MIL F 38363 : B (3)
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR
Superseded date
23-07-2013
Published date
12-01-2013
Publisher
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Criteria for design, performance, installation, and testing and maintenance of the fuel system and subsystems of aircraft powered by air breathing engines.
| DocumentType |
Standard
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| MIL-I-83294 Base Document:1971 | INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-F-87154 Base Document:1980 | FUEL SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
| DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| 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)/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)/11(2013) : 2013 | 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(PT7)SEC7/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| SAE ARP 1401 : 2012 | AIRCRAFT FUEL SYSTEM AND COMPONENT ICING TEST |
| DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL T 25920 : C | TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION |
| SAE AIR 1749 : 2013 | AIRCRAFT ENGINE FUEL FEED AND TRANSFER COMPONENT PRESSURE DEFINITIONS |
| MIL-N-25161 Revision C:1969 | NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
| MIL-A-25896 Revision E:1983 | ADAPTER, PRESSURE FUEL SERVICING, NOMINAL 2.5 INCH DIAMETER |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MIL B 83054 : B | BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
| MIL-G-26988 Revision C:1971 | GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
| MIL-STD-701 Revision P:1992 | LISTS OF STANDARD SEMICONDUCTOR DEVICES |
| MS24355 Revision C:2016 | COUPLING, RECEPTION - TYPE MA-2, FLIGHT-PRESSURE-REFUELING, ASSEMBLY OF |
| MS24335 Revision C:1994 | Flange, Bulkhead Mounting, Hydraulic, Self-Sealing Coupling |
| MIL-C-38373 Revision B:1975 | CAP, FLUID TANK FILLER |
| BB-N-411 Revision C:1973 | NITROGEN, TECHNICAL |
| MIL STD 470 : B | MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS) |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| MS29520 Revision H:1992 | ENVELOPE DIMENSIONS NOZZLE, PRESSURE FUEL SERVICING LOCKING AIRCRAFT, TYPE D-1 AND D-2 |
| MS29525 Revision F:1991 | CAP PRESSURE FUEL SERVICING, NOMINAL 2 1/2 INCH DIAMETER, FLUSH TYPE |
| MS33583 Revision C:1993 | TUBING END, DOUBLE FLARE, STANDARD DIMENSIONS FOR |
| MIL-STD-143 Revision B:1969 | STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| MS33645 Revision C:1977 | RECEPTACLE, GROUNDING, INSTALLATION OF |
| MIL-C-81511 Revision F:1992 | CONNECTOR, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT ENVIRONMENT RESISTING, AND ACCESSORIES GENERAL SPECIFICATION FOR |
| MIL V 38003 : NOTICE 1 | VALVE, FUEL LEVEL CONTROL, FUEL TANK, AIRCRAFT GENERAL SPECIFICATION FOR |
| MS33584 Revision C:1990 | TUBING END, STANDARD DIMENSIONS FOR FLARED |
| MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS |
| MIL-I-83294 Base Document:1971 | INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR |
| MS33611 Revision A:1983 | TUBE BEND RADII |
| MIL T 83323 : A (2) | TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING |
| MS29526 Revision E:1991 | CAP PRESSURE FUEL SERVICING, NOMINAL 2 1/2 INCH DIAMETER NON FLUSH TYPE |
| QQ-P-416 Revision F:1991 | PLATING, CADMIUM (ELECTRODEPOSITED) |
| MS33514 Revision G:1990 | FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (ASG) |
| MIL-STD-1247 Revision D:2009 | MARKINGS, FUNCTIONS AND HAZARDS DESIGNATIONS OF HOSE, PIPE, AND TUBE LINES FOR AIRCRAFT MISSILE, AND SPACE SYSTEMS |
| MIL-R-27521 Revision A:1971 | RECEPTACLE, FLYING BOOM, AERIAL REFUELING GENERAL SPECIFICATION FOR |
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