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FAA AC 25.981-2 : 2008
|
FUEL TANK FLAMMABILITY REDUCTION MEANS
|
|
SAE AIR 5128 : 2012
|
ELECTRICAL BONDING OF AIRCRAFT FUEL SYSTEMS
|
|
SAE AMS C 27725 : 2016
|
COATING, CORROSION PREVENTATIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS, FOR USE TO 250 DEGREES F (121 DEGREES C)
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FAA AC 20-53 : 2006
|
PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING
|
|
MIL T 5578 : C
|
TANK, FUEL, AIRCRAFT, SELF-SEALING
|
|
FAA AC 20-136 : 2011
|
AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
|
|
SAE ARP 8615 : 2011
|
FUEL SYSTEM COMPONENTS: GENERAL SPECIFICATION FOR
|
|
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
|
|
MIL-C-27725 Revision B:1969
|
COATING, CORROSION PREVENTIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS
|
|
MIL T 5624 : R
|
TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5
|
|
GOST 10227 : 1986 AMD 6 2012
|
|
|
SAE AMS S 7124 : 2011
|
SEALING COMPOUND, POLYSULFIDE, ACCELERATOR REQUIRED, FOR AIRCRAFT STRUCTURES
|
|
SAE AIR 1662 : 2013
|
MINIMIZATION OF ELECTROSTATIC HAZARDS IN AIRCRAFT FUEL SYSTEMS
|
|
SAE ARP 5413 : 1999
|
CERTIFICATION OF AIRCRAFT ELECTRICAL/ELECTRONIC SYSTEMS FOR THE INDIRECT EFFECTS OF LIGHTNING
|
|
MIL-STD-464 Revision C:2010
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
|
|
ASTM D 910 : 2017-05
|
SPECIFICATION FOR LEADED AVIATION GASOLINES
|
|
SAE ARP 4043 : 1999
|
FLIGHT LINE GROUNDING AND BONDING OF AIRCRAFT
|
|
SAE AMS S 4383 : 2015
|
SEALING COMPOUND, TOPCOAT, FUEL TANK BUNA-N TYPE
|
|
MIL-STD-1568 Revision D:2015
|
Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems
|
|
DEFSTAN 91-91/7(2011) : 2011
|
TURBINE FUEL, KEROSINE TYPE, JET A-1 NATO CODE: F-35 JOINT SERVICE DESIGNATION: AVTUR
|
|
MIL-STD-882 Revision E:2012
|
System Safety
|
|
MIL-STD-461 Revision G:2015
|
REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
|
|
SAE AIR 4069 : 2016
|
SEALING OF INTEGRAL FUEL TANKS
|
|
SAE AMS S 29574 : 2001
|
SEALING COMPOUND, POLYTHIOETHER, FOR AIRCRAFT STRUCTURES, FUEL AND HIGH TEMPERATURE RESISTANT, FAST CURING AT AMBIENT AND LOW TEMPERATURES
|
|
MIL-DTL-83133 Revision J:2015
|
TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34), NATO F-35, AND JP-8+100 (NATO F-37)
|
|
ASTM D 4154 : 2014 : REDLINE
|
Standard Performance Specification for Men’s and Boys’ Knitted and Woven Beachwear and Sports Shirt Fabrics
|
|
SAE ARP 5583 : 2010
|
GUIDE TO CERTIFICATION OF AIRCRAFT IN A HIGH-INTENSITY RADIATED FIELD (HIRF) ENVIRONMENT
|
|
SAE ARP 5416 : 2013
|
AIRCRAFT LIGHTNING TEST METHODS
|
|
JSSG-2009 Revision A:2013
|
Air Vehicle Subsystems
|
|
SAC GB 6537 : 1994
|
NO.3 JET FUEL
|
|
SAE ARP 5577 : 2002
|
AIRCRAFT LIGHTNING DIRECT EFFECTS CERTIFICATION
|
|
SAE ARP 5414 : 2012
|
AIRCRAFT LIGHTNING ZONE
|
|
SAE AMS 3279 : 2013
|
SEALING COMPOUND, SPRAYABLE, FOR INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, FOR INTERMITTENT USE TO 350 DEGREES F (177 DEGREES C)
|
|
FAA AC 25.981-1 : 2008
|
FUEL TANK IGNITION SOURCE PREVENTION GUIDELINES
|
|
ASTM D 6469 : 2017 : REDLINE
|
Standard Guide for Microbial Contamination in Fuels and Fuel Systems
|
|
MIL-B-5087 Revision B:1964
|
BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
|
|
SAE ARP 5412 : 2013
|
AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS
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