MIL-E-5007 Revision D:1973
Current
The latest, up-to-date edition.
Engine, Aircraft, Turbojet and Turbofan, General Specification for
15-10-1973
Gives performance, operating characteristics, design features, interface configuration definitions, and installation envelopes for turbojet and turbofan engines. Establishes tests, demonstrations, reports, inspection procedures, and other data required.
| DevelopmentNote |
INACTIVE FOR NEW DESIGN 8/1/97
|
| DocumentType |
Standard
|
| Pages |
235
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
This specification establishes the performance, operating characteristics, design features, detailed interface configuration definitions, and installation envelopes of turbojet and turbofan engines.
| MIL-I-83294 Base Document:1971 | Installation Requirement, Aircraft Propulsion Systems, General Specification for (No S/S Document) |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-HDBK-244 Revision A:1990 | Guide to Aircraft/Stores Compatibility |
| SAE AS681K | Gas Turbine Engine Performance Presentation for Computer Programs |
| FAA AC 33.28-3 : 2014 | GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, ENGINE CONTROL SYSTEMS |
| MIL-STD-3050 Base Document:2015 | Aircrew Breathing Systems (ACBS) |
| FAA AC 35.23-1 : 2011 | GUIDANCE MATERIAL FOR 14 CFR SECTION 35.23, PROPELLER CONTROL SYSTEM |
| MIL-C-0024196 Revision B:1991 | Cleaning System, Ultrasonic (No S/S Document) |
| MIL-C-24196 Revision A:1988 | Cleaning System, Ultrasonic |
| SAE AIR5867 | Assessment of the Inlet/Engine Total Temperature Distortion Problem |
| MIL-B-9972 Revision B:1994 | Brazing, Nickel Alloy, General Specification for (S/S by AWS-C3.6) |
| MIL T 25920 : C | TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION |
| API 11PGT : 1992 | RECOMMENDED PRACTICE FOR PACKAGED COMBUSTION GAS TURBINES |
| SAE ARP5638 | RMS Terms and Definitions |
| SAE ARP5757A | Guidelines for Engine Component Tests |
| MIL-S-38399 Revision A:1975 | Starter, Pneumatic, Aircraft Engine General Specification For (No S/S Document) |
| FAA AC 33-2 : 2013 | GENERAL TYPE CERTIFICATION GUIDELINES FOR TURBINE ENGINES |
| SAE ARP1827C | Measuring Aircraft Gas Turbine Engine Fine Fuel Filter Element Performance |
| MIL-D-8708 Revision C:1991 | Demonstration: Aircraft Weapon Systems, General Specification for |
| API 616 REDLINE : 2011 | GAS TURBINES FOR THE PETROLEUM, CHEMICAL, AND GAS INDUSTRY SERVICES |
| API 616 : 2011 | GAS TURBINES FOR THE PETROLEUM, CHEMICAL, AND GAS INDUSTRY SERVICES |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
Access your standards online with a subscription
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.
Important note : Users cannot be edited or removed once added to your Multi user PDF.