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Document ID:
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MIL-E-87231
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Overview
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Title:
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Engines, Aircraft, Turbojet and Turbofan (S/S by JSSG-2007)
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Scope:
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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.
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Status:
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Canceled
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Cancellation Date:
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09-SEP-2015
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FSC/Area:
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2840
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Doc Category:
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Detail Specification
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Amendments to military specifications or specification sheets issued after August 1, 2003 are incorporated in the modified document.
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Controlled Distribution Document(s)
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Revision History
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Click on column headings for a description of column content.
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 | Notice 2 - Cancellation | A | 09-SEP-2015 | 1 | 12.3 KB |
| Notice 1 - Cancellation | A | 11-JAN-1995 | 1 | 15.6 KB |
 | Amendment 1 | D | 15-APR-1986 | 1 | 41.7 KB |
| Base Document | D | 30-SEP-1985 | 315 | 11224.0 KB |
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