MIL MIL-E-87231 Notice 2 – Cancellation – Engines, Aircraft, Turbojet and Turbofan (S/S by JSSG-2007)
This specification establishes the performance, functional operation, durability, reliability, maintainability of subsystems, physical characteristics, and installation interface requirements for aircraft turbojet and turbofan engines. It establishes the inspections, analyses, demonstrations and tests necessary to verify compliance with the stated requirements.
Product Details
Published:
09/09/2015
Number of Pages:
1
File Size:
1 file , 46 KB
Note:
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