NPFC - MIL-E-5007

ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR

active, Most Current

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Organization:	NPFC
Publication Date:	15 October 1973
Status:	active
Page Count:	225

scope:

This specification establishes the performance, operating characteristics, design features, detailed interface configuration definitions, and installation envelopes for turbojet and turbofan engines. It also establishes the demonstrations, tests, reports, inspection procedures, and other data required for satisfactory completion and acceptance, by the Using Service, of the Preliminary Flight Rating Tests (PFRT) and the Qualification Tests (QT) for the engines. Further, this specification identifies the tests, procedures and data required for satisfactory completion of the Acceptance Tests (AT) of production units of either model engine. Notwithstanding the requirements for test verification of individual points of performance or operating characteristics of the engines covered by this specification for purpose of PFRT, QT, or AT, the engine manufacturer/contractor shall continue to be fully responsible for all features, characteristics, and performance of the engine throughout the operating envelope, to the extent required by the applicable contact. This specification also establishes the content and format to be used by the engine contractor for the preparation of the engine specification in accordance with 6.5

intended Use:

Engines covered by this specification are intended for aircraft propulsion.