SAE ARP 1616 : 2017

Withdrawn

View Superseded by

SELF-SEALING BREAKAWAY VALVES FOR CRASH-RESISTANT AIRCRAFT FUEL AND OIL SYSTEMS

Available format(s)

Hardcopy , PDF

Withdrawn date

31-08-2017

Language(s)

English

Published date

01-01-2017

Publisher

SAE International

1. SCOPE
2. REFERENCES
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. NOTES

Describes design, performance, and test criteria for self-sealing breakaway valves for use in crash-resistant aircraft fuel systems.

Committee	AE-5A
DocumentType	Standard
Pages	19
PublisherName	SAE International
Status	Withdrawn
SupersededBy	SAE AIR 1616 : 2012

MS33540 Revision J:1986	SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR
MIL-I-8500 Revision D:1980	INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES
MIL-STD-129 Revision R:2014	Military Marking for Shipment and Storage
MIL-STD-970 Base Document:1987	STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF
MIL-STD-130 Revision N:2007	IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
SAE ARP 868 : 2013	METHOD - PRESSURE DROP TESTS FOR FUEL SYSTEM COMPONENTS
MIL-STD-810 Revision G:2008	ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
MIL-STD-2073-1 Revision E:2008	STANDARD PRACTICE FOR MILITARY PACKAGING
MIL T 5624 : R	TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5
SAE AS 1055 : 2013	FIRE TESTING OF FLEXIBLE HOSE, TUBE ASSEMBLIES, COILS, FITTINGS AND SIMILAR SYSTEM COMPONENTS
MIL-STD-45662 Revision A:1988	CALIBRATION SYSTEMS REQUIREMENTS
QQ-A-367 Revision H:1973	ALUMINUM ALLOY FORGINGS
MIL-STD-2175 Revision A:1993	CASTING, CLASSIFICATION AND INSPECTION OF
MIL-STD-889 Revision C:2016	DISSIMILAR METALS
MIL C 7024 : D	CALIBRATING FLUID, AIRCRAFT FUEL SYSTEM COMPONENTS
ASTM D 910 : 2017-05	SPECIFICATION FOR LEADED AVIATION GASOLINES
MS33588 Revision E:1984	NUTS, SELF LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR
TT-S-735 Revision A:1988	STANDARD TEST FLUIDS, HYDROCARBON
MS20995 Revision E:1974	WIRE, SAFETY OR LOCK
MIL-STD-276 Revision A:1992	IMPREGNATION OF POROUS METAL CASTINGS AND POWDERED METAL COMPONENTS
MIL-STD-1290 Revision A:1988	LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE
MIL-S-8879 Revision C:1991	SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR
MIL A 8625 : F	ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
QQ-S-763 Revision F:1996	STEEL BARS, WIRE, SHAPES AND FORGINGS; CORROSION RESISTANT
MIL T 83133 : D	TURBINE FUELS, AVIATION, KEROSENE TYPES, NATO F-34 (JP-8) AND NATO F-35
MIL-F-8615 Revision D:1976	FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG]
MIL-B-5087 Revision B:1964	BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
FED-STD-595 Revision C:2008	COLORS USED IN GOVERNMENT PROCUREMENT
MIL-S-7742 Revision D:1991	SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR
MIL N 25027 : G	NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F
MIL T 31000 : 0	TECHNICAL DATA PACKAGES - GENERAL SPECIFICATION FOR