MIL A 8893 : 0
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
AIRPLANE STRENGTH AND RIGIDITY, SONIC FATIGUE
Amended by
Available format(s)
PDF
Language(s)
English
Publisher
Superseded date
23-07-2013
Superseded by
€16.67
Excluding VAT
Covers requirements for analysis, design and testing for the prevention of sonic fatigue in airplanes.
| DocumentType |
Standard
|
| Pages |
16
|
| ProductNote |
New child NOT 1 1987 now added
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL T 25920 : C | TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL A 8892 : 0 | AIRPLANE STRENGTH AND RIGIDITY, VIBRATION |
| MIL A 8892 : 0 | AIRPLANE STRENGTH AND RIGIDITY, VIBRATION |
| MIL-A-8870 Revision C:1993 | Airplane Strength and Rigidity Vibration, Flutter, and Divergence |
| MIL-A-8868 Revision B:1987 | Airplane Strength and Rigidity Data and Reports (No S/S Document) |
| MIL-A-8860 Revision B:1987 | Airplane Strength and Rigidity, General Specification for |
Summarise
Access your standards online with a subscription
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.
Important note : Users cannot be edited or removed once added to your Multi user PDF.