|
MIL-PRF-25439 Revision C:2013
|
TRANSMITTER RATE OF FLOW, IN-FLIGHT REFUELING, 0-10,000 PPM, TYPE MB-3 |
|
DEFSTAN 00-970(PT0)/17(2016) : 2016
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
DEFSTAN 00-970(PT0)/14(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)/13(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
SAE ARP 6385 : 2017
|
AIRCRAFT FUEL PUMP MECHANICAL AND ELECTRICAL SAFETY DESIGN |
|
DEFSTAN 00-970(PT0)/16(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
|
MS29521 Revision H:2015
|
DISK, VALVE |
|
SAE AIR5691A : 2017
|
GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY INDICATING SYSTEMS |
|
SAE ARP594 : 2017
|
FUEL PUMP THERMAL SAFETY DESIGN |
|
MIL-HDBK-516 Revision C:2014
|
AIRWORTHINESS CERTIFICATION CRITERIA |
|
MIL-DTL-7899 Revision D:2014
|
VALVES, CHECK, AIRCRAFT FUEL SYSTEM |
|
SAE AIR 5774 : 2012
|
COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS |
|
SAE AS 7510 : 2017
|
COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, SELF-LOCKING, FIXED CAVITY, HIGH CONDUCTIVITY, SELF-BONDING, PART SPECIFICATION |
|
JSSG-2009 Revision A:2013
|
Air Vehicle Subsystems |
|
MIL-PRF-83323 Revision D:2016
|
TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING |
|
SAE AIR1184B : 2016
|
CAPACITIVE FUEL GAUGING SYSTEM ACCURACIES |
|
SAE ARP 5794 : 2014
|
CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD |
|
SAE AIR 4023 : 2016
|
AIRCRAFT TURBINE FUEL CONTAMINATION HISTORY AND ENDURANCE TEST REQUIREMENTS |
|
SAE AS5751:2018(R2023)
|
Design and Operating Requirements of the Onboard Aircraft Refueling System and Associated Ground Refueling Equipment Interface |