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MIL-F-8615 Revision D:1976

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

Fuel System Components, General Specification for (S/S by SAE-ARP8615)

Available format(s)

PDF

Published date

29-03-1976

Superseded date

29-05-2013

Superseded by

SAE ARP8615

£13.91
Excluding VAT

Covers requirements for aircraft fuel, vent, and propulsion system functional components.

DevelopmentNote
D NOTICE 1 - Notice of Cancellation/Superseded by SAE ARP 8615. (06/2013)
DocumentType
Standard
Pages
31
PublisherName
US Military Specs/Standards/Handbooks
Status
Superseded
SupersededBy

This specification covers the requirements for aircraft fuel, vent, and propulsion system functional components.

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DEFSTAN 00-970(PT0)/11(2013) : 2013 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
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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
MIL-C-7413 Revision B:1970 Coupling, Quick Disconnect, Automatic Shutoff, General Specification for (S/S by SAE-AS7413)
MIL-A-19736 Revision A:1960 Air Refueling Systems, General Specification for
MIL V 7899 : C VALVE, CHECK, AIRCRAFT FUEL SYSTEM
MIL-I-23870 Base Document:1963 Indicator, Fuel Rate of Flow, 0 to 15 GPM (No S/S Document)
MIL-S-8710 Revision B:1969 Strainer, Airframe Fuel System, General Specification for
MIL-V-8610 Revision B:1984 Valve, Fuel Shutoff Solenoid Operated, 28 Volt DC
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MIL T 25439 : A (1) TRANSMITTER, RATE OF FLOW, IN-FLIGHT REFUELLING, 0-10,000 PPM, TYPE MB-3
MIL-P-5238 Revision C:1974 Pump, Centrifugal, Fuel Booster, Aircraft, General Specification For
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MIL C 24788 : 0 COUPLING ASSEMBLY, SEMI-DRY-BREAK QUICK-DISCONNECT, FUEL WITH OR WITHOUT CONTINUITY SWITCH
MIL-A-25896 Revision E:1983 Adapter, Pressure Fuel Servicing, Nominal 2.5-Inch Diameter
MIL-T-81838 Base Document:1971 Tank, Fuel, Aircraft, Auxiliary External 300 Gallon, Type Aero-1D (No S/S Document)
MIL-N-25161 Revision C:1969 NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2
MIL-P-85315 Base Document:1979 Pump, Ejector, Air Vehicle Fuel, General Specification For
MIL-STD-1606 Revision A:1983 TECHNICAL INFORMATION REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE PROPOSALS (NO S/S DOCUMENT)

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MIL-STD-704 Revision F:2004 Aircraft Electric Power Characteristics
MIL-STD-130 Revision N:2007 Identification Marking of U.S. Military Property
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
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MIL T 5624 : R TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5
MIL-E-6051 Revision D:1967 Electromagnetic Compatibility Requirements, Systems (S/S by MIL-STD-464)
MIL-E-25499 Revision C:1970 Electrical System, Aircraft, Design and Installation of, General Requirements for (No S/S Document)
MIL-STD-889 Revision C:2016 Galvanic Compatibility of Electrically Conductive Materials
MIL C 7024 : D CALIBRATING FLUID, AIRCRAFT FUEL SYSTEM COMPONENTS
MS33656 Revision J:1987 FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL (S/S BY SAE-AS4395)
MIL-STD-831 Base Document:1963 TEST REPORTS, PREPARATION OF
QQ-C-320 Revision B:1974 CHROMIUM PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-C-320)
MIL-F-7190 Revision B:1985 Forging, Steel, for Aircraft/Aerospace Equipment and Special Ordinance Applications (S/S by SAE-AMS-F-7190)
MIL C 38999 : J CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS
TT-S-735 Revision A:1988 STANDARD TEST FLUIDS, HYDROCARBON (S/S BY ASTM-D471)
MIL-G-5572 Revision F:1969 Gasoline, Aviation: Grades 80/87, 100/130, 115/145 (S/S by ASTM-D910)
MIL R 25988 : B RUBBER, FLUOROSILICONE ELASTOMER, OIL AND FUEL RESISTANT, SHEETS, STRIPS, MOLDED PARTS AND EXTRUDED SHAPES
MIL-STD-143 Revision B:1969 STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970)
MIL-STD-882 Revision E:2012 System Safety
MIL-M-8609 Revision B:1965 Motor, DC, 28 Volt System, Aircraft, General Specification for
MIL-STD-461 Revision G:2015 Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment
MIL-S-8879 Revision C:1991 Screw Threads, Controlled Radius Root withIncreased Minor Diameter, General Specification for (S/S by SAE-AS8879)
MS16142 Revision C:1979 BOSS, GASKET SEAL STRAIGHT THREAD TUBE FITTING, STANDARD DIMENSIONS FOR (S/S BY SAE-J1926/1 AND ISO725)
MIL-STD-1523 Revision A:1984 AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIEL (FOR AEROSPACE APPLICATIONS) (S/S BY SAE-AS1933 AND SAE-ARP5316)
MIL-STD-471 Revision A:1973 MAINTAINABILITY VERIFICATION/ DEMONSTRATION/EVALUATION (S/S BY MIL-HDBK-471)
MIL-A-21180 Revision D:1984 Aluminum-Alloy Castings, High Strength (S/S by SAE-AMS-A-21180)
MIL-STD-794 Revision E:1982 PART AND EQUIPMENT, PROCEDURES FOR PACKAGING AND PACKING OF
MIL-S-4040 Revision G:2012 Solenoid, Electrical General Specification for (No S/S Document)
MIL-STD-100 Revision G:1997 ENGINEERING DRAWINGS (S/S BY ASME-Y14.100, ASME-Y14.24, ASME-Y14.35M, AND ASME-14.34M)
MIL-M-7969 Revision C:1965 Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for
MIL-STD-462 Revision D:1993 MEASUREMENT OF ELECTROMAGNTIC INTERFERENCE CHARACTERISTICS (S/S BY MIL-STD-461)
MIL-STD-202 Revision H:2015 Electronic and Electrical Component Parts
QQ-P-416 Revision F:1991 Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416)
MIL-B-5087 Revision B:1964 Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464)
MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
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MIL-E-7080 Revision B:1962 Electric Equipment, Aircraft, Selection and Installation of (S/S by MIL-STD-7080)
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£13.91
Excluding VAT