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   Data updated: 16 Jan 2026. Home |  About Quick Search |  ASSIST |  ASSIST Updates Document Details
Document ID:   MIL-E-27675       Scroll down to access document images

Overview
Title:  Engine Pressure Ratio System, Turbofan Engine A/A24J-13 (No S/S Document)
Scope:  This specification covers one type of turbofan engine pressure ratio measuring system with vertical tape scale presentation, designated as A/A24J-13.
Status:  Canceled Cancellation Date:  04-MAY-2015      
6620 Doc Category:   Detail Specification  

Responsibilities
Lead Standardization Activity:  71  Air Force Sustainment Center - Oklahoma City  
  Preparing Activity: 71  Air Force Sustainment Center - Oklahoma City
Coordination:  Limited  
Air Force Custodian:  71   Air Force Sustainment Center - Oklahoma City  

Amendments to military specifications or specification sheets issued after August 1, 2003 are incorporated in the modified document.
Revision History Click on column headings for a description of column content.
MediaDocument Part DescriptionDist StmtDocument DatePagesSize
Document ImageRevision B Notice 4 - CancellationA04-MAY-2015112.2 KB
Document ImageRevision B Notice 3 - ValidationA08-SEP-200811.9 KB
Document ImageRevision B Notice 2 - InactivationA15-MAR-19961154.9 KB
Document ImageRevision B Notice 1 - ValidationA13-JUN-1988124.3 KB
Document ImageRevision B Amendment 2 A21-MAR-19836205.7 KB
Document ImageRevision B A10-AUG-1964401638.5 KB

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