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  • SAE AMS 2770 : 2015

    View superseded by
    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
    View superseded by

    HEAT TREATMENT OF WROUGHT ALUMINUM ALLOY PARTS

    Available format(s): 

    Superseded date:  11-04-2019

    Language(s): 

    Published date:  01-01-2015

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. TECHNICAL REQUIREMENTS
    4. QUALITY ASSURANCE PROVISIONS
    5. PREPARATION FOR DELIVERY
    6. ACKNOWLEDGMENT
    7. REJECTIONS
    8. NOTES

    Abstract - (Show below) - (Hide below)

    Describes the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts.

    General Product Information - (Show below) - (Hide below)

    Committee AMS-D
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By

    Standards Referenced By This Book - (Show below) - (Hide below)

    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

    Standards Referencing This Book - (Show below) - (Hide below)

    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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