MIL A 83444 : 0
Withdrawn
Withdrawn
AIRPLANE DAMAGE TOLERANCE REQUIREMENTS
Amended by
Available format(s)
PDF
Language(s)
English
Publisher
Withdrawn date
07-23-2013
US$20.00
Excluding Tax where applicable
Covers damage tolerance design requirements applicable to airplane safety of flight structure.
| DocumentType |
Standard
|
| Pages |
19
|
| ProductNote |
New child NOT 1 1987 is now added
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL I 6870 : E | INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-P-87210 Base Document:1984 | Pneumatic Power Systems, High Pressure (No S/S Document) |
| 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 |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL-STD-1530 Revision D:2016 | Aircraft Structural Integrity Program (ASIP) |
| MIL-A-8867 Revision C:1987 | Airplane Strength and Rigidity Ground Tests |
| MIL-A-8866 Revision C:1987 | Airplane Strength and Rigidity Reliability Requirements, Repeated Loads, Fatigue and Damage Tolerance |
Summarise
US$20.00
Excluding Tax where applicable
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