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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Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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Superseded date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

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Superseded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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