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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Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

AIRPLANE STRENGTH AND RIGIDITY, SONIC FATIGUE
Available format(s)

PDF

Superseded date

23-07-2013

Language(s)

English

Covers requirements for analysis, design and testing for the prevention of sonic fatigue in airplanes.

DocumentType
Standard
Pages
16
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Superseded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 JOINT SERVICE SPECIFICATION GUIDE - 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
MIL-A-8860 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR

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