MIL-H-6088 Revision G:1991
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
Heat Treatment of Aluminum Alloys (S/S by SAE-AMS-H-6088)
Available format(s)
PDF
Published date
01-04-1991
Publisher
Superseded date
26-09-1997
€16.67
Excluding VAT
Covers all aspects of heat treatment of aluminum alloy products by material producers, including raw forgings and castings. Coverage includes applicable documents, process establishment, periodic process surveys, periodic product monitoring, heat treatment of parts, furnaces, air chamber furnaces, salt baths, pyrometric equipment, continuous furnaces, quench baths, circulation, spray quenching equipment, and rinsing equipment.
| DevelopmentNote |
MIL-H-6088 G NOTICE 1 - NOTICE OF CANCELLATION Future heat treatment should refer to SAE-AMS-H-6088
|
| DocumentType |
Standard
|
| Pages |
73
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
This specification covers the requirements and recommendations for the heat treatment of aluminum alloy rolled, extruded, forged, drawn, and cast product (see 6.1 and 6.5.1). It does not cover the requirements for the heat treatment of aluminum alloy parts (see 3.4).
| MIL-STD-2156 Base Document:1983 | Launcher, Rail, Guided Missile, Aircraft, General Design Criteria for |
| SAE AS8662 | Knife, Hunting, Sheathed, Survival, Pilot’s |
| SAE AS4060 | Tube Fitting Swaged Joint, Roller Expander Manual Process, Requirements for |
| FF-R-556 Revision D:1981 | Rivet, Solid, Small; Rivet, Split, Small; Rivet, Tubular, Small Flat Washer (Burr); and Cap, Rivet, General Purpose |
| MIL-A-83577 Revision B:1988 | Assemblies, Moving Mechanical, for Space and Launch Vehicles, General Specification for (No S/S Document) |
| DIN 65570:1990-12 | AEROSPACE; HEAT TREATMENT FACILITIES; GENERAL REQUIREMENTS |
| SAE AMS4240G | Castings, Sand, 10Mg, Solution Heat Treated and Naturally Aged |
| SAE MAM4131B | Aluminum Alloy, Die and Hand Forgings 5.6zn 2.5mg 1.6cu 0.23cr Solution Heat Treated and Aged |
| MIL-F-71131 Base Document:1992 | Fin, Mortar Cartridge: M32 |
| BS EN ISO 11846:2008 | Corrosion of metals and alloys. Determination of resistance to intergranular corrosion of solution heat- treatable aluminium alloys |
| QQ-A-200 Revision E:1980 | Aluminum Alloy, Bar, Rod, Shapes, Structural Shapes, Tube and Wire, Extruded; General Specification for (Refer to ASTM-B241/B241M, ASTM-B221, ASTM-B308/B308M and SAE-AMS-QQ-A-200) |
| MIL-A-22771 Revision D:1984 | Aluminum Alloy Forgings, Heat Treated (S/S by SAE-AMS-A-22771) |
| MIL-F-48076 Revision A:1984 | Fin, Assembly, M158 |
| QQ-A-225 Revision G:1990 | ALUMINUM AND ALUMINUM ALLOY BAR, ROD, WIRE, OR SPECIAL SHAPES; ROLLED, DRAWN, OR COLD FINISHED; GENERAL SPECIFICATION FOR (S/S BY ASTM-B211 AND SAE-AMS-QQ-A-225) |
| ASTM G 110 : 1992 : R2009 | Standard Practice for Evaluating Intergranular Corrosion Resistance of Heat Treatable Aluminum Alloys by Immersion in Sodium Chloride + Hydrogen Peroxide Solution |
| MIL A 46192 : B | ALUMINUM ALLOY ARMOR ROLLED PLATE (1/2 TO 4 INCHES THICK), WELDABLE (ALLOY 2519) |
| FF-B-584 Revision F:1989 | Bolts, Square Neck and Tee Head (S/Sby ASME-B18.5, ASME-B18.9,and ASME-B18.18.1M) |
| MIL-STD-1892 Base Document:1985 | WELDING, ARC AND OXYFUEL GAS, PROCESS AND REQUIREMENTS FOR (NO S/S DOCUMENT) |
| MIL-C-8603 Revision B:1984 | Clamps, Loop Type, and Straps, Support |
| MIL T 8878 : D | TURNBUCKLE, POSITIVE SAFETYING |
| MIL R 007885 : C SUPP 1 | RIVETS; BLIND, STRUCTURAL, LOCKED AND FRICTION RETAINED SPINDLE, GENERAL SPECIFICATION FOR |
| DOD-E-83578 Revision A:1987 | EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) (NO S/S DOCUMENT) |
| MIL-C-7438 Revision G:1985 | Core Material, Aluminum, for Sandwich Construction (See Notice 1 for Replacement Information) |
| SAE AMSWWT700B | Tube, Aluminum and Aluminum Alloy, Drawn, Seamless, General Specification for |
| SAE AMS4318A | Aluminum Alloy, Rolled or Cold Finished Bars and Rods, 12.2Si - 1.0Mg - 0.90Cu - 0.90Ni (4032-T86) Solution Heat Treated, Cold Worked, and Artificially Aged |
| MIL-A-23121 Revision C:1970 | Aircrew Environmental, Escape and Survival Cockpit Capsule System General Specification for (No S/S Document) |
| MIL-HDBK-1587 Base Document:1996 | Materials and Process Requirements for Air Force Weapons Systems (S/S by MIL-STD-1587) |
| MIL-A-81973 Base Document:1974 | Aircrew Automated Escape Systems, Test Vehicles for Ground Track Performance Testing, Rocket and/or Jet Engine Propelled, General Specification for (No S/S Document) |
| MIL-S-7839 Revision B:1973 | SCREW, STRUCTURAL, AIRCRAFT (S/S BY NASM7839) |
| MIL-A-21180 Revision D:1984 | Aluminum-Alloy Castings, High Strength (S/S by SAE-AMS-A-21180) |
| MIL-R-27384 Revision B:1970 | RIVET, BLIND, DRIVE TYPE (S/S BY NASM27384) |
| MIL-R-5674 Revision F:1994 | Rivets, Structural, Aluminum Alloy, Titanium Columbium Alloy, General Specification for (S/S by NASM5674) |
| MIL-R-85880 Base Document:1988 | ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| I.S. EN 14101:2002 | SPACE PRODUCT ASSURANCE - MATERIAL SELECTION FOR CONTROLLING STRESS-CORROSION CRACKING |
| SAE AS4444 | Fittings, 24° Cone Flareless, Fluid Connection, 5000 psi |
| MIL-H-9890 Revision E:1988 | Hardware, Individual Load Carrying Equipment: and Hardware, Miscellaneous |
| MIL-W-22248 Revision A:1971 | Weldments, Aluminum and Aluminum Alloy |
| MIL F 70546 : 0 | FIN ASSEMBLIES, MORTAR CARTRIDGE, 81MM, M28, M29 |
| SAE AMS4148F | Aluminum Alloy Die Forgings (7175-T66) Solution and Precipitation Heat Treated |
| MIL-F-71153 Base Document:1993 | Fin, Mortar, Cartridge: M33 |
| QQ-A-596 Revision E:1981 | Aluminum Alloy Permanent and Semipermanent Mold Castings (S/S by ASTM-B108) |
| MIL-S-8512 Revision D:1974 | Support Equipment, Aeronautical, Special, General Specification for the Design of |
| MIL-F-80188 Revision B:1985 | Furnace, Heat Treating, Electric, Metal Lined, Box Design (No S/S Document) |
| MIL-STD-2131 Revision A:1991 | Launcher, Ejection, Guided Missile, Aircraft, General Design Criteria for |
| MIL R 46963 : A | ROCKET MOTOR, M42A1, BOOSTER |
| MIL-F-14888 Revision A:1981 | Fin Assembly, XM170 (No S/S Document) |
| PREN 6071 : 200P1 | AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PLATE |
| SAE ARP1675 | Structural Weldbonding of Aluminum Structures |
| QQ-A-200-16 Revision A:1974 | ALUMINUM ALLOY STRUCTURAL SHAPES, EXTRUDED, 6061 (REFER TO SAE-AMS-QQ-A-200/16 AND ASTM-B308/B308M) |
| MIL-W-8604 Revision A:1982 | WELDING, FUSION; ALUMINUM ALLOYS; PROCESS AND PERFORMANCE OF (S/S BY MIL-STD-2219) |
| MIL-K-8662 Revision E:1974 | Knife, Hunting, Sheathed, Survival, Pilot\'s (S/S by SAE-AS8662) |
| SAE MAM4247B | Aluminum Alloy, Hand Forgings 7.7zn 2.4mg 1.6cu 0.16cr (7049-T7352) Solution Heat Treated, Stress Relieved By Compression, and Precipitation Heat Treated |
| MIL-S-85510 Base Document:1981 | Seats, Helicopter Cabin, Crashworthy, General Specification for |
| MIL A 46118 : D | ALUMINUM ALLOY ARMOR, 2219, ROLLED PLATE AND DIE FORGED SHAPES |
| SAE AMS2772G | Heat Treatment of Aluminum Alloy Raw Materials |
| MIL-F-85731 Base Document:1986 | Fastener, Positive Locking, Electronic Equipment General Specificationfor |
| BS ISO 11846 : 1995 | CORROSION OF METALS AND ALLOYS - DETERMINATION OF RESISTANCE TO INTERGRANULAR CORROSION OF SOLUTION HEAT-TREATABLE ALUMINIUM ALLOYS |
| MIL-T-7081 Revision D:1965 | TUBE, ALUMINUM ALLOY, SEAMLESS, ROUND, DRAWN 6061, AIRCRAFT HYDRAULIC QUAL ITY (S/S BY SAE-AMS-T-7081) |
| MIL-Q-22631 Revision B:1964 | Quality Control of Metal Wrought Products Except Forgings Procured to Non-Governmental Specification (No S/S Document) |
| MIL-F-5509 Revision D:1978 | Fitting, Flared Tube, Fluid Connection (see Notice 2 for Additional Superseding Information) |
| NASA MSFC SPEC 504 : 1990 | WELDING, ALUMINIUM ALLOYS |
| MIL S 25073 : 0 | |
| SAE AMS4051G | Aluminum Alloy, Sheet and Plate, Alclad, 6.8Zn - 2.8Mg - 2.0Cu - 0.23Cr (Alclad 7178-O), Annealed |
| MIL P 25995 : B | PIPE, ALUMINUM ALLOY, DRAWN OR EXTRUDED |
| MIL F 71037 : NOTICE 2 | FIN ASSEMBLY, MORTAR CARTRIDGE |
| FF-N-836 Revision E:1994 | Nut: Square, Hexagon, Cap, Slotted, Castle, Knurled, Welding and Single Ball Seat |
| SAE MA2150 | Clamps, Loop or P Style, Single Point Mount, Multiple Shapes, Metric |
| SAE AMS4023F | Aluminum Alloy Sheet and Plate, Alclad 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (Alclad 6061; -T6 Sheet, -T651 Plate) |
| SAE MAM4323B | Aluminum Alloy, Hand Forgings, 5.6zn 2.5mg 1.6cu 0.23cr, Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated |
| I.S. EN ISO 11846:2008 | CORROSION OF METALS AND ALLOYS - DETERMINATION OF RESISTANCE TO INTERGRANULAR CORROSION OF SOLUTION HEAT-TREATABLE ALUMINIUM ALLOYS |
| ISO 11846:1995 | Corrosion of metals and alloys — Determination of resistance to intergranular corrosion of solution heat-treatable aluminium alloys |
| EN 14101:2001 | Space product assurance - Material selection for controlling stress-corrosion cracking |
| DIN 50900-3:1985-09 | CORROSION OF METALS; TERMS; TERMS OF CORROSION TESTING |
| DOD C 63976 : 0 | CASE, CARTRIDGE, 30MM, AMMUNITION FOR M788 M789 AND M799 SERIES OF 30 MM, AMMUNITION |
| MIL-F-18280 Revision F:1995 | Fittings, Flareless Tube, Fluid Connection (S/S by SAE-AS18280) |
| MIL-B-543 Revision G:1990 | Buckles, Tongueless and Web Strap |
| MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL S 9479 : C | |
| MIL-F-13926 Revision B:1984 | Fire Control Materiel, Manufacture and Inspection, General Specification for |
| MIL-C-8956 Revision A:1970 | Clamps, Loop, Tube Support (For Future Req. use MIL-C-8603 and MIL-C-85052 |
| QQ-A-200-8 Revision F:1983 | Aluminum Alloy 6061, Bar, Rod, Shapes, Tube and Wire, Extruded (Refer to ASTM-B241/B241M, ASTM-B221 and SAE-AMS-QQ-A-200/8) |
| MIL-S-81771 Revision A:1975 | Seat System; Aircrew, Crash Resistant; General Specification for |
| MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| MIL-A-63547 Base Document:1982 | Aluminum Alloy 7475, Rod (No S/S Document) |
| JSSG-2010-12 Base Document:1998 | Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
| MIL-P-63137 Revision B:1981 | Projectile, 8-Inch, HE, RA, M650 Warhead Section, Forward (No S/S Document) |
| MIL-R-7885 Revision D:1988 | Rivets, Blind, Structural, Mechanically LockedSpindleand Friction Locked Spindle, General Specification for |
| SAE AS85731B | Fastener, Positive Locking, Electronic Equipment, General Specification For |
| ASTM G 110 : 1992 : R2015 | Standard Practice for Evaluating Intergranular Corrosion Resistance of Heat Treatable Aluminum Alloys by Immersion in Sodium Chloride + Hydrogen Peroxide Solution |
| ASTM B 313M : 1988 | Specification for Aluminum and Aluminum-Alloy Round Welded Tubes (Metric) (Withdrawn 1990) |
| EN ISO 11846:2008 | Corrosion of metals and alloys - Determination of resistance to intergranular corrosion of solution heat-treatable aluminium alloys (ISO 11846:1995) |
| SAE MAM4141B | Aluminum Alloy, Die Forgings, 5.6zn 2.5mg 1.6cu 0.23cr Solution and Precipitation Heat Treated |
| MIL-I-43684 Revision B:1989 | Intrenching Tool, Hand, Folding, Lightweight (S/S by A-A-59337) |
| MIL-R-51344 Revision B:1982 | ROCKET, INCENDIARY, 66MM, TPA, 4-ROUND CLIP, M74 OR M74A1 (NO S/S DOCUMENT) |
| SAE AMS4021H | Aluminum Alloy, Alclad Sheet and Plate, 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (Alclad 6061-0) Annealed |
| MIL A 81596 : A | ALUMINUM FOIL FOR SANDWICH CONSTRUCTION |
| MIL-STD-645 Revision B:1981 | DIP BRAZING OF ALUMINUM ALLOYS |
| MIL-B-21902 Revision A:1963 | Boyd Helicopter Rescue Seat (No S/S Document) |
| NASA MSFC STD 506 : 1988 | MATERIALS AND PROCESSES CONTROL |
| QQ-A-601 Revision F:1981 | Aluminum Alloy Sand Castings (S/S by ASTM-B26/B26M) |
| SAE MA2151 | Clamp Assemblies, Saddle or Omega Style, Two Point Mount, Multiple Shapes, Metric |
| MIL-STD-40002 Base Document:1991 | HEAT TREATMENT CODING SYSTEM, GENERAL (NO S/S DOCUMENT) |
| SAE AMS4321B | Aluminum Alloy Forgings 7.7Zn - 2.5Mg - 1.5Cu - 0.16Cr (7049-01) High Temperature Annealed |
| ASTM G 110 : 1992 : R2003 : EDT 1 | Standard Practice for Evaluating Intergranular Corrosion Resistance of Heat Treatable Aluminum Alloys by Immersion in Sodium Chloride + Hydrogen Peroxide Solution |
| SAE MAM4248B | Aluminum Alloy, Hand Forgings and Rolled Rings 1.0mg 0.60si 0.28cu 0.20cr Solution Heat Treated, Stress Relieved By Compression, and Precipitation Heat Treated |
| ASTM G 110 : 1992 : R1997 | Standard Practice for Evaluating Intergranular Corrosion Resistance of Heat Treatable Aluminum Alloys by Immersion in Sodium Chloride + Hydrogen Peroxide Solution |
| ASTM B 308M : 1988 | Specification for Aluminum-Alloy 6061-T6 Standard Structural Shapes, Rolled or Extruded (Metric) (Withdrawn 1990) |
| BS EN 14101:2001 | Space product assurance. Material selection for controlling stress-corrosion cracking |
| DIN EN ISO 11846:2008-08 | CORROSION OF METALS AND ALLOYS - DETERMINATION OF RESISTANCE TO INTERGRANULAR CORROSION OF SOLUTION HEAT-TREATABLE ALUMINIUM ALLOYS |
| PREN 6052 : 200P1 | AEROSPACE SERIES - RIVETS - COLLAR - SYSTEM IN ALUMINIUM ALLOY SHEAR TYPE INCH SERIES - TECHNICAL SPECIFICATION |
| SAE AMS2770M | Heat Treatment of Wrought Aluminum Alloy Parts |
| MIL-STD-45662 Revision A:1988 | Calibration Systems Requirements (Refer to ISO-10012-1 and ANSI-Z540-1 or Comparable Standards as Alternatives to MIL-STD-45662) |
| ASTM B 557 : 2015 : REDLINE | Standard Test Methods for Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products |
| ASTM E 10 : 2017-05 | TEST METHOD FOR BRINELL HARDNESS OF METALLIC MATERIALS |
| MIL-STD-1537 Revision C:2002 | Electrical Conductivity Test for Verification of Heat Treatment of Aluminum Alloys, Eddy Current Method |
| SAE AMS2750E | Pyrometry |
| ASTM E 103 : 2017 : REDLINE | Standard Practice for Rapid Indentation Hardness Testing of Metallic Materials |
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