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SAE ARP1616B

Withdrawn

Withdrawn

View Superseded by

Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel and Oil Systems

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

08-31-2017

Withdrawn date

08-31-2017

Superseded by

SAE AIR1616A

US$152.22
Excluding Tax where applicable

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.

DocumentType
Standard
Pages
19
PublisherName
SAE International
Status
Withdrawn
SupersededBy
Supersedes

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

MS33540 Revision J:1986 SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR (S/S BY NASM33540)
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 (NO S/S DOCUMENT)
MIL-STD-130 Revision N:2007 Identification Marking of U.S. Military Property
SAE ARP868C 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 AS1055D Fire Testing of Flexible Hose, Tube Assemblies, Coils, Fittings, and Similar System Components
MIL-STD-45662 Revision A:1988 Calibration Systems Requirements (Refer to ISO-10012-1 and ANSI-Z540-1 or Comparable Standards as Alternatives to MIL-STD-45662)
QQ-A-367 Revision H:1973 Aluminum Alloy Forgings (S/S by SAE-AMS-QQ-A-367)
MIL-STD-2175 Revision A:1993 CASTINGS, CLASSIFICATION AND INSPECTION OF (S/S BY SAE-AMS-STD-2175)
MIL-STD-889 Revision C:2016 Galvanic Compatibility of Electrically Conductive Materials
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 (S/Sby NASM33588)
TT-S-735 Revision A:1988 STANDARD TEST FLUIDS, HYDROCARBON (S/S BY ASTM-D471)
MS20995 Revision E:1974 WIRE, SAFETY OR LOCK (S/S BY NASM20995)
MIL-STD-276 Revision A:1992 Impregnation of Porous Metal Castings and Powdered Metal Components
MIL-STD-1290 Revision A:1988 Light Fixed and Rotary-Wing Aircraft Crash Resistance
MIL-S-8879 Revision C:1991 Screw Threads, Controlled Radius Root withIncreased Minor Diameter, General Specification for (S/S by SAE-AS8879)
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 (S/S BY SAE-AMS-QQ-S-763)
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 (S/S by SAE-ARP8615)
MIL-B-5087 Revision B:1964 Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464)
FED-STD-595 Revision C:2008 Colors Used in Government Procurement (S/S By SAE-AMS-STD-595)
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

US$152.22
Excluding Tax where applicable