MIL-A-21180 Revision D:1984
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Aluminum-Alloy Castings, High Strength (S/S by SAE-AMS-A-21180)
Available format(s)
PDF
Published date
05-11-1984
Publisher
Superseded date
10-09-1999
Superseded by
£13.91
Excluding VAT
1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PACKAGING
6 NOTES
Describes the requirements for six alloy compositions, four inspection classes, four radiographic quality grades and six classes of mechanical properties of high strength aluminum-alloy castings.
| DevelopmentNote |
D NOTICE 1 - Notice of Cancellation/Superseded by SAE AMS A 21180 (05/2004)
|
| DocumentType |
Standard
|
| Pages |
31
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| Standards | Relationship |
| SAE AMSA21180B | Similar to |
| SAE AMS4133E | Similar to |
| SAE AMS4215H | Similar to |
| MIL-E-16400 Revision H:1987 | Electronic, Interior Communication and Navigation Equipment, Naval Ship and Shore: General Specification for (S/S by MIL-STD-2036) |
| MIL-A-8860 Revision B:1987 | Airplane Strength and Rigidity, General Specification for |
| MIL-W-63328 Base Document:1979 | Warhead GM, HE, M248 Inert Parts for |
| MIL-I-983 Revision E:1966 | Interior Communication Equipment, Naval Shipboard; Basic Design Requirements for (S/S by MIL-STD-2036) |
| MIL-I-85071 Revision A:1992 | Inverters, Aircraft, DC to AC, General Specification for (S/S by MIL-PRF-7032) |
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| MIL-HDBK-11991 Base Document:1996 | Design of Electrical, Electronic, and Electro-Mechanical Equipment, Guided Missile and Associated Weapon Systems (No S/S Document) |
| MIL-A-81724 Base Document:1969 | Adapter, Launcher, Aircraft, ADU-299/E (No S/S Document) |
| SAE AS8860 | Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications |
| MIL-A-23121 Revision C:1970 | Aircrew Environmental, Escape and Survival Cockpit Capsule System General Specification for (No S/S Document) |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-HDBK-1587 Base Document:1996 | Materials and Process Requirements for Air Force Weapons Systems (S/S by MIL-STD-1587) |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
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| 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) |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-STD-278 Revision F:1987 | WELDING AND CASTING STANDARD (REPLACEMENT DOCUMENT NAVSEA TECH PUB S9074-AR-GIB-010/278) |
| MIL-STD-2156 Base Document:1983 | Launcher, Rail, Guided Missile, Aircraft, General Design Criteria for |
| MIL-W-22248 Revision A:1971 | Weldments, Aluminum and Aluminum Alloy |
| MIL-STD-2131 Revision A:1991 | Launcher, Ejection, Guided Missile, Aircraft, General Design Criteria for |
| MIL-DTL-85110 Revision B:1997 | Bar, Repeatable Release Holdback (RRHB), Aircraft Launching, General Requirement for |
| NEMA XR 14-1990 (R1995, R2000) | RECOMMENDED PRACTICES FOR LOAD-BEARING MECHANICAL ASSEMBLIES USED IN DIAGNOSTIC IMAGING |
| MIL-R-85880 Base Document:1988 | ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| DOD-E-8983 Revision C:1977 | ELECTRONIC EQUIPMENT, AEROSPACE, EXTENDED SPACE ENVIRONMENT, GENERAL SPECIFICATION FOR |
| MIL-STD-1547 Revision B:1992 | Electronic Parts, Materials, and Processes for Space and Launch Vehicles |
| MIL A 87221 : 0 | AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
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| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL-C-24105 Revision D:1995 | Converters, Synchro Signal (Panel Mounted), General Specification for |
| MIL-R-24358 Base Document:1968 | RESTORATION SHIPBOARD ELECTRONIC EQUIPMENT F, 1N AND 2N COGNIZANCE (S/S BY MIL-STD-2110) |
| MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| NAVSEA S9074 AQ GIB 010/248 : 0 | REQUIREMENTS FOR WELDING AND BRAZING PROCEDURE AND PERFORMANCE QUALIFICATION |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| JSSG-2010-12 Base Document:1998 | Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
| MIL-A-28772 Revision C:1984 | Antenna, High Frequency (HF) Fixed Rotatable Log Periodic (No S/S/ Document) |
| MIL-F-8615 Revision D:1976 | Fuel System Components, General Specification for (S/S by SAE-ARP8615) |
| MIL-P-85315 Base Document:1979 | Pump, Ejector, Air Vehicle Fuel, General Specification For |
| DOD-C-85050 Base Document:1982 | Charger, Battery, Nickel-Cadmium, Aircraft General Specification for (No S/S Document) |
| MIL C 7115 : F | CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| QQ-A-601 Revision F:1981 | Aluminum Alloy Sand Castings (S/S by ASTM-B26/B26M) |
| MIL-W-5013 Revision L:1991 | Wheel and Brake Assemblies, Aircraft General Specification For |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| SAE AMS3025D | Polyalkylene Glycol Heat Treat Quenchant |
| MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (SEE NAS410 AS A POSSIBLE REPLACEMENT) |
| MIL I 6866 : B | INSPECTION, PENETRANT METHOD OF |
| ASTM E 155 : 2015 : REDLINE | Standard Reference Radiographs for Inspection of Aluminum and Magnesium Castings |
| MIL-STD-2175 Revision A:1993 | CASTINGS, CLASSIFICATION AND INSPECTION OF (S/S BY SAE-AMS-STD-2175) |
| ASTM B 557 : 2015 : REDLINE | Standard Test Methods for Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products |
| MIL-STD-1537 Revision C:2002 | Electrical Conductivity Test for Verification of Heat Treatment of Aluminum Alloys, Eddy Current Method |
| MIL-STD-453 Revision C:1984 | Inspection, Radiographic (S/S By ASTM-E1742) |
| MIL-STD-649 Revision C:1976 | Aluminum and Magnesium Products Preparation for Shipment and Storage(S/S by ASTM-B660) |
| MIL-H-6088 Revision G:1991 | Heat Treatment of Aluminum Alloys (S/S by SAE-AMS-H-6088) |
| MIL-I-25135 Revision E:1984 | Inspection Materials, Penetrants (S/S by SAE-AMS2644) |
| MIL-STD-105 Revision E:1989 | Sampling Procedures and Tables for Inspection by Attributes (See Notice 3 for Replacement Information) |
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£13.91
Excluding VAT
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