SAE AMS2770M
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Heat Treatment of Wrought Aluminum Alloy Parts
Superseded date
11-04-2019
Superseded by
Published date
26-05-2015
Publisher
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
Describes the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts.
| DocumentType |
Standard
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| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy |
This specification specifies the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts (See 8.8.1). It also covers heat treatment by warehouses or distributors converting raw material from one temper to another temper (See 1.3 and 8.5). It covers the following aluminum alloys:1100, 2004, 2014, 2017, 2024, 2098, 2117, 2124, 2219, 2224, 3003, 5052, 6013, 6061, 6063, 6066, 6951, 7049, 7050, 7075, 7149, 7178, 7249, 7475
| SAE AMS4028H | Aluminum Alloy Sheet and Plate 4.4Cu - 0.85Si - 0.80Mn - 0.50Mg (2014-O) Annealed |
| SAE AMS4295D | Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr (2219 - O, F, T31, T351, T37, T81, T851, T87) |
| MS27229 Revision C:2015 | FLANGE NIPPLE ASSEMBLY 45 DEGREES, ADAPTER, HOSE TO TUBE, REUSABLE, HYDRAULIC, FUEL AND OIL LINES |
| BS ISO 7169:2014 | Aerospace. Separable tube fittings for fluid systems, for 24° cones, for pressures up to 3 000 psi or 21 000 kPa. Procurement specification, inch/metric |
| MS27225 Revision C:2007 | Nipple Assembly 45 Degrees, Adapter, Hose to Tube, Reusable, Hydraulic, Fuel and Oil Lines |
| MIL-DTL-8878 Revision L:2014 | TURNBUCKLES, POSITIVE SAFETYING, GENERAL SPECIFICATION FOR |
| SAE AMS4321B | Aluminum Alloy Forgings 7.7Zn - 2.5Mg - 1.5Cu - 0.16Cr (7049-01) High Temperature Annealed |
| MS27227 Revision C:2015 | FLANGE NIPPLE ASSEMBLY 90 DEGREES, ADAPTER, HOSE TO TUBE, REUSABLE, HYDRAULIC, FUEL AND OIL LINES |
| SAE AMS4601A | Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr Solution Heat Treated, Cold Worked and Naturally Aged (2219 -T31/-T351) |
| MIL-HDBK-1587 Base Document:1996 | MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| SAE AMS4021H | Aluminum Alloy, Alclad Sheet and Plate, 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (Alclad 6061-0) Annealed |
| SAE AS4444 | Fittings, 24° Cone Flareless, Fluid Connection, 5000 psi |
| SAE AS4875A | Fittings, Straight Threaded Boss or Flanged, Fluid Connection |
| MIL-STD-1587 Revision D:2017 | MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
| MIL-DTL-85052-9 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 550 DEGREES F, POLY-TETRAFLUOROETHYLENE (PTFE) |
| SAE ARP5812 | Actuators, Linear Mechanical, General Specification Guide |
| MIL-DTL-85052-5 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 275 DEGREES F, ETHYLENE PROPYLENE |
| MIL-DTL-85110 Revision B:1997 | BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
| SAE AMSH6088C | Heat Treatment of Aluminum Alloys |
| SAE AMS4146G | Aluminum Alloy Forgings and Rolled or Forged Rings 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061 - T4) Solution Heat Treated and Naturally Aged |
| MIL-HDBK-115 Revision C:2016 | U.S. ARMY REVERSE ENGINEERING HANDBOOK (GUIDELINES AND PROCEDURES) |
| MIL-STD-186 Revision F:2002 | PROTECTIVE FINISHING SYSTEMS FOR ROCKETS, GUIDED MISSILES, SUPPORT EQUIPMENT AND RELATED MATERIALS |
| SAE AS7222A | Aluminum Rivets, UNS A92117 2.5Cu - 0.3Mg (2117-T4) Procurement Specification |
| MIL-DTL-85052-10 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 275 DEGREES F, NITRILE BUTADIENE RUBBER FUEL AND PETROLEUM BASED HYDRAULIC FLUID RESISTANT |
| SAE AMS2772G | Heat Treatment of Aluminum Alloy Raw Materials |
| MIL-DTL-85052-6 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 400 DEGREES F, FLUOROSILICONE |
| SAE AS4841B | Fittings, 37° Internal Flare, Fluid Connection, Procurement Specification |
| MIL-DTL-83798 Revision D:2008 | FITTING, RUBBER HOSE, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| SAE AMS4051G | Aluminum Alloy, Sheet and Plate, Alclad, 6.8Zn - 2.8Mg - 2.0Cu - 0.23Cr (Alclad 7178-O), Annealed |
| MIL-DTL-85052-8 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 500 DEGREES F, SILICONE RUBBER, FABRIC REINFORCED |
| SAE AS4842A | Fittings and Bosses, Pipe Threaded, Fluid Connection |
| SAE AS18280F | Fittings, 24° Cone Flareless, Fluid Connection, 3000 psi |
| NASA MSFC SPEC 3679 : 2012 | PROCESS SPECIFICATION - WELDING AEROSPACE HARDWARE |
| NASA MSFC SPEC 3635 : 2012 | PYROTECHNIC SYSTEM SPECIFICATION |
| NASA STD 6016(INT) : 2006 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA STD 5005(INT) : 2007 | THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
| NASA KSC DE 512-SM : 2012 | FACILITY SYSTEMS, GROUND SUPPORT SYSTEMS, AND GROUND SUPPORT EQUIPMENT GENERAL DESIGN REQUIREMENTS |
| NASA STD 5005 : 2013 | STANDARD FOR THE DESIGN AND FABRICATION OF GROUND SUPPORT EQUIPMENT |
| NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
| NASA STD 5006 : 2015 | GENERAL FUSION WELDING REQUIREMENTS FOR AEROSPACE MATERIALS |
| NASA JSC 27301 : 2009 | MATERIALS AND PROCESSES SELECTION, CONTROL, AND IMPLEMENTATION PLAN FOR JSC FLIGHT HARDWARE |
| ASTM B 483/B483M : 2013 | Standard Specification for Aluminum and Aluminum-Alloy Drawn Pipe for General Purpose Applications |
| NASA PRC 2002 : 2011 | PROCESS SPECIFICATION FOR THE HEAT TREATMENT OF ALUMINUM ALLOYS |
| MIL-H-6088 Revision G:1991 | HEAT TREATMENT OF ALUMINIUM ALLOYS |
| SAE AMS3025E | Polyalkylene Glycol Heat Treat Quenchant |
| ISO 7169:2014 | Aerospace Separable tube fittings for fluid systems, for 24 degree cones, for pressures up to 3 000 psi or 21 000 kPa Procurement specification, inch/metric |
| 09/30204364 DC : 0 | BS EN 6104 - AEROSPACE SERIES - RIVETS, SOLID, IN ALUMINIUM OR ALUMINIUM ALLOY - INCH SERIES - TECHNICAL SPECIFICATION |
| SAE AMS4080P | Aluminum Alloy, Drawn Seamless Tubing 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-O) Annealed |
| SAE AS4843A | Fittings, Beaded, Fluid Connection |
| ASTM B 483/B483M : 2013 : EDT 1 | Standard Specification for Aluminum and Aluminum-Alloy Drawn Tube and Drawn Pipe for General Purpose Applications |
| MS27223 Revision C:2007 | Nipple Assembly 90 Degrees, Adapter, Hose to Tube, Reusable, Hydraulic, Fuel and Oil Lines 1/4 Inch through 2 Inch Tube Sizes |
| MIL-DTL-85052-7 Revision A:2016 | CLAMP, LOOP, ALUMINUM 2024-T42, 212 DEGREES F, CHLOROPRENE |
| MIL-STD-40002 Base Document:1991 | HEAT TREATMENT CODING SYSTEM, GENERAL |
| SAE AMS2767 | Uphill Quenching of Aluminum Alloy Product |
| 10/30233643 DC : 0 | BS EN 6104 - AEROSPACE SERIES - RIVETS, SOLID, IN ALUMINIUM OR ALUMINIUM ALLOY - INCH SERIES - TECHNICAL SPECIFICATION |
| SAE AMS3025D | Polyalkylene Glycol Heat Treat Quenchant |
| SAE AMS2750E | Pyrometry |
| SAE AMS2772G | Heat Treatment of Aluminum Alloy Raw Materials |
| SAE AMS2658D | Hardness and Conductivity Inspection of Wrought Aluminum Alloy Parts |
| SAE ARP 1962 : 1995 | TRAINING AND APPROVAL OF HEAT-TREATING PERSONNEL |
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