SAE AS18802
Current
The latest, up-to-date edition.
Fuel and Oil Lines, Aircraft, Installation of
Hardcopy , PDF
English
09-08-2013
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. NOTES
Covers the requirements for installation of fuel and oil lines in aircraft, except those lines furnished as part of the engine.
| DocumentType |
Standard
|
| Pages |
10
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
This specification covers the requirements for installation of fuel and oil lines in aircraft, except those lines furnished as part of the engine.
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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 |
| 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)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(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)/16(2015) : 2015 | 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 |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| MIL-T-8606 Revision C:1973 | TUBING, STEEL, CORROSION RESISTANT (18-8 STABILIZED AND EXTRA LOW CARBON) |
| MS33786 Revision B:2013 | Fitting, Installation, Flared Tube and Hose, Swivel |
| MIL T 5578 : C | TANK, FUEL, AIRCRAFT, SELF-SEALING |
| MIL-F-18280 Revision F:1995 | FITTING, FLARELESS TUBE, FLUID CONNECTION |
| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL H 8794 : D | HOSE, RUBBER, HYDRAULIC, FUEL AND OIL RESISTANT |
| MS33515 Revision J:1973 | FITTING END, STANDARD DIMENSIONS FOR BULKHEAD FLARELESS TUBE CONNECTIONS |
| AND10104 : REV 5 | TUBING, STEEL, CORROSION RESISTANT, ROUND, STANDARD DIMENSIONS FOR |
| MS21919 Revision E:1981 | CLAMP, LOOP TYPE, CUSHIONED, SUPPORT |
| MS33656 Revision J:1987 | FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL |
| MIL T 6396 : E | TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
| MS33583 Revision C:1993 | TUBING END, DOUBLE FLARE, STANDARD DIMENSIONS FOR |
| MIL-STD-143 Revision B:1969 | STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF |
| MS33584 Revision C:1990 | TUBING END, STANDARD DIMENSIONS FOR FLARED |
| MS33611 Revision A:1983 | TUBE BEND RADII |
| MIL H 8795 : D | HOSE ASSEMBLY, RUBBER HYDRAULIC, FUEL AND OIL RESISTANT |
| MIL T 5579 : 0 | TANK, SELF-SEALING OIL, AIRCRAFT |
| AND10064 : LATEST | FITTINGS - INSTALLATION OF FLARED TUBE, STRAIGHT THREADED CONNECTORS |
| MS33514 Revision G:1990 | FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (ASG) |
| MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
| MS28741 Revision K:2010 | HOSE ASSEMBLY, DETACHABLE END FITTING, MEDIUM PRESSURE |
| MIL C 22263 : B | COUPLING FUEL LINE, FLEXIBLE, 125 PSI, GENERAL SPECIFICATION FOR |
| MIL-S-7742 Revision D:1991 | SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR |
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