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MIL-E-5007D, MILITARY SPECIFICATION: ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR (15 OCT 1973) [SUPERSEDING MIL-E-5007C, MIL-E-5008C, & MIL-E-5009D] [NO S/S DOCUMENT]

MIL-E-5007D, MILITARY SPECIFICATION: ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR (15 OCT 1973) [SUPERSEDING MIL-E-5007C, MIL-E-5008C, & MIL-E-5009D] [NO S/S DOCUMENT]., This specification establishes the performance, operating characteristics, design features, detailed interface configuration definitions, and installation envelopes of turbojet and turbofan engines.

MIL-E-5007 Rev. D

    

Version:
D01-199720.41 KB MIL-E-5007D_NOTICE-1
D12-199523.63 KB MIL-E-5007D_AMENDMENT-3
D10-1982293.32 KB MIL-E-5007D_AMENDMENT-2
D10-197319.06 MB MIL-E-5007D

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