MIL-F-87154 Base Document:1980
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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FUEL SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503
01-07-1992
Outlines performance, compatibility, and verification prerequisites for an aircraft fuel system and its parts.
| DocumentType |
Standard
|
| Pages |
134
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| 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)/14(2014) : 2014 | 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)/11(2013) : 2013 | 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)/13(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 |
| SAE AIR1749 | Aircraft Engine Fuel Feed and Transfer Component Pressure Definitions |
| MS29559 Revision C:1974 | Fitting, (O) Ring, Circular, Thru Bolt Type, Single Groove, Tank |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MS29560 Revision C:1974 | Fitting, (O) Ring, Circular, Threaded Insert Type, Single Groove, Tank |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-C-38373 Revision B:1975 | Cap, Fluid Tank Filler (No S/S Document) |
| MIL STD 470 : B | MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS) |
| MIL T 38219 : B (1) | TURBINE FUEL, LOW VOLTALITY JP 7 |
| MS29558 Revision C:1974 | Fitting, (O) Ring, Circular, Compression Type, Single Groove, Tank (No S/S Document) |
| MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
| MIL-STD-1587 Revision D:2017 | Material and Process Requirements for Aerospace Weapons Systems |
| MS33645 Revision C:1977 | Receptacle, Grounding, Installation of (No S/S Document) |
| MIL V 38003 : NOTICE 1 | VALVE, FUEL LEVEL CONTROL, FUEL TANK, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL F 38363 : B (3) | FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL T 83133 : D | TURBINE FUELS, AVIATION, KEROSENE TYPES, NATO F-34 (JP-8) AND NATO F-35 |
| MIL-I-83294 Base Document:1971 | Installation Requirement, Aircraft Propulsion Systems, General Specification for (No S/S Document) |
| MS33611 Revision A:1983 | TUBE BEND RADII (S/S BY SAE-AS33611) |
| MIL-STD-202 Revision H:2015 | Electronic and Electrical Component Parts |
| MIL-STD-1247 Revision D:2009 | Markings, Functions and Hazards Designations of Hose, Pipe, and Tube Lines for Aircraft Missile, and Space Systems |
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