SAE AMSA21180B
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH
Superseded date
13-06-2017
Superseded by
Published date
01-01-2011
Publisher
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| DocumentType |
Standard
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| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| MIL-A-21180 Revision D:1984 | Similar to |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-STD-2088 Revision B:2007 | BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(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)/12(2014) : 2014 | 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 |
| MIL-PRF-7115 Revision G:2012 | CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| MIL-STD-1587 Revision D:2017 | MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
| SAE ARP 4058 : 2017 | GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS |
| PREN 4632-002 : 200P1 | AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 002: HOMOGENEOUS ASSEMBLIES ALUMINIUM AND ALUMINIUM ALLOYS |
| NF EN 4632-002 : 2008 | AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 002: HOMOGENEOUS ASSEMBLIES ALUMINIUM AND ALUMINIUM ALLOYS |
| SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
| MIL-DTL-9490 Revision E:2008 | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MS16051 Revision G:2014 | COUPLING, GROUND COOLING, COMBAT TYPE AIRCRAFT |
| MIL-PRF-7032 Revision H:2010 | INVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| BS EN 4632-002:2008 | Aerospace series. Welded and brazed assemblies for aerospace constructions. Weldability and brazeability of materials Homogeneous assemblies aluminium and aluminium alloys |
| EN 4632-002:2008 | Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 002: Homogeneous assemblies aluminium and aluminium alloys |
| NFL 06 380-20 : 2003 | AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 20: HOMOGENEOUS ASSEMBLIES ALUMINIUM AND ALUMINIUM ALLOYS |
| SAE ARP 5794 : 2014 | CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD |
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