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AIR FORCE - MIL-S-5711 CANC NOTICE 1

STRUCTURAL CRITERIA, PILOTED AIRPLANES STRUCTURAL TESTS, FLIGHT

inactive, Most Current
Organization: AIR FORCE
Publication Date: 23 April 1969
Status: inactive
Page Count: 1

Document History

MIL-S-5711 CANC NOTICE 1
April 23, 1969
STRUCTURAL CRITERIA, PILOTED AIRPLANES STRUCTURAL TESTS, FLIGHT
A description is not available for this item.
MIL-S-5711
December 14, 1954
STRUCTURAL CRITERIA, PILOTED AIRPLANES STRUCTURAL TESTS, FLIGHT
A description is not available for this item.

References

This document is referenced by:
MIL-A-8860 - Airplane Strength and Rigidity, General Specification for
Published by NPFC on June 24, 2019
A description is not available for this item.
This document is referenced by:
MIL-A-8861 - Airplane Strength and Rigidity Flight Loads
Published by NPFC on July 9, 2019
A description is not available for this item.
This document is referenced by:
MIL-A-8865 - Airplane Strength and Rigidity Miscellaneous Loads
Published by NPFC on June 24, 2019
A description is not available for this item.
This document is referenced by:
MIL-A-8866 - AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
Published by NPFC on May 20, 1987
This specification defines the strength and rigidity requirements for repeated loading condition applicable to Navy procured airplanes.
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