STRUCTURAL REPAIR MANUAL PROCESSES — GENERAL · 2. Finishes, Processes and Nondestructive Test...

PROCESSES — GENERAL

1. Individual Process and Finish Codes

A. General Information

This specification contains finish and process letters that have been assigned to individual finishesand processes.

Control specifications such as government, industry or Gulfstream are listed, where applicable, alongwith finish and process description. Gulfstream specifications refer only to those contained elsewherein this manual.

Where two specifications are listed for an item, the upper specification is the material and the lowerthe application specification.

Color numbers shall be in accordance with FED-STD-595, except as otherwise noted.

This specification is not intended to be a complete and comprehensive listing of existing process andfinish information for Gulfstream aircraft. It pertains only to those finishes and processes that arerelevant to the repair of structural components covered in the preceding chapters of this manual.Contact Gulfstream Technical Operations for information not directly available in this specification.See Table 1.

B. Specification Cross Reference List

The following information is provided to ease communication when dealing with Gulfstream TechnicalOperations department in regard to specifications provided in this manual.

Although it has been attempted to relate the intent of the specification, they have not always beentranslated in full.

Should it be necessary to request or refer to the internal Gulfstream document (original), the followinglist shall provide the relevant document information to make the correct request.

In and of itself, the following listing conveys no information of use to an operator beyond abovementioned communication with Gulfstream. See Table 2 for cross reference list.

Table 1: Individual Process And Finish Codes

CODE FINISH / PROCESS GOVERNMENT /INDUSTRY GULFSTREAM

1 Abrasive method, surface prep ____ Preparation of Surfaces by Abrasive Methods,51-28-10, Repair

2 Cadmium plating up to 180 - 200ksi QQ-P-416,Type II, Class 2

20 Corrosion preventative compound MIL-C-16173 Corrosion Inhibitors, 51-13-10, General

35 Black oxide coating MIL-C-13924, Class 1

36Chemical corrosion treatment ofmagnesium and magnesiumalloys

MIL-M-3171 Contact Gulfstream Technical Operations

75 Cadmium coating - Vacuumdeposited

MIL-C-8837, Type II, Class2

76 Chemical film - Alodine 1200 MIL-C-5541, Class 1A Chromate Conversion Coating of Aluminum Alloys,51-21-00, Repair

STRUCTURAL REPAIR MANUAL

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81 Anticorrosion, fuel resistantcoating, integral fuel cells MIL-C-27725 Integral Fuel Tank Coating - MIL-C-27725

Application, 51-22-00, Repair

84 Anodize (hardcoat) MIL-A-8625, Type III

88 Anodize chromic acid MIL-A-8625, Type 1

92 Antistatic coating Antistatic Epoxy Primer - General Application,51-07-10, Repair

120 Chem film alodine - Exterior MIL-C-81706

123 Brush cadmium plate QQ-P-416, Type II

139 Resin coating, unpigmented MIL-R-3043

144 Corrosion preventative coating -Integral fuel tanks MIL-C-27725 Integral Fuel Tank Coating - MIL-C-27725

Application, 51-22-00, Repair

213 Chemical film - Alodine 600 MIL-C-5541, Class 3 Chromate Conversion Coating of Aluminum Alloys,51-21-00, Repair

222 Epoxy primer ____

Epoxy Primer Coating - Preparation andApplication (Including Finish 2012), 51-07-10,RepairEpoxy Primer Coating - Hydraulic Fluid Resistant(Finish 2012), 51-07-10, Repair

2012 Epoxy primer - Skydrol resistant ____

Epoxy Primer Coating - Preparation andApplication (Including Finish 2012), 51-07-10,RepairEpoxy Primer Coating - Hydraulic Fluid Resistant(Finish 2012), 51-07-10, RepairWaterborne Epoxy Primer - Preparation andApplication (Finish 3012), 51-07-10, Repair

2013 Epoxy, fluid resistant topcoat ____ Gloss Epoxy Finish - Application (Includes Finish2013 and 3013), 51-07-10, Repair

3012 Epoxy primer, skydrol resistant,waterborne ____ Waterborne Epoxy Primer - Preparation and

Application (Finish 3012), 51-07-10, Repair

3013 Epoxy, fluid resistant topcoat ____ Gloss Epoxy Finish - Application (Includes Finish2013 and 3013), 51-07-10, Repair

A Structural adhesive bonding ____Composite Components, 51-78-10, GeneralMetal Honeycomb and Metal to Metal BondedAssemblies, 51-79-10, General

M Magnetic particle inspection MIL-STD-1949

AD Installation solid and tubularrivets ____

Hole Preparation Specification - Metallic andComposite Structure Fasteners, 51-42-00, RepairFasteners - Rivets, 51-41-00, StructuralIdentification

AE Installation blind rivets ____

Hole Preparation Specification - Metallic andComposite Structure Fasteners, 51-42-00, RepairFasteners - Hi-Lok / Hi-Tigue, 51-41-00, StructuralIdentification

AF Installation blind bolts ____



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AG Installation Hi-lok fasteners ____


AJ Installation Hi-shear blind boltsrivets ____


APSealing, pressurized areas, skinjoints, faying surfaces, accessclosures and exterior coating

____Sealing Pressurized Areas, Skin Joints, FayingSurfaces, Access Closures and Coating ExteriorSurfaces, 51-22-00, Repair

AS Sealing of surfaces foraerodynamic smoothness ____ Sealing of Surfaces for Aerodynamic Smoothness,

51-14-00, Repair

FB Clean, descale - Titanium andtitanium alloys ____ Cleaning and Descaling of Titanium and Titanium

Alloys, 51-21-00, Repair

FP Penetrant inspect MIL-STD-6866

JBSealing compound; fuel resistant,fillet and faying, -65°F to 360°Fservice

____Fuel Resistant Sealing Compound - Fillet andFaying (−65°F to +360°F Service), 51-21-00,Repair

UA Ultrasonic inspection - Aluminumalloy MIL-STD-2154 Ultrasonic Quality Requirements for Aluminum

Alloy Products, 51-29-00, Repair

US Ultrasonic inspection - Low alloysteel MIL-STD-2154

XR Radiographic inspection MIL-STD-453

PS Passivate CRES QQ-P-35

Table 2: Specification Cross Reference List

SRM TITLE / SECTION GULFSTREAM NO.

Aerodynamic Contour Smoothness, 51-14-00, Repair 1159C-GER-027

Sealing of Surfaces for Aerodynamic Smoothness, 51-14-00, Repair GAMPS 7102

Epoxy Primer Coating - Preparation and Application (Including Finish 2012), 51-07-10,Repair GAMPS 3103

Chromate Conversion Coating of Aluminum Alloys, 51-21-00, Repair GAMPS 6108

Cleaning and Chemical Surface Treatment of Aircraft Surfaces, 51-21-00, Repair GAMPS 3201

Surface Preparation and Painting Procedure, 51-07-10, Repair GAMPS 4000

Alkaline Cleaning of Ferrous and Nonferrous Alloys, 51-21-00, Repair GAMPS 4105

Cleaning and Descaling of Titanium and Titanium Alloys, 51-21-00, Repair GAMPS 4107

Epoxy Primer Coating - Hydraulic Fluid Resistant (Finish 2012), 51-07-10, Repair GMS 5001

Sealing Pressurized Areas, Skin Joints, Faying Surfaces, Access Closures and CoatingExterior Surfaces, 51-22-00, Repair GAMPS 7101

Aerodynamic Sealant Compound, 51-21-00, Repair GAC 115W


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SRM TITLE / SECTION GULFSTREAM NO.

Fuel Resistant Sealing Compound - Fillet and Faying (−65°F to +360°F Service), 51-21-00,Repair GMS 4107

Waterborne Epoxy Primer - Preparation and Application (Finish 3012), 51-07-10, Repair GAMPS 3116

Gloss Epoxy Finish - Application (Includes Finish 2013 and 3013), 51-07-10, Repair GAMPS 3205

Swaging of Tubing to Deutsch PermaswageT Fittings, 51-27-00, Repair GAMPS 2507

Ultrasonic Quality Requirements for Aluminum Alloy Products, 51-29-00, Repair GAMPS 9101

Epoxy Topcoat - Hydraulic Fluid Resistant Series 2000, 51-07-10, Repair GMS 5002

Compound Sealant Polysulfide, 51-22-00, General GC115AL

Faying Surface Sealing Compound - Corrosion Inhibitive, 51-22-00, Repair GMS 4108

Integral Fuel Tank Coating - MIL-C-27725 Application, 51-22-00, Repair GAMPS 3102

Hole Preparation Specification - Metallic and Composite Structure Fasteners, 51-42-00,Repair GAH11AL

Preparation of Surfaces by Abrasive Methods, 51-28-10, Repair GAMPS 4101

Application of Epoxy Polyamide Primer Coating, 51-07-10, Repair GAMPS 3104

Urethane Enamel - Preparation and Application, 51-07-10, Repair GAMPS 3209

White Primer Coating / Sanding Sealer, 51-07-10, Repair GAMPS 3105

GIV Finish Specification, 51-14-00, Repair SP-FS-159-3C

Individual Process and Finish Codes, 51-20-00, General GAF14A

Antistatic Epoxy Primer, 51-07-10, Repair GMS 5003

Antistatic Epoxy Primer - General Application, 51-07-10, Repair GAMPS 3113

Electrical Bonding Requirements, 51-80-00, Repair GAMPS 2605

Metal Honeycomb and Metal to Metal Bonded Assemblies, 51-79-10, GeneralComposite Components, 51-78-10, General

GAMPS 4104

GAMPS 4108

GAMPS 8101

GAMPS 8109

GAMPS 8110

GAMPS 8115

GAMPS 8118

2. Finishes, Processes and Nondestructive Test (NDT) Inspection — Methodology and Equipment

A. Protective Treatment of Aluminum (Optional)

Where chromic acid anodize, MIL-A-8625, Type I is specified, sulfuric acid anodize, nondyed andsealed, per MIL-A-8625, Type II, Class 1 may be substituted.

NOTE: Approval from Gulfstream Technical Operations is required prior to substitution since thereare items where sulfuric acid anodizing may be questionable as a substitution (parts withjoints, seams, recesses, etc. that could entrap fluids or parts that will be adhesive bonded).


51-20-00February 29/04

Where Alodine 1000 is called out on drawings, sulfuric acid anodize, nondyed, unsealed, per MIL-A-8625, Type II, Class 1 may be substituted.

NOTE: Restricted to stair treads and associated hardware.

Where Alodine 1000 or MIL-C-5541, Class 1A is specified Alodine 600 may be substituted.

Where Alodine 600 / MIL-C-5541, Class 3 is specified, Alodine 1200 may be substituted.

NOTE: In order to maintain an equivalent electrical conductivity with the Alodine 1200 finish it iscritical that the proper solution concentrations and immersion dwell times per chromateconversion coating of aluminum alloys be adhered to. See Chromate Conversion Coating ofAluminum Alloys, 51-21-00, Repair.

B. Cadmium Plating of Steel Parts (Optional)

Where electro-deposited cadmium plating per QQ-P-416 is specified, vacuum deposited cadmiumplating per MIL-C-8837, Type II, Class 2 may be substituted.

NOTE: Vacuum cadmium plating of all steel parts heat treated above 180,000 psi requiresGulfstream Technical Operations review and approval.

When vacuum cadmium plating is utilized, parts must pass a dry tape adhesion test usingfresh (less than 6 months old) 3M No. 254 tape. Parts failing this test shall be stripped andreprocessed to attain satisfactory adhesion.

C. Age Control of Elastomeric Material (Mandatory)

Age sensitive elastomeric materials must meet the requirements of MIL-STD-1523.

D. Surface Finish Requirements

Surface roughness of routed sheet metal edges (mandatory) - Unless otherwise specified on theengineering drawing, all routed sheet metal edges shall be finished to 125 RMS.

E. Nondestructive Tests

Nondestructive Test (NDT) inspection procedures (methodology and equipment).

NOTE: Refer to GIV NDT Manual for inspection procedures.

F. Hardness Testing of Metals

Procedure - Hardness tester verification (to be performed by qualified personnel).

– Testers with Rockwell or Brinell scales shall be verified by using the correct side of a standardtest block on each instrument at the beginning of each investigation. Each time a new scale isused, it shall also be verified by the specific test block.

– Conductivity meters shall be operated only by qualified individuals who are well conversed withaerospace NDT procedures. Instrument calibration verification via standards attached to eachmeter shall constitute proper preliminary equipment testing.

Operation - Testers with Rockwell, Brinell and Barcol Scales:

NOTE: Surface finish is essential for obtaining accurate readings against the parts in question. Theprepared surface should not exceed (RMS) ME4V SQ 125 and or 125 micro inches orbetter.

– Valid hardness readings require proper combination of load and penetration, correct anvil and asmooth, flat, properly prepared surface normal to the axis of the indenter. See Figure 1 andFigure 2.

– Reading shall be taken in areas where indentations cannot later contribute to failure. Only


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material that will not be destroyed or mutilated beyond serviceability shall be tested by thismethod.

– Limit the number of indentations to the minimum necessary for accurate determination.– When testing curved surfaces correction factors must be added.– When a part cross section is relatively constant, hardness may be determined by a single

reading.– When part cross section changes significantly or when a narrow hardness range is required,

three readings are taken and averaged.– When three Rockwell readings are taken, they must be within two hardness points of each

other.– When three Brinell readings are taken, they must be within 20 hardness points of each other.– When evidence of a hardness indentation in contact with an anvil is observed on the reverse

side of the part, the hardness reading is not valid.– When decarburization or other surface condition is suspected of causing erroneous readings,

the surface condition can be removed provided the part tolerance is not exceeded.

Valid conductivity readings require a smooth, flat surface normal to the axis of the probe.

Requirements

– Table 3 establishes Rockwell correction factors which are added when testing convexcylindrically curved surfaces.

– Table 4 established minimum material thickness for each Rockwell hardness scale.– Table 5 establishes approximate equivalent Rockwell hardness values for steel.– Table 6 establishes approximate equivalent Rockwell hardness values for wrought aluminum.– Table 7 establishes Rockwell and Brinell hardness values for the following:

Wrought carbon steels (1015, 1018, 1020, 1025, 1065, 1095, drill rod and hi-carbon musicwire).Wrought low alloy steels (3312, 4130, 4140, 4330 Va. Modified, 4340, 6150, 8740, D6 AC,Graph-Mo, H-11 and hy-tuff).Wrought Martensitic stainless steels (410, 416, 420, 431 and 40-G).

– Table 8 establishes hardness to tensile strength values for wrought carbon and low alloy steels.– Table 9 establishes hardness requirements for wrought aluminum alloys.– Table 10 establishes electrical conductivity requirements for wrought aluminum alloys.– Table 11 establishes hardness requirements for aluminum alloy and magnesium alloy castings.– Table 12 establishes hardness requirements for wrought precipitation hardening, corrosion and

heat resistant alloys.– Table 13 establishes hardness requirements for copper alloys.– Table 14 establishes hardness requirements for titanium alloys.– Other approved type hardness testers may be used in accordance with the manufacturer’s

data.

Laboratory tensile testing - When the hardness check is carried out on a fire damaged structure andis inconclusive, a section of the damaged structure must be cut out and tensile tested to determinethe serviceability of the remaining part of the structure. When sending parts or samples to thelaboratory for analysis, include a descriptive report about the type and duration of the fire.

NOTE: Gulfstream Technical Operations review and approval required.


51-20-00February 29/04

Table 3: Rockwell Hardness Scale

ROCKWELL CORRECTION FACTORS ADDED FOR CYLINDRICALLY CURVED SURFACES (1)

Diameter Of Specimen Or Part (Inches)

Scale ObservedReading 1/4 3/8 1/2 5/8 3/4 7/8 1.0

EFG

100 3.3 2.5 1.3 1.5 1.0 1.0 0.5

90 4.0 3.0 2.0 1.5 1.5 1.5 1.0

80 5.0 3.5 2.5 2.0 1.5 1.5 1.5

70 6.0 4.0 3.0 2.5 2.0 2.0 1.5

60 7.0 5.0 3.5 3.0 2.5 2.0 2.0

50 8.0 5.5 4.0 3.5 3.0 2.5 2.0

40 9.0 6.0 4.5 4.0 3.0 2.5 2.5

30 10.0 6.5 5.0 4.5 3.5 3.0 2.5

20 11.0 7.5 5.5 4.5 4.0 3.5 3.0

10 12.0 8.0 6.0 5.0 4.0 3.5 3.0

0 12.5 8.5 6.5 5.5 4.5 3.5 3.0

ACD

80 0.5 0.5 0.5 0 0 0 0

70 1.0 1.0 0.5 0.5 0.5 0 0

60 1.5 1.0 1.0 0.5 0.5 0.5 0.5

50 2.5 2.0 1.5 1.0 1.0 0.5 0.5

40 3.5 2.5 2.0 1.5 1.0 1.0 1.0

30 5.0 3.5 2.5 2.0 1.5 1.5 1.0

20 6.0 4.5 3.5 2.5 2.0 1.5 1.5

Scale ObservedReading 1/8 1/4 3/8 1/2 5/8 3/4 1.0

15N30N45N

90 0.5 0.5 0 0 0 0 0

85 0.5 0.5 0.5 0 0 0 0

80 1.0 0.5 0.5 0.5 0 0 0

75 1.5 1.0 0.5 0.5 0.5 0.5 0

70 2.0 1.0 1.0 0.5 0.5 0.5 0.5

65 2.5 1.5 1.0 0.5 0.5 0.5 0.5

60 3.0 1.5 1.0 1.0 0.5 0.5 0.5

55 3.5 2.0 1.5 1.0 1.0 0.5 0.5

50 3.5 2.0 1.5 1.0 1.0 1.0 0.5

45 4.0 2.5 2.0 1.0 1.0 1.0 1.0

40 4.5 3.0 2.0 1.5 1.0 1.0 1.0


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ROCKWELL CORRECTION FACTORS ADDED FOR CYLINDRICALLY CURVED SURFACES (1)

Diameter Of Specimen Or Part (Inches)

15T30T45T

90 1.5 1.0 1.0 0.5 0.5 0.5 0.5

80 3.0 2.0 1.5 0.5 1.0 1.0 0.5

70 5.0 3.5 2.5 2.0 1.5 1.0 1.0

60 6.5 4.5 3.0 2.5 2.0 1.5 1.5

50 8.5 5.5 4.0 3.0 2.5 2.0 1.5

40 10.0 6.5 4.5 3.5 3.0 2.5 2.0

30 11.5 7.5 5.0 4.0 3.5 2.5 2.0

20 13.0 9.0 6.0 4.5 3.5 3.0 2.0

(1) Per Wilson (Rockwell) Chart No. 55.

Table 4: Minimum Material Thickness for Each Hardness Scale

THICKNESS SCALE

Inches 15M 30M 45M A B C

0.006 92 — — — — —

0.005 90 — — — — —

0.010 88 — — — — —

0.012 83 82 77 — — —

0.014 76 80 74 — — —

0.016 68 74 72 86 — —

0.018 X 66 68 84 — —

0.020 X 57 63 82 77 —

0.022 X 47 58 78 75 69

0.024 X X 51 76 72 67

0.026 X X 37 71 68 65

0.028 X X 20 67 63 62

0.030 X X X 60 58 57

0.032 X X X X 51 52

0.034 X X X X 43 45

0.036 X X X X X 37

0.038 X X X X X 28

0.040 X X X X X 20

INCHES 15T 30T 45T F B C

0.005 93 — — — — —

0.010 90 87 — — — —


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THICKNESS SCALE

0.015 78 77 77 — — —

0.020 X 58 62 100 — —

0.025 X X 26 92 92 90

0.030 X X X 67 68 69

0.035 X X X X 44 46

0.040 X X X X 20 22

NOTE: X signifies no minimum hardness.

This table per Wilson (Rockwell) chart No. 55.

Table 5: Hardness Testing (Steel)

ROCKWELL HARDNESS ROCKWELL SUPERFICIAL BRINELL HARDNESS TENSILESTRENGTH

APPROXX 10`PSI

C150 KgBrale

A60 KgBrale

15-N15 Kg

NBrale

30-N30 Kg

NBrale

45-N45 Kg

NBrale

3000 KgBrinell

Hultgren 10 MMBall

68 85.5 — 84.5 75.5

67 85.0 93.0 83.5 74.5

66 84.5 92.5 83.0 73.0

65 84.0 92.0 82.0 72.0

64 83.5 — 81.0 71.0

63 83.0 91.5 80.0 70.0

62 82.5 91.0 79.0 69.0

61 81.5 90.5 78.5 67.5

60 81.0 90.0 77.5 66.5 614

59 80.5 89.5 76.5 65.5 600

58 80.0 — 75.5 64.0 587

57 79.5 89.0 75.0 63.0 573

56 79.0 88.5 74.0 62.0 560

55 78.5 88.0 73.0 61.0 547 301

54 78.0 87.5 72.0 59.5 534 291

53 77.5 87.0 71.0 58.5 522 282

52 77.0 86.5 70.5 57.5 509 273

51 76.5 86.0 69.5 56.0 496 264

50 76.0 85.5 68.5 55.0 484 255

49 75.5 85.0 67.5 54.0 472 246

48 74.5 84.5 66.5 52.5 460 237


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ROCKWELL HARDNESS ROCKWELL SUPERFICIAL BRINELL HARDNESS TENSILESTRENGTH

APPROXX 10`PSI

C150 KgBrale

A60 KgBrale

15-N15 Kg

NBrale

30-N30 Kg

NBrale

45-N45 Kg

NBrale

3000 KgBrinell

Hultgren 10 MMBall

47 74.0 84.0 66.0 51.5 448 229

46 73.5 83.5 65.0 50.0 437 221

45 73.0 83.0 64.0 49.0 426 214

44 72.5 82.5 63.0 48.0 415 207

43 72.0 82.0 62.0 46.5 404 200

42 71.5 81.5 61.5 45.5 393 194

41 71.0 81.0 60.5 44.5 382 188

40 70.5 80.5 59.5 43.0 372 182

39 70.0 80.0 58.5 42.0 362 177

38 69.5 79.5 57.5 41.0 352 171

37 69.0 79.0 56.5 39.5 342 166

36 68.5 78.5 56.0 38.5 332 162

35 65.0 78.0 55.0 37.0 322 157

34 67.5 77.0 54.0 36.0 313 153

33 67.0 76.0 53.0 35.0 305 148

32 66.5 76.0 52.0 33.5 297 144

31 66.0 75.5 51.5 32.5 290 140

30 65.5 75.0 50.5 31.5 283 136

29 63.0 74.5 49.5 30.0 276 132

28 64.5 74.0 43.5 29.0 270 129

27 64.0 73.5 47.5 28.0 265 126

26 63.5 72.5 47.0 26.5 260 123

25 63.0 72.0 46.0 25.5 255 120

24 62.5 71.5 45.0 24.0 250 117

23 62.0 71.0 44.0 23.0 245 115

22 61.5 70.5 43.0 22.0 240 112

21 61.0 70.0 42.5 20.5 235 110

20 60.5 69.5 41.5 19.5 230 108


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Table 6: Hardness Testing (Aluminum)

ROCKWELL HARDNESS ROCKWELL SUPERFICIAL BRINELL HARDNESS

BARCOLREADING (1)

TENSILESTRENGTH

APPROXX 10`PSI

B100 Kg

1/16 InchBall

A60 KgBrale

15-T15 Kg

1/16 InchBall

30-T30 Kg

1/16 InchBall

45-T45 Kg

1/16 InchBall

500 Kg10 MM

Ball

3000 KgD.P.H10 Kg

100 61.5 93.0 82.0 72.0 201 240 116

99 61.0 92.5 81.5 71.5 195 234 112

98 60.0 — 81.0 70.0 189 228 109

97 59.5 92.0 80.5 69.0 184 222 106

96 59.0 — 80.0 68.0 179 216 103

95 58.0 91.5 79.0 67.0 175 210 101

94 57.5 — 78.5 66.0 171 205 98

93 57.0 91.0 78.0 65.5 167 200 96

92 56.5 90.5 77.5 64.5 163 195 93

91 56.0 — 77.0 63.5 160 190 91

90 55.5 90.0 76.0 62.5 157 185 89

89 55.0 89.5 75.5 61.5 154 180 87

88 54.0 — 75.0 60.5 151 176 85

87 53.5 89.0 74.5 59.5 148 172 83

86 53.0 88.5 74.0 58.5 145 169 81

85 52.5 — 73.5 58.0 142 165 80

84 52.0 88.0 73.0 57.0 140 162 78

83 51.0 87.5 72.0 56.0 137 159 77

82 50.5 — 71.5 55.0 135 156 75

81 50.0 87.0 71.0 54.0 133 153 74

80 49.5 86.5 70.0 53.0 130 150 72

79 49.0 — 69.5 52.0 128 147

78 48.5 86.0 69.0 51.0 126 144

77 48.0 85.5 68.0 50.0 124 141

76 47.0 — 67.5 49.0 122 139

75 46.5 85.0 67.0 48.5 120 137

74 46.0 — 66.0 47.5 118 135

73 45.5 84.5 65.5 46.5 116 132

72 45.0 84.0 65.0 45.5 114 130

71 44.5 — 64.0 44.5 112 127

70 44.0 83.5 63.5 43.5 110 125


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BARCOLREADING (1)

TENSILESTRENGTH

APPROXX 10`PSI

B100 Kg

1/16 InchBall

A60 KgBrale

15-T15 Kg

1/16 InchBall

30-T30 Kg

1/16 InchBall

45-T45 Kg

1/16 InchBall

500 Kg10 MM

Ball

3000 KgD.P.H10 Kg

69 43.5 83.0 62.5 42.5 109 123 89.0

68 43.0 — 62.0 41.5 107 121

67 42.5 82.5 61.5 40.5 106 119

66 42.0 82.0 60.5 39.5 104 117

65 — — 60.0 38.5 102 116 87.0

64 41.5 81.5 59.5 37.5 101 114

63 41.0 81.0 58.5 36.5 99 112

62 40.5 — 58.0 35.5 98 110 85.0

61 40.0 80.5 57.0 34.5 96 108

60 39.5 — 56.5 33.5 95 107 83.5

59 39.0 80.0 56.0 32.0 94 106

58 39.5 79.5 55.0 31.0 92 104 82.0

57 38.0 — 54.5 30.0 91 103

56 — 79.0 54.0 29.0 90 101

55 37.5 78.5 53.0 28.0 89 100

54 37.0 — 52.5 27.0 87 80.0

53 36.5 78.0 51.5 26.0 86

52 36.0 77.5 51.0 25.0 85 79.0

51 35.5 — 50.5 24.0 84

50 35.0 77.0 49.5 23.0 83

49 — 76.5 49.0 22.0 82 77.5

48 34.5 — 48.5 20.5 81

47 34.0 76.0 47.5 19.5 80

46 33.5 75.5 47.0 18.5 —

45 33.0 — 46.5 17.5 79

44 32.5 75.0 45.5 16.5 78 76.0

43 32.0 74.5 45.0 15.5 77

42 31.5 — 44.0 14.5 76

41 31.0 74.0 43.5 13.5 75 75.0

40 — 73.5 43.0 12.5 —

39 30.5 — 42.0 11.0 74

38 30.0 73.0 41.5 10.0 73


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BARCOLREADING (1)

TENSILESTRENGTH

APPROXX 10`PSI

B100 Kg

1/16 InchBall

A60 KgBrale

15-T15 Kg

1/16 InchBall

30-T30 Kg

1/16 InchBall

45-T45 Kg

1/16 InchBall

500 Kg10 MM

Ball

3000 KgD.P.H10 Kg

37 29.5 72.5 40.5 9.0 72

36 29.0 — 40.5 8.0 — 73.5

35 28.5 72.0 39.5 7.0 71

34 28.0 71.5 38.5 6.0 70 73.0

33 — — 38.0 5.0 69

32 27.5 71.0 37.5 4.0 —

31 27.0 — 36.5 3.0 68 72.5

30 26.5 70.5 36.0 2.0 67

29 26.0 70.0 35.5 1.0 —

28 25.5 — 34.5 66 72.0

27 25.0 69.5 34.0 —

26 24.5 69.0 33.0 65

25 — — 32.5 64 71.0

24 24.0 68.5 32.0 —

23 23.5 68.0 31.0 63

22 23.0 — 30.5 — 70.0

21 22.5 67.5 29.5 62

20 22.0 — 29.0 —

19 21.5 67.0 28.5 61 69.5

18 — 66.5 27.5 —

17 21.0 — 27.0 60 68.5

16 20.5 66.0 26.0 —

15 20.0 65.5 25.5 59

14 — 25.0 — 67.5

13 65.0 24.0 58

12 64.5 23.5 —

11 — 23.0 — 66.5

10 64.0 22.0 57

9 — 21.5 —

8 63.5 20.5 — 66.0

7 63.0 20.0 56

6 — 19.5 —


51-20-00

February 29/04


BARCOLREADING (1)

TENSILESTRENGTH

APPROXX 10`PSI

B100 Kg

1/16 InchBall

A60 KgBrale

15-T15 Kg

1/16 InchBall

30-T30 Kg

1/16 InchBall

45-T45 Kg

1/16 InchBall

500 Kg10 MM

Ball

3000 KgD.P.H10 Kg

5 62.5 18.5 55 65.5

4 62.0 18.0 —

3 — 17.0 — 65.0

2 61.5 16.5 54

1 61.0 16.0 —

0 — 15.0 53 64.0

(1) The barcol readings are based upon the engineering data chart established by Barber-Colman Company, GYZJ 934-1.

Table 7: Wrought / Low Alloy Steel Hardness Values

ALLOY SPEC FORM COND STANDARD SUPERFICIAL BRINELL

Low carbonsteel QQ-W-461 Safety wire Annealed B92 max

Spring steel(1060) QQ-W-428 Spring wire

Annealed B93

Spring temper C40 - 45 30N 59.5 - 64

High carbonspring steel QQ-A-470 Spring wire Spring temper

Carbon steel1010 - 10361112 - 1137

CommercialQQS-S-633 Bar (rod) Hot rolled

Cold finished C21 max 30N 42.3 max

1035 QQ-S-631 Bar (rod)Hot rolled 241

Cold finished 221

1070 Commercial Bar (rod) Annealed C21 max 30N 42.3 max

1095 MIL-S-8559 Bar (rod)Spherodizeanneal, cold

finishedB95 max 229 max

Carbon steel1010 - 1018 Commercial Sheet

Soft temper B60 max

Full hard temper B84 - 96

1095 MIL-S-7947 Sheet (strip)Spherodizedannealed, hot

rolledB85 max


51-20-00February 29/04


4130

MIL-S-6758 Bar (rod) forgings Annealed C21 max

MIL-18727 Sheet (plate)

Normalized<0.187 B93 min

Normalized 0.188- 1.5B91 min

Annealed B88 max

MIL-T-6736 Tubing

Normalized<0.187 wall B93 min

Normalized>0.187 wall B91 min

AMS 6371 TubingHot finished B99 max

Cold finished C25 max

4135 MIL-T-6735 Tubing

Normalized<0.187 wall B96 min

Normalized>0.187 wall

4140 MIL-S-5626 Bar (rod) forgings

Normalized 311 max

Annealed C21 max 229 max

Cold finished C23 max 241 max

4330 Mod AMS 6427

Bar (rod) forgings

Hot finish bar 241 max

Annealed forging 241 max

Cold finish bar 248 max

NormalizedT-forgings 248 max

TubingHot finish B99 max

Cold finish C25 max

4340

MIL-S-5000 Bar (rod) forgings

Annealed C22 max 235

Cold finished C27 max 265

Normalized(Tempered) C27

AMS 6414 Bar (rod) forgings(VAC Melt)

Hot finished 229 max

Cold finished 245 max

AMS 6359 Sheet (plate)Sheet B98 max

Hot finished plate C25 max

AMS 6415 Tubing (mech)Hot finished C22 max

Cold finished C30 max


51-20-00

February 29/04


301 MIL-S-5059

Sheet (strip)

Annealed B95 max

1/4 Hard C20 -31

1/2 Hard C28 - 36

plate3/4 Hard C33 -45

Hard C38 min

302

QQ-W-423Wire Spring temper B88 min

Other products

Annealed B95 max

MIL-S-50501/4 Hard C25 - 35

1/2 Hard C32 - 40

QQ-S-7633/4 Hard C37 - 42

Hard C40 - min

303QQ-S-763

All productsAnnealed B95 max

QQ-S-764 1/4 Hard C25-35

304QQ-S-763

All products Annealed B95 maxQQ-S-764

305 QQ-S-763 Bar (rod) Annealed C27 max

310

QQ-S-763 Bar (rod) Annealed B90 max

AMS 5521 Sheet strip (plate) Solution H.T. B90 max

AMS 5368 Casting As Cast —

316

MIL-S-5059 Sheet strip (plate)

Annealed B95 max 30 T78 max 217 max

1/4 Hard C25 - 35 — 255 max

1/2 Hard C32 - 40 372 max

QQ-W-423 Wire Spring temper B88 min

QQ-S-763 Bar (rod)Annealed C25 max

Cold Work B88 min

321

MIL-S-6721 Sheet strip (plate)Annealed B95 max

1/4 Hard C25

QQ-S-763 Bar (rod)Cold Work B88 min

Annealed C25 max

QQ-W-423 Wire Spring temper B88 min

MIL-S-867 Casting Annealed B87 max 170 max

347

QQ-S-763 Bar (rod) Annealed C25 max 30 N 46 max 241 max

MIL-S-6721 Sheet strip (plate) Annealed B95 max 30 T79 max 210 max

MIL-S-8844 Casting Annealed B83 max 160 max


51-20-00February 29/04


4340 MIL-S-8844 Bar Tubing(mechanical)

Hot finishedBar / Annealed C27 max 265 max

Annealed Tube B99 max

NormalizedTempered C33 max 311 max

300 M AMS 6417Bar forgings

Tubing(Mechanical)

Hot finished Bars 241 max

Cold finishedBars 262 max

Normalized /Tempered 248 max

Hot finished Tube B99 max

Cold finishedTube B25 max

8615 - 8630 MIL-S-8690 Bar (rod)forgings Annealed C21 max 229 max

8735 MIL-S-6098 Bar (rod)Annealed C21 max 229 max


8740MIL-S-6049

Bar (rod)Annealed C21 max 229 max

AMS 6322 Cold finished C23 max 241 max

9310 AMS 6260Bar (rod)Tubing

(Mechanical)



Hot finishedTubing B99 max

Cold finishedTubing C25 max

52100 MIL-S-7420 BarNot finished B94.5 max 207 max


H-11 AMS 6487 Bar forgings



Normalized /Temperedforgings

248 max

Table 8: Hardness to Tensile Strength Values for Wrought Carbon and Low Alloy Steels

HEAT TREAT COND OR TENSILESTRENGTH RANGE ROCKWELL SCALE BRINELL

PSI B C Diameter OfImpression

HardnessNumber

Annealed 78 — 5.03 141


51-20-00

February 29/04

HEAT TREAT COND OR TENSILESTRENGTH RANGE ROCKWELL SCALE BRINELL

PSI B C Diameter OfImpression

HardnessNumber

Annealed 90 — 4.47 181

Normalized 90 — 4.45 183

120 / 150 KSI — 27 - 32 3.73 - 3.50 265 - 302

150 / 165 KSI — 33 - 37 3.45 - 3.23 311 - 345

165 / 180 KSI — 37 - 40 3.28 - 3.16 345 - 373

180 / 200 KSI — 39 - 42 3.20 - 3.09 363 - 391

200 / 220 KSI — 43 - 46 3.05 - 2.94 401 - 432

220 / 240 KSI — 46 - 49 2.94 - 2.84 432 - 464

240 / 260 KSI — 49 - 52 — —

260 / 280 KSI — 50 - 53 — —

280 / 305 KSI — 53 - 56 — —

Table 9: Hardness Requirements for Wrought Aluminum Alloys

ALLOY ANDTEMPER (1)

ROCKWELL HARDNESS SCALE

B E H 15T 30T

2024 / 2124-0 — 73 max 95 max — 34 max

-T3 and T4 69 - 83 97 - 106 111 - 118 87 - 93 62 - 72

-T36 76 - 90 100 - 110 — 85 - 90 —

-T6 73 - 84 98 - 106 — 83 - 88 62 - 68

-T81 75 - 84 99 - 106 — 84 - 88 —

-T84 81 min — — 86 min 71 min

-T86 83 - 90 105 - 110 — 87 - 90 —

-T351 69 min 97 min — 83 min 62 min

-T851 76 min 100 min — 85 min 67 min

O Clad — — 90 max — —

-T3 and T4 Clad 52 - 71 91 - 102 109 - 116 — —

-T81 Clad 60 min — — — —

2219-0 — 73 max 95 max — 34 max

-T31 58 - 72 — — 80 - 84 56 - 65

-T351 and T352 50 - 75 — — — 49 - 67

-T62 59 min 93 min — 80 min 56 min

-T81 68 - 85 — — 82 - 88 62 - 73


51-20-00February 29/04

ALLOY ANDTEMPER (1)


B E H 15T 30T

-T851 and T852 70 - 86 — — — 63 - 74

-T87 71 min — — 83.5 min 64 min

5052-0 — 65 max 92 max 66 max —

-H32 — 61 - 81 — 63 - 74 —

-H34 — 67 - 84 — 65 - 75 —

-H36 — 73 - 87 — 70 - 77 —

-H38 — 80 - 90 — 75 - 79 —

6160-0 — — 75 max — —

-T4 Sheet — 60 - 85 88 - 100 64 - 75 —

-T4 Extrusion — 70 - 85 82 - 103 67 - 78 —

-T6 XX 47 min 85 - 97 — 78 - 84 —

-T6 Clad — 84 - 96 — — —

6063-T5 — 55 - 70 89 - 97 63 - 70 —

-T6 — 70 - 85 — — —

7075-0 Bare andClad — 73 max 95 max — 34 max (Bare)

-T6 and T65X 85 - 94 106 - 114 — 87 - 92 —

-T6 Clad 73 - 88 102 - 110 — — —

-T73XXX 78 - 89 102 - 108 — 86 min 69 min

7079-T6 and T65 X 81 - 93 104 - 114 — 87 - 92 —

7175-T736 85 - 94 106 -114 — 87 - 92 —

7178-T6 85 min 105 min — 88 min —

-T6 Clad 82 min 102 min — — —

-T76 and T765XXX 84 min — — — 73 min

7050-T73XXX 81 - 94 104 - 114 — — 71 - 79

-T76XX 81 - 94 104 - 114 — — 71 - 79

7049-T73 81 - 93 104 - 114 — — 71 - 79

1100-0 — — 50 max — —

-H12 — — 46 min — —

-H14 — — 65 min — —

-H16 — — 67 min — —

-H18 — — 74 min — —

3003-0 — — 65 max — —

-H12 — — 68 min — —


51-20-00

February 29/04

ALLOY ANDTEMPER (1)


B E H 15T 30T

-H14 — — 80 - 90 — —

-H16 — — 88 - 95 62 - 68 —

-H18 — 66 - 75 — 66 - 73 —

2014-0 (Bare andClad) — — 95 max —

-T3 and T4 65 - 70 95 - 100 — — 60 min

T6 and T65X 78 - 90 102 - 110 — 86 - 90 69 - 76

T6 Clad 74 - 82 101 - 106 — — —

(1) For alloys and tempers not listed, contact Gulfstream Technical Operations.

Table 10: Electrical Conductivity Requirements for Wrought Aluminum Alloys

ALLOY AND TEMPERCONDUCTIVITY VALUES

Typical (% IACS) Range (% IACS)

1100 - All 59 57.0 - 61.8

3003-0 50 44.7 - 50.0

-H12, H14, H16, H18 41 37.8 - 51.8

2014-0 50 48.6 - 51.0

-T3, T4 34 32.5 - 35.0

-T6 40 35.0 - 41.5

2024 / 2124-0 50 46.0 - 50.0

-T3XX 30 28.6 - 35.0

-T4 30 27.5 - 31.0

-T36 30 29.1 - 31.0

-T6XX 38 35.0 - 39.0

-T81 38 35.5 - 40.0

-T851 (Up To 3.999) 39 37.0 - 42.5

-T851 (4 Inches and Up) 39 37.0 - 41.5

2219 - 0 44 40 - 46 (1)

-T31, T35, T37 28 26 - 34 (1)

-T6, T62, T81, T87 30 28 - 35 (1)

5052 (All) 35 33.6 - 37.6

6061-0 52 42.0 - 52.0

-T4 41 35.0 - 44.0

-T6 45 41.0 - 52.0

6063-T5 55 50.0 - 60.0


51-20-00February 29/04

ALLOY AND TEMPERCONDUCTIVITY VALUES

Typical (% IACS) Range (% IACS)

-T6 53 50.0 - 60.0

7075-0 — 44.5 - 47.8

-W — 28.5 - 30.5

-T6, T651 33 30.0 - 33.5

-T73XXX 40 38.0 - 41.0

7079-T6 32 30.0 - 35.0

7175-T736 40 38.0 min

7178-T6 31 26.8 - 32.6

-T76, T765XX 38 36.5 min

7050-T73XXX 40 40.0 min

-T7651 39 39.0 min

7049-T73XX 40 38.0 min

(1) Range additions to be made to the specification, derived from MDAC specifications and QQ-A-250/30.

Table 11: Hardness Requirements for Aluminum and Magnesium Alloy Castings

ALUMINUM AND MAGNESIUM ALLOY CASTINGS (1)

Alloy And Temper Rockwell Hardness Minimum

Aluminum Alloys E Scale

43FSand 30

Permanent mold 33

195-T4Sand 73

Permanent mold 77

195-T6Sand 77

Permanent mold 88

220-T4 Sand 77

355-T6Sand 80

Permanent mold 88

356-T6Sand 73

Permanent mold 80

142-T571 Sand 85

142-T77 Sand 78

142-T571 Permanent mold 95

142-T61 Permanent mold 97

122-T61 Sand 100


51-20-00

February 29/04

ALUMINUM AND MAGNESIUM ALLOY CASTINGS (1)

Alloy And Temper Rockwell Hardness Minimum

108F Sand 56

113F Sand 73

40E-T5 Sand 77

319-F Sand 73

A356-T6Sand 72

Permanent mold 80

A380 Die casting 82

380 Die casting 81

218 Die casting 80

85 Die casting 78

85X Die casting 75

A360 Die casting 78

360 Die casting 78

Magnesium Alloys E Scale

A10-HAT 72

ZK60A-EA (T5) 84

AZ63-HTA 70

AZ91-HTA 67

AZ80A-F 80

AN-M-36-HTA 72

(1) For alloys and tempers not listed, contact Gulfstream Technical Operations.

Table 12: Precipitation Hardened, Corrosion and Heat Resistant Alloys


410

QQ-S-763 Forgings Annealed B93 max 202 max

QQ-S-766 Sheet (strip) plateAnnealed B94 max

Cold work B88 min

416 QQ-S-764 Forgings Annealed B93 max 202 max

431 QQ-S-704 Forgings Annealed C29 max 277 max

440C QQ-S-763 Bar (rod)Hot finished B87 max 269 max

Cold finished 285 max


51-20-00February 29/04


A286

AMS 5737 Bar (rod)Forgings (tubing)

Solution H.T. — — —

STA-1325 age C30 30N45 - 55 248 - 341

AMS 5525 Sheet (plate)Solution H.T. B90 max

STA-1325 age C30 min 30N45 - 55 248 - 341

AM350MIL-S-8840

AllSCT-850 C40 - 47 15N80 - 83.5

AMS-5547 SCT-1050 C36 - 42 15N78 - 81

PH13-8MO AMS 5629 Bar (rod) forgings

Solution 363 max

H950 C45 - 48

H1000 C43 - 47

PH14-8MO AMS 5603 All

CH900 C50 min 15N85 min

SRH950 C46 - 51 15N83 - 85.5

SRH1050 C40 - 46 15N80 - 83

PH15-7MO AMS 5520 Sheet (strip) plate

Annealed B100 max

H900 C40 - 47 30N59.5 - 65.8

TH1050 C41 - 46

TH1100 C42 - 47

15-5PH AMS5659 Forgings

Solution 363 max

H900 C40 - 45 388 - 438

H1025 C35 - 39

17-7PH

AMS 5673 Wire Spring temper — — —

MIL-S-25043 Sheet (strip) plateBar (rod)

Annealed B92 max

TH1050 C39 - 44

TH1100 C34 - 40

AMS Wire CH900 C46 min 15N83 min

17-4PH AMS 5643 Bar (rod)Forgings

Solution annealed C39 max 363 max

H900 C41 - 46 375 - 462

H925 C38 - 45

H1025 C35 - 41

H1075 C32 - 37


51-20-00

February 29/04


Inconel 600

QQ-W-390 WireRegular temper 15N70 min

Spring temper 15N75 min

MIL-N-6710 Bar (rod)

Annealed B86 max 30T74 max 120 - 170

Cold drawn B90 max 30T75.5 max 180 - 290

Hot rolled B62 min 30T58 min 110 min

MIL-N-6840 Forging Hot finishedannealed 140 - 210

MIL-N-6840 Sheet strip (plate)Annealed B80 max 30T70 max 150 max

Spring temper B65 - 68

MIL-T-7840 Tubing Cold annealed B65 - 88 120 - 180

Inconel 625AMS 5666 Bar (rod) Annealed B95 min

AMS 5599 Sheet Annealed B95 min

Inconel 718MMS 163 Bar (rod) forgings Annealed, aged C39 min 30N58.6 min

MMS 164 Sheet(strip) plate Solution, aged C36 min

Inconel X750

AMS 5667 Bar (rod) forgings

Annealed B100 max

Aged 30N52 max 302 - 363

Stress equal. C32 max 302 max

MIL-N-7786 Sheet (strip)

Annealed B100 max

Aged C32 - 42 300 min

Solution C30 min

Monel 400

QQ-N-281

Bar (rod) Cold drawn C26 min 30N46 min 260 min

Sheet (strip) plate

Annealed B90

Hard stressrelieved B93 max

MIL-T-1368 Tubing

Annealed B90 max

Hard stressrelieved B96 min

Monel K500

All Annealed (aged) C24 min

Bar, forging Aged C27 min

Tubing Aged C30 min

Sheet1/2 hard (aged) C30 min

Full hard (aged) C34 min


51-20-00February 29/04


Rene’ 41 AMS 5712

Bar Solution 363 max

Sheet

Annealed -0.040 C35 min 15N754 max

Annealed -0.040to 0.070 A64 max

Annealed -0.070to 0.187 C30 max

Aged C35 min 30N55 min

Table 13: Hardness Requirements for Copper Alloy

ALLOY COND FORMROCKWELL HARDNESS SCALE

A B C E 15N 15T 30T

Copper Annealed

Sheet -0.019 — — — — — 68 max —

0.020 andover — — — 65 max — — —

Copper Annealed Bar — — — 50 max — — —

Beryllium -Copper Cond A Bar Over

0.124 — — 45 - 85 — — — —

Beryllium -Copper Cond H

Bar 0.125 -0.375 — 92 - 103 — — — — —

0.376 -1.000 — 91 - 102 — — — — —

Over 1.000 — 88 - 101 — — — — —

Beryllium -Copper Cond AT Bar Over

0.124 — — 34 - 40 — — — —

Beryllium -Copper Cond HT

Bar 0.124 -0.375 — — 39 - 45 — — — —

0.376 -1.000 — — 38 - 44 — — — —

Over 1.000 — — 37 - 43 — — — —

Beryllium -Copper Cond A

Sheet0.010 -0.030

— — — — — 78 - 86 —

0.031 -0.050 — — — — — — 46 - 69

0.051 -0.075 — — — 82 - 101 — — —

Over 0.075 — 45 - 79 — — — — —

Beryllium -Copper

Cond 1/4Hard

Sheet0.010 -0.031

— — — — — — 66 - 75

Over 0.031 — 74 - 90 — — — — —


51-20-00

February 29/04

ALLOY COND FORMROCKWELL HARDNESS SCALE

A B C E 15N 15T 30T

Beryllium -Copper

Cond 1/2Hard

Sheet0.010 -0.020

— — — — — 88.5 - 91.5 —

0.021 -0.045 — — — — —

Over 0.045 — 89 - 96 — — — — —

Beryllium -Copper Cond H

Sheet0.010 -0.031

— — — — — — 80 - 83

Over 0.031 — 96 - 102 — — — — —

Beryllium -Copper Cond AT

Sheet0.010 -0.020

— — — — 77 min — —

0.021 -0.065 67 min — — — — — —

Over 0.065 — — 34 min — — —

Beryllium -Copper

Cond 1/4HT

Sheet0.010 -0.019

— — — — 78 min — —

0.020 -0.049 68 min — — — — — —

Over 0.049 — 36 min — — — —

Beryllium -Copper

Cond 1/2HT

Sheet0.010 -0.020

— — — — 80 min — —

0.021 -0.060 69 min — — — — — —

Over 0.060 — 38 min — — — —

Beryllium -Copper Cond HT

Sheet0.010 -0.019

— — — — 80 min — —

0.020 -0.049 70 min — — — — — —

Over 0.049 — — 39 min — — — —


51-20-00February 29/04

Table 14: Titanium Alloys

ALLOY FORM SPEC COND ROCKWELLHARDNESS

Unalloyed

Sheet and plate MIL-T-9046 T.I. C.C.

Annealed

B90 max

AMS4901, MIL-T-9046,T-1, C-B B100 max

Bar and rod AMS4921, MIL-T-9047,T-1, C-A B100 max

Forgings MIL-T-9047. C-1, MIL-F-83142, T-1 B100 max

T-1 5A1 - 2.5SN

Sheet and plate MIL-T-9046, T-11, C-A

Annealed

C36 max

Bar and rod AMS4926, MIL-T-9047,TII, CA —

Forgings AMS4966, MIL-T-9047,C-2, MIL-F-83142, T-2 —

T1-6A1-4V

Sheet and plate AMS4911, MIL-T-9046,T-III, C-C

Annealed

C36 max

Bar and rod AMS4928, MIL-T-9047,C-6 C39 max

Forgings AMS4928, MIL-T-9047,C-6, MIL-F-83142, T-3 C39 max

Extrusions AMS4935 C36 max

T1-6A1-6V-2SN

Sheet and plate MIL-T-9045, T-III, C-E

Annealed

C38 max

Bar and rod forgings MIL-T-9047, T-III, C-C,MIL-F-83142, T-3, C-8 C38 max

T1-8MN Sheet and plate MIL-T-9046, T-III, C-A Annealed C32 max

T1-8A1-1MO-IV Sheet and plate MMS-129, MIL-T-9046,T-II, C-F Annealed C38 max

NOTE: Hardness values do not provide a basis for verifying conformance to mechanical propertiesin applicable specifications or rejecting parts. Hardness values in excess of those indicatedmay be used to screen parts for material in STA condition or presence of alpha case.

The effect of heat on Titanium cannot be evaluated properly by hardness tests to evaluatethe properties of Titanium accurately, a metallurgical examination must be made. However,Titanium surfaces oxidize and change color with increasing heat and scale at hightemperatures. This characteristic can be used to assess the intensity of the heat imposedon the Titanium structure. Gulfstream Technical Operations review and approval required.


51-20-00

February 29/04

Portable Hardness Tester - Barcol and ErnstFigure 1


51-20-00February 29/04

Portable Hardness Tester - RiehleFigure 2


51-20-00

February 29/04

3. Original Finishes

Table 15: GIV Original Finishes

PART NAME PART SUBSTRATE

FINISHSUPPLEMENTAL

EXTERIOR FINISHINTERIOR(1)

EXTERIOR(2)

Fuselage

Radome Glass / EpoxyNomex Core None 92

95 (Ref AV-1159-TS360.0)(3)

Skins Aluminum 2012213 213 None

Gear well Aluminum88

2132012

2013 None

Aluminum bulkhead Aluminum 2012213 None 2012 as required by drwing

Flat pressure bulkhead Graphite / Epoxy None None None

Tail compartment Aluminum (only) 20122013 N/A N/A

Floor Panels

Forward floor panelsMetal bondedassembly

Aluminum N/A 2012 None

Composite Graphite / Epoxy N/A 2012 92

Aft floor panelsMetal bondedassembly

Aluminum N/A 2012 None

Composite Graphite / Epoxy N/A 2012 92

Wing Body Fairings

Forward fairings Graphite / Epoxy None None 92

Aft fairings Graphite / Epoxy None None 92

Skid plate (Skeg) Glass / Epoxy None 2012 None

Engine Cowling

Pylon fairing Graphite / Epoxy None None 92

Fixed cowl Graphite / Epoxy 2012 2012 92

Nose cowl Aluminum 2132012 Polished None

Aft cowl Aluminum 2132012

2132012 None

Cowl door - upper Graphite / Epoxy 2012 2012 92

Cowl door - lower Graphite / Epoxy 2012 2012 92

Wings

Leading Edge (LE) Aluminum None Polished None


51-20-00February 29/04


FINISHSUPPLEMENTAL


EXTERIOR(2)

Upper planks Aluminum 88144

8820124012

None

Lower planks Aluminum 88144

8820124012

None

Center box Aluminum 88144

8820124012

None

Front beam Aluminum 88144

8820124012

None

Rear beam Aluminum 88144

8820124012

None

Integral tank Aluminum 88144

8820124012

None

Gear wells Aluminum

88 / 213 /2012

or4012 /2013

None

Trailing Edge (TE) Box- inboardMetal BondedAssembly

Aluminum 2132012

2132012 None

Composite Graphite / Epoxy None None 92(3)

TE Box - Outboard Graphite / Epoxy None None 92(3)

Lighting

Nav / strobe assembly Aluminum

88 / 213 /2012

or4012 /2013

88 / 213 /2012

or4012 / 2013

None

Landing light Aluminum

88 / 213 /2012

or4012 /2013

88 / 213 /2012

or4012 / 2013

None

Winglets

Main assembly Aluminum N/A 213(5) None

Winglet - LE Aluminum N/A Polished None

Aileron

Bonded metalassembly aluminum Aluminum N/A 213(5) None


51-20-00

February 29/04


FINISHSUPPLEMENTAL


EXTERIOR(2)

Graphite / epoxycomposite assembly Graphite / Epoxy N/A 92(5) (3)

Spoilers

Upper surfacebonded metalassembly

Aluminum N/A 213(5) None

Graphite / epoxycomposite assembly Graphite / Epoxy (4) N/A 92(5) (3)

Lower surfacebonded metalassembly

Aluminum N/A 213(5) None

Graphite / epoxycomposite assembly Graphite / Epoxy (4) N/A 92(5) (3)

Flaps

Metal assembly Aluminum 2132012 213(5) None

Graphite / epoxycomposite assembly Graphite / Epoxy (4) N/A N/A (3)

Empennage

Vertical fin Aluminum 2132012 213(5) None

Vertical fin LE Aluminum 2132012 Polished None

High Frequency (HF)antenna

Glass Epoxy w /Nomex Core None (5) None

Rudder Graphite / Epoxy N/A 92(5) (3)

Horizontal stabilizer Aluminum 2132012 213(5) None

Horizontal stabilizer LE Aluminum 2132012 Polished None

Horizontal stabilizerOH panelbonded metalassembly

Aluminum21320122013

213(5) None

Horizontal stabilizerOH panel Graphite / Epoxy (4) N/A N/A(5) None

Elevators Aluminum 2132012 213(5) None

Bullet assembly Glass / Epoxy None None (3)

Miscellaneous

Interior surfaces Ferrous alloy 2 N/A None


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FINISHSUPPLEMENTAL


EXTERIOR(2)

Exterior surfaces Ferrous alloy N/A2

20122013

None

Elastomeric surfaces Noted None N/A None

Flight control ballast Tungsten None2

20122013

None

(1) All entries noting 2012 or 4012 primer are replaced by 2012, 4012 or 3012.(2) All entries noting 2013 are replaced by 2013 or 3013.(3) Environmental Protective Finish (EPF) for protection against ultra violet light, acid rain and bird damage.(4) Indicates graphite fiber with epoxy resin matrix.(5) 2012 and / or GAMPS 4000 Pratt & Lambert primer (usually). Topcoat (GAMPS 4000 Pratt & Lambert or

operator specified material.

NOTE: The following GAC codes pertain to Table 15.

• 2 - GAC code for Low Embrittlement Cadmium Plating per QQ-P-416 Type II, Class• 88 - GAC code for Anodize - Chromic Acid per MIL-A-8625, Type I, Class 1• 144 - GAC code for Corrosion Preventive Coating - Integral Fuel Tanks per MIL-C-27725• 213 - GAC code for Chromate Conversion Coating per MIL-C-5541, Class 3• 2012 - GAC code for Epoxy Primer - Skydrol Resistant, green - DeSoto 515X333 / 910X350• 2013 - GAC code for Epoxy, Fuel / Skydrol Resistant Topcoat, gloss white - DeSoto 521X315 / 190-

037 / 020-004• 4012 - GAC code for Epoxy Primer (Chlorinated Solvent), Skydrol Resistant (DeSoto 515X383 /

910X749 / 010 / 313) - Product Discontinued as of 1994• 3012 - GAC code for Epoxy Primer, Water Reducible, Low VOC, Di-phosphate Ester Hydraulic Fluid

Resistant• 3013 - GAC code for Epoxy Topcoat, High Solids, Di-phosphate Ester Hydraulic Fluid Resistant


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STRUCTURAL REPAIR MANUAL PROCESSES — GENERAL · 2. Finishes, Processes and Nondestructive Test...

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