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SAE AMS 2770 : 2015

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 WROUGHT ALUMINUM ALLOY PARTS
Superseded date

04-11-2019

Published date

01-01-2015

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.

Committee
AMS-D
DocumentType
Standard
PublisherName
SAE International
Status
Superseded
SupersededBy

SAE AMS 4028 : 2014 ALUMINUM ALLOY SHEET AND PLATE, 4.4CU - 0.85SI - 0.80MN - 0.50MG (2014-O), ANNEALED
SAE AMS 4295 : 2013 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 AMS 4321 : 2016 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 AMS 4601 : 2017 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 AMS 4021 : 2017 ALUMINUM ALLOY, ALCLAD SHEET AND PLATE, 1.0MG - 0.60SI - 0.28CU - 0.20CR (ALCLAD 6061-0) ANNEALED
SAE AS 4444 : 2013 FITTINGS, 24 DEGREE CONE FLARELESS, FLUID CONNECTION, 5000 PSI
SAE AS 4875 : 2016 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 ARP 5812 : 2017 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 AMS H 6088 : 2000 HEAT TREATMENT OF ALUMINUM ALLOYS
SAE AMS 4146 : 2014 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 AS 7222 : 2013 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 AMS 2772 : 2016 HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS
MIL-DTL-85052-6 Revision A:2016 CLAMP, LOOP, ALUMINUM 2024-T42, 400 DEGREES F, FLUOROSILICONE
SAE AS 4841 : 2017 FITTINGS, 37 DEGREES INTERNAL FLARE, FLUID CONNECTION, PROCUREMENT SPECIFICATION
MIL-DTL-83798 Revision D:2008 FITTING, RUBBER HOSE, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR
SAE AMS 4051 : 1985 ALUMINUM ALLOY SHEET AND PLATE, ALCLAD 6.8ZN - 2.8MG - 2.0CU - 0.23CR (ALCLAD 7178-0) ANNEALED
MIL-DTL-85052-8 Revision A:2016 CLAMP, LOOP, ALUMINUM 2024-T42, 500 DEGREES F, SILICONE RUBBER, FABRIC REINFORCED
SAE AS 4842 : 2016 FITTINGS AND BOSSES, PIPE THREADED, FLUID CONNECTION
SAE AS 18280 : 2017 FITTINGS, 24 DEGREES 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 AMS 3025 : 2018 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 AMS 4080 : 2016 ALUMINUM ALLOY, DRAWN SEAMLESS TUBING, 1.0MG - 0.60SI - 0.28CU - 0.20CR (6061-0), ANNEALED
SAE AS 4843 : 2016 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 AMS 2767 : 2013 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 AMS 3025 : 2017 POLYALKYLENE GLYCOL HEAT TREAT QUENCHANT
SAE AMS 2750 : 2012 PYROMETRY
SAE AMS 2772 : 2016 HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS
SAE AMS 2658 : 2016 HARDNESS AND CONDUCTIVITY INSPECTION OF WROUGHT ALUMINUM ALLOY PARTS
SAE ARP 1962 : 1995 TRAINING AND APPROVAL OF HEAT-TREATING PERSONNEL

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