SAE AMS4031H
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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, SHEET AND PLATE, 6.3CU - 0.30MN - 0.18ZR - 0.10V - 0.06TI (2219-O) ANNEALED OR WHEN SPECIFIED, 'AS FABRICATED' (2219-F)
Superseded date
16-07-2017
Superseded by
Published date
01-01-2011
Publisher
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| DocumentType |
Standard
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
| 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 |
| FAA AC 33-6 : 2017 | WELD REPAIR OF ALUMINUM CRANKCASES AND CYLINDERS OF PISTON ENGINES |
| 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 |
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