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SAE ARP1616B

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

View Superseded by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

31-08-2017

Withdrawn date

31-08-2017

Superseded by

SAE AIR1616A

€123.00
Excluding VAT

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Withdrawn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

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€123.00
Excluding VAT