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SAE AS 1710 : 2014
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COUPLING, FUEL, FLEXIBLE, VARIABLE CAVITY, THREADED TYPE WITH FERRULES |
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MIL-DTL-22263 Revision C:2009
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Coupling Fuel Line, Flexible, 125 PSI General Specification for |
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SAE AS 5304 : 2011
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STANDARD SPECIFICATION FOR TURBINE FLOWMETERS |
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MIL-DTL-85061 Revision C:2009
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COUPLING, FUEL LINE, FLEXIBLE, 125 PSI |
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MIL-PRF-81975 Revision C:2008
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COUPLINGS, REGULATED, AERIAL PRESSURE REFUELING TYPE MA-2, TYPE MA-3 AND TYPE MA-4 |
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MIL-DTL-7899 Revision D:2014
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VALVES, CHECK, AIRCRAFT FUEL SYSTEM |
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GEIASTD0007B:2013
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LOGISTICS PRODUCT DATA |
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SAE AS 1650 : 2017
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COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, FIXED CAVITY, SELF-BONDING, PROCUREMENT SPECIFICATION |
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SAE ARP 1827C : 2014
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MEASURING AIRCRAFT GAS TURBINE ENGINE FINE FUEL FILTER ELEMENT PERFORMANCE |
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SAE AS 7510 : 2017
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COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, SELF-LOCKING, FIXED CAVITY, HIGH CONDUCTIVITY, SELF-BONDING, PART SPECIFICATION |
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MIL-PRF-57267 Base Document:2017
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COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5 |
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MIL-PRF-83323 Revision D:2016
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TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING |
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MIL-PRF-62625 Revision B:2009
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VALVE, FUEL-DRAIN |
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MIL-PRF-25017 Revision H:2011
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INHIBITOR, CORROSION/LUBRICITY IMPROVER, FUEL SOLUBLE (NATO S-1747) |
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MIL-DTL-24788 Revision B:2017
|
Coupling Assembly, Semi-Dry-Break, Quick-Disconnect Fuel, with or without Continuity Switch |
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SAE MAP 749 : 2015
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AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT ENDURANCE TEST PROCEDURE (ROOM TEMPERATURE CONTAMINATED FUEL) |
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SAE AS 5877 : 2016
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DETAILED SPECIFICATION FOR AIRCRAFT PRESSURE REFUELING NOZZLE |
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SAE AIR 786 : 2014
|
ELASTOMER COMPATIBILITY CONSIDERATIONS RELATIVE TO ELASTOMERIC SEALANT SELECTION |
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SAE ARP 1953 : 2014
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ACCEPTANCE TEST PROCEDURES AND STANDARDS TO ENSURE CLEAN FUEL SYSTEM COMPONENTS |
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MIL-N-25161 Revision C:1969
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NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
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SAE ARP 1797 : 2014
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AIRCRAFT AND AIRCRAFT ENGINE FUEL PUMP LOW LUBRICITY FLUID ENDURANCE TEST |