Heat Treat:Screw and Grommet: 160 K.S.I. minimum ultimate tensilestrength per MIL-H-6875.

Finish:Screw and Grommet: Cadmium Plated per QQ-P-416, TypeII, Class 3.

Specifications: See Page 2.

Notes:1. Use with FX10-15009 hold-out grommet (see Page 6) toprovide flush condition on bottom side of panel in retractedposition, and with FX10-1502( ) Series or FX10-1510( )Series receptacle. Retaining ring is not required.2. Anti-seize compound per MIL-A-907 applied to thread.3. For stud part number selection see Page 8.4. For other head styles and recesses, contact FairchildFasteners.

Receptacle AssembliesFX10-1502( ) SeriesFX10-1510( ) Series

*“A” dimension, when .03 or .08, provides extra jackout to allowstud hold-out spring to engage panel.**Locking feature maintains 5 inch pounds minimum running torque-out after 200 complete cycles.

Material:Receptacle: 1050 Steel per ASI C1050.Nut: 8740 Alloy Steel per MIL-S-6049.Insert: 4140 Alloy Steel per MIL-S-5626.

Heat Treat:Receptacle: Ftu 150 K.S.I. minimum per MIL-H-6875.Nut: Ftu 180 K.S.I. minimum per MIL-H-6875.Insert: Ftu 160 K.S.I. minimum MIL-H-6875.

Finish:Receptacle, Nut, and Insert: Cadmium Plated per QQ-P-416, Type II, Class 3.

Weight: .016 lbs. each, approximate.

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P3-01051-01XF 65. 55. 163. 034. 710.

P4-01051-01XF 36. 26. 134. 005. 910.

P5-01051-01XF 07. 96. 105. 075. 120.

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Hold-Out GrommetFX10-15009-( ) Series

Material:Grommet: 18-8 Type 300 SeriesCRES per ASTM-A-582.Spring: 17-7PH CRES per AMS 5673.

Heat Treat:Grommet: None.Spring: Condition CH900.

Finish:Grommet and Spring: Passivatedper QQ-P-35.

Flaring ToolFX10-15009-T( ) Series

Material:Tool SteelHeat Treat:Rc45 min. perMIL-H-6875Finish:Black Oxide perMIL-C-13924

Stud Assembly Installation ToolFX10-15009-T11Used to install FX10-15010-( )P Series stud assembly intoFX10-15009-( ) grommet assembly.



Notes:1. Use grommet with FX10-15010-( )P Series studassembly and FX10-1502 Series or FX10-1510Series receptacles.2. First and second oversize styles are designed toprovide greater strength or replacement of basic styledue to panel damage.3. See Page 71 for hole preparation and installationinformation.

Back-Up ToolFX10-15009-T( ) Series

Material:Tool SteelHeat Treat:Rc45 min. per MIL-H-6875Finish:Black Oxide per MIL-C-13924

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Panel/Substructure Preparation and Installation Data.

Flush Head Styles.

*Subject to approval of structures group.

Notes:1. Locate and drill “A” diameter hole through panel andsubstructure.

2. Countersink panel to diameter.

3. Counterbore to “B” diameter backside of panel or

frontside of substructure to deep. Location is

optional when “T1” = .125 or greater. Otherwisecounterbore substructure (panel is preferred location).

4. Locate, drill and countersink two holes for rivets (notsupplied).

5. Shim is required when total thickness (“T1” + “T2” plusany compressed gasketing material, paint or other finishes)equals .155 or less. Contact Fairchild Fasteners for details.

Basic Installation.

Notes:1. Place stud assembly into panel.2. Install retaining ring (see Page 3).3. Rivet receptacle in place.

Protruding Head Styles.

Notes:1. Refer to table at left.

2. Locate and drill “A” diameter hole through panel andsubstructure.

3. Counterbore to “B” diameter backside of panel or

frontside of substructure to deep. Location is optional

when “T1” = .065 or greater. Otherwise counterbore sub-structure (Panel is preferred location).

4. Locate, drill and countersink two holes for rivets (notsupplied).

5. Shim is required when total thickness (“T1”+”T2” plus anycompressed gasketing material, paint or other finishes)equals .155 or less. Contact Fairchild Fasteners for details.

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GrommetFX10-15010-( )P Series.

Notes:1. Select grommet dash number to panel “T1” thickness.2. Locate and drill “H” diameter hole through panel.

3. Countersink top of panel to “J” diameter.

4. Counersink bottom of panel to “K” depth.

Stud Assembly and Grommet AssemblyInstallation

Notes:1. Place correct size grommet assembly in panel.

2. Place correct size flaringtool and back-up tool in placeand apply sufficient pressureto flare grommet.

3. Insert pilot of stud installation tool into thread end of studassembly.4. Push tool and stud assembly through grommet until studis captivated by hold-out spring.5. Remove tool.

5. Locate and drill diameter hole through substructure.

6. Locate and drill two holes for rivets (not supplied).

6. Rivet receptacle in place.7. Installation is complete.

Stud Part Number Selectio n

Notes:1. Determine grip range thickness. Note: Grip rangethickness equals “T1” + “T2” plus the compressedthickness of any gasket (if used). Also allow for paint orother finish thickness.2. Refer to appropriate table for stud type and style(see Pages 2, 4 or 5).3. Locate grip range in table and find the correspondingpart no.

Panel/Substrucutre Preparation and Installation Data (cont’d.).

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2-90051-01XF 651. 641.

3-90051-01XF 521. 5715.0515.

066.556.

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4-90051-01XF 651. 641.

5-90051-01XF 521. 5335.0135.

796.296.

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6-90051-01XF 651. 641.

10199

10199

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°°

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GrommetFX10-15009-( )P Series.

Notes:1. Select grommet dash number to panel “T1” thickness.2. Locate and drill “H” diameter hole through panel.

3. Countersink top of panel to “J” diameter.

4. Counersink bottom of panel to “K” depth.

Stud Assembly and Grommet AssemblyInstallation

Notes:1. Place correct size gromet assembly in panel.

2. Place correct size flaringtool and back-up tool in placeand apply sufficient pressureto flare grommet.

3. Insert pilot of stud installation tool into thread end of studassembly.4. Push tool and stud assembly through grommet until studis captivated by hold-out spring.5. Remove tool.

5. Locate and drill diameter hole through substructure.

6. Locate and drill two holes for rivets (not supplied).

6. Rivet receptacle in place.7. Installation is complete.

Stud Part Number Selectio n

Notes:1. Determine grip range thickness. Note: Grip rangethickness equals “T1” + “T2” plus the compressedthickness of any gasket (if used). Also allow for paint orother finish thickness.2. Refer to appropriate table for stud type and style(see Pages 2, 4 or 5).3. Locate grip range on stud assembly drawing and find thecorresponding part dash no.

Panel/Substrucutre Preparation and Installation Data (cont’d.).

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3-90051-01XF 521. 5715.0515.

066.556.

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5-90051-01XF 521. 5335.0135.

796.296.

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10199

10199

.378

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°°

°°

°°

THIS PAGE INTENTIONALLY LEFT BLANK

72

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NOTES:

1. MATERIAL:1.1 SCREW: 8740 ALLOY STEEL PER MIL-S-6049.1.2 GROMMET: 4140 ALLOY STEEL PER MIL-S-56261.3 SPRING: 17-7 PH CRES PER AMS 5673.

2. HEAT TREAT:2.1 SCREW AND GROMMET: 160 K.S.I. MINIMUM ULTIMATE TENSILE STRENGTH PER

MIL-H-6875.2.2 SPRING: CONDITION CH900 PER MIL-H-6875.

3. FINISH:3.1 SCREW AND GROMMET: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS 3.3.2 SPRING: PASSIVATE PER QQ-P-35.

4. .375 DIAMETER HOLE IN T2 MAY BE ENLARGED TO .390 DIAMETER (MAXIMUM) TO ALLOW FOR HOLEMISALIGNMENT.

5. RECESS OPTIONS AND CALLOUTS:5.1 MS9006 RECESS: ADD “P” AFTER DASH NUMBER. EXAMBLE: FX10-1559-2P5.2 NAS1078 RECESS: ADD “TS” AFTER DASH NUMBER. EXAMPLE: FX10-1559-2TS.

6. ANTI-SEIZE COMPOUND PER MIL-A-907 APPLIED TO THREAD.

INSTALLATIONPANEL PREPARATION HOLD-OUT POSITION


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][5- 36. 96. 134. 005. 910.

][6- 07. 67. 105. 075. 120.

][7- 77. 38. 175. 046. 320.

][8- 48. 09. 146. 017. 520.

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][11- 50.1 11.1 158. 029. 130.DRAWING PROVIDES FORM, FITAND FUNTION DATA. DO NOTATTEMPT TO MANUFACTUREPRODUCT USING THIS DRAWING.


NOTES:

1. MATERIAL:1.1 SCREW: 8740 ALLOY STEEL PER MIL-S-6049.1.2 GROMMET: 4140 ALLOY STEEL PER MIL-S-56261.3 SPRING: 17-7 PH CRES PER AMS 5673


MIL-H-6875.2.2 SPRING: CONDITION CH900 PER MIL-H-6875.

3. FINISH:3.1 SCREW AND GROMMET: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS 3.3.2 SPRING: PASSIVATE PER QQ-P-35.

4. USE WITH FX10-1510 OR FX10-1502 RECEPTACLE AND FX10-1525 RETAINING RING.

5. .375 DIAMETER HOLE IN T2 MAY BE ENLARGED TO .390 DIAMETER (MAXIMUM) TO ALLOW FOR HOLEMISALIGNMENT.

6. RECESS OPTIONS AND CALLOUTS:6.1 MS9006 RECESS: ADD “P” AFTER DASH NUMBER. EXAMBLE: FX10-1558-2P.6.2 NAS1078 RECESS: ADD “TS” AFTER DASH NUMBER. EXAMPLE: FX10-1558-2TS.



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INSTALLATIONPANEL PREPARATION HOLD-OUT POSITION




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P2- 94. 84. 192. 063. 510.

P3- 65. 55. 163. 034. 710.

P4- 36. 26. 134. 005. 910.

P5- 07. 96. 105. 975. 120.




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NOTES:

1. MATERIAL:1.1 SCREW: 8740 ALLOY STEEL PER MIL-S-6049.1.2 GROMMET: 4140 ALLOY STEEL PER MIL-S-5626


MIL-H-6875.

3. FINISH:3.1 SCREW AND GROMMET: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS 3.

4. USE WITH FX10-15009 OR CA17064 HOLD-OUT GROMMET TO PROVIDE FLUSHCONDITION ON BOTTOM SIDE OF PANEL IN RETRACTED POSITION, AND FX10-1502RECEPTACLE. SEE GROMMET DRAWING FOR PANEL PREPARATION AND INSTALLATION.

5. AN FX10-1579-T11 INSTALLATION TOOL MUST BE USED TO INSTALL SCREW ASSEMBLYINTO FX10-15009 GROMMET.



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1. MATERIAL:1.1 RECEPTACLE: 1050 STEEL PER AISI C1050 OR AMS 5085.1.2 NUT: 4140 OR 8740 ALLOY STEEL PER MIL-S-5626 OR MIL-S-6049.1.3 INSERT: 4140 ALLOY STEEL PER MIL-S-5626.

2. HEAT TREAT:2.1 RECEPTACLE: FTU 150ksi MINIMUM PER MIL-H-6875.2.2 NUT: FTU 180 KSI MINIMUM PER MIL-H-6875.2.3 INSERT: FTU 160 KSI MINIMUM PER MIL-H-6875.

3. FINISH:3.1 RECEPTACLE, NUT AND INSERT: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS 3.

4. TO BE USED WITH FX10-1500 AND FX10-15000 SERIES, 4 LEAD SCREW ASSEMBLIES.

5. SHIMS FOR THIS RECEPTACLE: SEE FX10-1550 DRAWING.

6. RECEPTACLE MAINTAINS 5 IN-LBS (MINIMUM) RUNNING TORQUE-OUT AFTER 200 COMPLETE CYCLES.

S43

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NOTES:

1. MATERIAL:1.1 RECEPTACLE: 1050 STEEL PER AISI C1050 OR AMS 5085.1.2 NUT: 4140 OR 8740 ALLOY STEEL PER MIL-S-5626 OR MIL-S-6049.1.3 INSERT: 4140 ALLOY STEEL PER MIL-S-5626.

2. HEAT TREAT:2.1 RECEPTACLE: FTU 150 KSI MINIMUM PER MIL-H-6875.2.2 NUT: FTU 180 KSI MINIMUM PER MIL-H-6875.2.3 INSERT: FTU 160 KSI MINIMUM PER MIL-H-6875.

3. FINISH:3.1 RECEPTACLE, NUT AND INSERT: CADMIUM PLATE PER QQ-P-416, TYPE II, CLASS 3.

4. TO BE USED WITH FX10-1500 AND FX10-15000 SERIES, 4 LEAD SCREW ASSEMBLIES.

5. SHIMS FOR THIS RECEPTACLE: SEE FX10-1550 DRAWING.

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NOTES:

1. THIS RING DESIGNED FOR USE ON FX10-1500 SERIES SCREW ASSEMBLIES ANDCA1797 TYPE STUD NUTS.

2. INSTALLATION TOOL:A.) USE FX10-1530T TO INSTALL RINGS ON FX10-1500 SERIES SCREW ASSEMBLYS.B.) USE CA1797-T10 TO INSTALL RINGS ON CA1795-( ) AND CA17036-( ) STUD NUTS.

3. PANEL PREPARATION DATA:A.) RETAINING RING RECESS: C’BORE .531 DIA X .030-.035 DEEP.B.) MAX SUBSTRUCTURE HOLE: .390 DIA.

4. MATERIAL: 18-8 TYPE 300 SERIES CRES, PER MIL-S-5059 AND/OR QQ-S-766 (CHEMISTRY ONLY).

5. HEAT TREAT: STRESS RELIEVE.

6. FINISH: PASSIVATED PER QQ-P-35.

7. WEIGHT: .312 LBS/1000 PIECES (APPROXIMATE).

S42

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DRAWING PROVIDES FORM, FITAND FUNCTION DATA. DO NOTATTEMPT TO MANUFACTUREPRODUCT USING THIS DRAWING.

Fairchild Fasteners

SERCHP7-71 8255SMA

EMANROLAIRETAM NOITACIFICEPS

DEIFICEPSESIWREHTOSSELNU NGNE 07-03-9

GNIRGNINIATER:SECNARELOT:SLAMICED

XX. ± 010.XXX. ± 500.°1±SELGNA

:HSINIF

DETAVISSAP53-P-QQREP

:TAERTTAEH

84-44cR

NGNE

D'PPA 07-4-01

SRENETSAFXAFLACDNASTRESNINOTWENFOS'RFM6263-577-312:SENOHP,80909,AINROFILAC,ECNARROT,.DVLBATIMOL.W0003

6751-01XFYLPPUSLAREDEF

27392EDOC :THGIEW 001/SBL340. :ELACS 1:4 1FO1TEEHS

Trid

air P

rodu

cts

83ETAD VER EGNAHC

07-03-9 F NWARDER&DESIVER

07-11-21 G SECNARELOTDETCERROC

FX10-1576

G


Fairc

hild

Fas

tene

rs

NOTES:1. TO BE USED WITH FX10-1502, FX10-1520, FX10-1570

FX10-1540 SCREW ASSEMBLIES.2. C’BORE .625 +.010 DIA. x .031 DEEP IN

-.000OUTER PANEL, OR INNER STRUCTUREFOR RETAINING RING RECESS.

SERCSEIRES003EPYT8-81-TEMMORG 285-A-MTSA

SERCNP7-71-GNIRPS 5T65SMA


292-57DEIFICEPSESIWREHTOSSELNU NGNE 07-52-2 YSSATEMMORGTUO-DLOHDUTS

:SECNARELOT:SLAMICED

XX. ± 510.XXX. ± 010.

°1±SELGNA

:HSINIF

DETAVISSAP53-P-QQREP

:TAERTTAEH

:GNIRPSDNOC009NC

NGNE

D'PPA CJF 07-4-3



27392EDOC :THGIEW :ELACS 1:4 2FO1TEEHS

Trid

air P

rodu

cts

84ETAD VER EGNAHC

07-02-1 A

07-42-6 B

07-61-01 C

08-11-6 D 0846-OCE

08-51-21 E 4047-OCE

28-42-4 F 0939-OCE

Fairc

hild

Fas

tene

rs

NOTES:

1. SELECT DASH NO. ACCORDING TO PANEL THICKNESS T2. USE FX10-19009-T11 TOOL TO INSTALL STUD IN GROMMET AS

SHOWN ON SHT 23. SEE SHT 2 FOR GROMMET & PANEL PREPARATION

DIMENSIONS.


FX

10

-50

09


292-57DEIFICEPSESIWREHTOSSELNU NGNE 07-52-2 YSSATEMMORGTUO-DLOHDUTS

:SECNARELOT:SLAMICED

XX. ± 510.XXX. ± 010.

°1±SELGNA

:HSINIF :TAERTTAEH NGNE

D'PPA CJF 07-4-3



27392EDOC :THGIEW :ELACS 1:4 2FO2TEEHS

Trid

air P

rodu

cts

85ETAD VER EGNAHC

1TEEHSEES

Fairc

hild

Fas

tene

rs

FX10-15009

F


EZIS .ONTRAP

SNOISNEMIDTEMMORG AERALENAP SLOOTNOITALLATSNI

AOEHTPRAHS

BNIMAID

C'C LLAMS

AID

DMORG

AID

E.TSLLOH

)FER(

FTEMMORG

HTGNEL

GTEMMORG

HTGNEL

TLENAP

CIHT

HELOH

EZIS

JCNIS'C

AID

KLIMS'CHTPED

LGNIRALF

LOOT

M.TSNIDUTS

LOOT

NPU-KCAB

LOOT

CISAB1-90051-01XF

926. 095. 095.994.694.

090.921. 821. 521. 99941 036. 011.

01T-90051-01XF 11T-90051-01XF 21T-90051-01XF2-90051-01XF 451. 991. 691. 0205. 336. 641.

TS1EZISREVO

3-90051-01XF056. 526. 095.

415.115.

690.921. 821. 521. 0515. 596. 011.

91T-90051-01XF 11T-90051-01XF 41T-90051-01XF4-90051-01XF 491. 991. 691. 5715. 066. 641.

DN2EZISREVO

5-90051-01XF756. 096. 095.

035.725.

660.921. 821. 521. 0135. 296. 011.

51T-90051-01XF 11T-90051-01XF 61T-90051-01XF6-90051-01XF 651. 991. 691. 9999. 796. 641.


YBGNIWARD :ETAD97-82-11

ELTIT

LOOTGNIRALFYBDEVORPPA :ETAD97-6-21


:YBDEVORPPA :ETAD DEIFICEPSEGNARREHTFOSSELNUHSINIFECAFRUSSRETEMILLIMSECNARELOT

SEHCNIORCIM521050.20.=XX.SLAMICED520.020.=XXX.

°2=SELGNA

01T-90051-01XF



NOI

SIV

ER


NOTES:1. MATERIAL: TOOL STEEL, AISI TYPE06.

2. HEAT TREAT: Rc 45 MINIMUM PER MIL-H-6875.

3. FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS I.

4. THIS TOOL IS TO BE USED WITH A FX10-15009-T12 BACK-UP TOOLTO INSTALL FX10-15009-1 AND FX10-15009-2 GROMMET.

5. TOOL SHALL HAVE PART NUMBER ETCHED OR STAMPED IN AREA SHOWN.


NOTES:1. MATERIAL: TOOL STEEL.


3. FINISH: BLACK OXIDE PER MIL-C-13924A, CLASS 1.

4. TOOL SHALL HAVE DASH NUMBER, (-T11) ETCHED OR STAMPED ON.374-.369 DIA.


YBGNIWARDRSR

:ETAD97-72-11

ELTIT

LOOTNOITALLATSNI.YSSAWERCS


YBDEVORPPAWLR

:ETAD97-4-21


SEHCNIORCIM521050.20.=XXSLAMICED520.020.=XXX

°2=SELGNA

11T-90051-01XF


NOI

SIV

ER

A#

OL

E6

51

6H

WTL

97-

03-

21


FX10-15010-[ ] SCREW ASSEMBLY(REF.)

FX10-15009-[ ] GROMMET ASSEMBLY(REF.)

FX10-15009-T11 TOOL(REF.)

NOTE:INSERT TOOL AND SCREW ASSEMBLY AS SHOWNTHROUGH TOP SIDE OF GROMMET.



2. HEAT TREAT: Rc 62-67 PER MIL-H-6875.


4. THIS TOOL IS TO BE USED WITH A FX10-15009-T10 FLARE TOOL TOINSTALL FX10-15009-1 AND FX10-15009-2 GROMMETS.

5. TOOL SHALL HAVE PART NUMBER ETCHED OR STAMPED INAREA SHOWN.


YBGNIWARDRSR

:ETAD97-72-11

ELTIT

PUKCAB,LOOTYBDEVORPPA :ETAD97-3-21

YBDEVORPPAWLR

:ETAD97-4-21

:YBDEVORPPA :ETAD DEIFICEPSEGNARREHTOSSELNUHSINIFECAFRUSSRETEMILLIMSECNARELOT


°2=SELGNA

21T-90051-01XF


NOI

SIV

ER

AH

WJ9

7-0

3-2

1B

#O

CE

42

97

TWJ

18-

12-

4






4. THIS TOOL IS TO BE USED WITH A FX10-15009-T14 BACK-UP TOOLTO INSTALL FX10-15009-3 AND FX10-15009-4 GROMMETS




ELTIT


YBDEVORPPAWLR

:ETAD97-4-21



°2=SELGNA

31T-90051-01XF


NOI

SIV

ER

A9

7-0

2-2

1H

WJ




2. HEAT TREAT: Rc 45 PER MIL-H-6875.


4. THIS TOOL IS TO BE USED WITH A FX10-15009-T16 BACKUP TOOL TOINSTALL FX10-15009-5 AND FX10-15009-6 GROMMET.




ELTIT


YBDEVORPPAWLR

:ETAD97-4-21



°2=SELGNA

51T-90051-01XF


NOI

SIV

ER

A9

7-8

2-2

1H

WJ






4. THIS TOOL IS TO BE USED WITH A FX10-15009-T16 BACK-UP TOINSTALL FX10-15009-3 AND FX10-15009-4 GROMMETS.




ELTIT

PU-KCAB,LOOTYBDEVORPPA :ETAD97-3-21

YBDEVORPPACSM

:ETAD97-4-21

:YBDEVORPPAWLR

:ETAD DEIFICEPSEGNARREHTFOSSELNUHSINIFECAFRUSSRETEMILLIMSECNARELOT


°2=SELGNA

51T-90051-01XF


NOI

SIV

ER

A9

7-0

2-2

1H

WJ




2. HEAT TREAT: Rc 62-67 PER MIL-H-6875.


4. THIS TOOL IS TO BE USED WITH A FX10-15009-T15 FLARE TOOL TOINSTALL FX10-15009-5 AND FX10-15009-6 GROMMETS.



YBGNIWARDRSR

:ETAD97-72-11

ELTIT

PU-KCAB,LOOTYBDEVORPPA :ETAD97-3-21

YBDEVORPPAWLR

:ETAD97-4-21


SEHCNIORCIM521050.+20.=XXSLAMICED520.+020.=XXX

°2=+SELGNA

61T-90051-01XF


NOI

SIV

ER

A9

7-8

2-2

1H

WJ


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