MIL-A-8892 › Airplane Strength and Rigidity, Vibration (for Future Procure. See MIL-A-87221)

MIL-A-8892 - CANCELLATION NOTICE 1 - CANCELLED
Show Complete Document History


Airplane Strength and Rigidity, Vibration (for Future Procure. See MIL-A-87221)


To find similar documents by Federal Supply Class Code:

FSC 1510 (Aircraft, Fixed Wing)

 

Customers who bought this document also bought:

NAS-410
NAS Certification and Qualification of Nondestructive Test Personnel

AWS-D17.1/D17.1M
Specification for Fusion Welding for Aerospace Applications

MIL-H-7199
Heat Treatment of Wrought Copper-Beryllium Alloys, Process for (Copper Alloys: Numbers C17000, C17200, C17300, C17500, and C17510) (Superseded by SAE-AMS-H-7199)

ORDER



Document Number

MIL-A-8892

Revision Level

CANCELLATION NOTICE 1

Status

Cancelled

Publication Date

May 18, 1987