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NAVY - NAVAIR 13130.1A

(AIR-4.3.3) ROTARY WING AIRCRAFT STRUCTURAL LIFE LIMITS CHG NOT 1 - 10/20/97

inactive
Organization: NAVY
Publication Date: 31 March 1987
Status: inactive
Page Count: 54

Document History

NAVAIRI 13130.1
January 2, 1997
(AIR-4.3.3) ROTARY WING AIRCRAFT STRUCTURAL LIFE LIMITS CHG NOT 1 - 10/20/97
This instruction applies to all Navy rotary wing aircraft. It requires implementation by all naval activities having responsibilities for assuring continued safe aircraft operations. Maintaining and...
NAVAIR 13130.1B
January 2, 1997
(AIR-4.3.3) ROTARY WING AIRCRAFT STRUCTURAL LIFE LIMITS CHG NOT 1 - 10/20/97
A description is not available for this item.
NAVAIR 13130.1A
March 31, 1987
(AIR-4.3.3) ROTARY WING AIRCRAFT STRUCTURAL LIFE LIMITS CHG NOT 1 - 10/20/97
A description is not available for this item.
NAVAIR 13130.1
November 21, 1985
(AIR-4.3.3) ROTARY WING AIRCRAFT STRUCTURAL LIFE LIMITS CHG NOT 1 - 10/20/97
A description is not available for this item.

References

This document references:
NAVAIR 13920.1 - (AIR-4.3.3) PROCEDURES FOR SUBMITTING FLIGHT LOADS, LAUNCH, AND LANDING DATA FOR THE STRUCTURAL APPRAISAL OF FATIGUE EFFECTS PROGRAM
Published by NAVY on November 1, 2000
This instruction applies to all active Naval Aircraft Reporting Custodians (Naval Aviation Depots (NAVAVNDEPOTs), Naval Air Warfare Centers (NAVAIRWARCENs), Type Commanders (TYCOMs), and Fleet...
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