SAE AS1969
Current
The latest, up-to-date edition.
Coupling Assembly, Self-Sealing, Quick Disconnect Fuel and Oil System Components
Hardcopy , PDF
English
02-01-2013
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1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 NOTES
This specification covers the requirements for self-sealing, quick-disconnect couplings for fuel and oil system components.
| DocumentType |
Standard
|
| Pages |
21
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
This specification covers the requirements for self-sealing, quick-disconnect couplings for fuel and oil system components.
| MIL-R-83248 Revision C:1994 | RUBBER, FLUOROCARBON ELASTOMER, HIGH TEMPERATURE, FLUID, AND COMPRESSION SET RESISTANT |
| SAE ARP24E | Determination of Hydraulic Pressure Drop |
| MIL L 7808 : K (1) | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-P-5315 Revision B:1964 | PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| QQ-P-35 Revision C:1988 | PASSIVATION TREATMENTS FOR CORROSION-RESISTANT STEEL |
| MIL L 23699 : E | LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
| SAE ARP868C | Method-Pressure Drop Tests for Fuel System Components |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| SAE AIR1047D | A Guide for the Selection of Quick-Disconnect Couplings for Aerospace Fluid Systems |
| MIL T 5624 : R | TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5 |
| MS8000 Revision E:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, REUSABLE FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARE-TO-FLARE |
| MS8005 Revision E:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PERMANENTLY ATTACHED FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARE-TO-FLARE |
| MIL C 7024 : D | CALIBRATING FLUID, AIRCRAFT FUEL SYSTEM COMPONENTS |
| QQ-C-320 Revision B:1974 | CHROMIUM PLATING (ELECTRODEPOSITED) |
| TT-S-735 Revision A:1988 | STANDARD TEST FLUIDS, HYDROCARBON |
| MIL R 25988 : B | RUBBER, FLUOROSILICONE ELASTOMER, OIL AND FUEL RESISTANT, SHEETS, STRIPS, MOLDED PARTS AND EXTRUDED SHAPES |
| MS8001 Revision E:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, REUSABLE FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARELESS-TO-FLARELESS |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-L-6082 Revision E:1990 | LUBRICATING OIL, AIRCRAFT PISTON ENGINE (NONDISPERSANT MINERAL OIL) |
| MIL-F-8615 Revision D:1976 | FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
| MIL H 8795 : D | HOSE ASSEMBLY, RUBBER HYDRAULIC, FUEL AND OIL RESISTANT |
| MS28741 Revision K:2010 | HOSE ASSEMBLY, DETACHABLE END FITTING, MEDIUM PRESSURE |
| MS8006 Revision D:2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PERMANENTLY ATTACHED FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARELESS-TO-FLARELESS |
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