MIL-HDBK-510 Revision A:2014
Current
The latest, up-to-date edition.
AEROSPACE FUELS CERTIFICATION
English
1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. GENERAL GUIDANCE
5. DETAILED REQUIREMENTS
6. NOTES
APPENDIX A - REQUIREMENTS DECOMPOSITION AND TRACEABILITY
APPENDIX B - FUEL PROPERTIES/CHARACTERISTIC TESTING
APPENDIX C - BASELINE AEROSPACE FUEL PROPERTY INFORMATION
APPENDIX D - EVALUATING THE COMPATIBILITY OF ADDITIVES OR
ALTERNATIVE FUELS WITH FUEL SYSTEM MATERIALS
APPENDIX E - TOXICITY TEST PROTOCOL AND ESOH BASELINE
INFORMATION
APPENDIX F - FIRE PROTECTION AND SURVIVABILITY/VULNERABILITY
APPENDIX G - AIRCRAFT PROPULSION FUELS CERTIFICATON PROCESS
APPENDIX H - AEROSPACE FUELS INFRASTRUCTURE REQUIREMENTS
APPENDIX I - RISK ASSESSMENT RESULTS
APPENDIX J - CERTIFICATION LESSONS LEARNED
APPENDIX K - ENVIRONMENTAL, SAFETY AND OCCUPATIONAL HEALTH
APPENDIX L - FUEL PROPERTY TRACEABILITY INDEX
APPENDIX M - EVALUATION OF POTENTIAL CANDIDATE FUELS FOR
CERTIFICATION
APPENDIX N - STREAMLINED CERTIFICATION PROCESS
APPENDIX O - EVALUATION OF COMMERCIAL FUEL SPECIFICATION
CHANGES
Defines and documents a lean, knowledge-based process to evaluate, approve, and certify fuels and fuel additives for use in military aviation-fuel using and handling equipment.
Committee |
FSC 91GP
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DevelopmentNote |
Supersedes MIL HDBK 510-1 (A) & MIL HDBK 510-2. (09/2014) NEW CHILD NOT 1 IS ADDED
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DocumentType |
Standard
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Pages |
368
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ProductNote |
NEW CHILD NOT 1 IS ADDED
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PublisherName |
US Military Specs/Standards/Handbooks
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Status |
Current
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Supersedes |
SAE AIR 7484 : 2018 | GUIDANCE ON THE IMPACT OF FUEL PROPERTIES ON FUEL SYSTEM DESIGN AND OPERATION |
SAE AMS I 7444 : 2013 | INSULATION SLEEVING, ELECTRICAL, FLEXIBLE |
SAE AMS DTL 23053/5A : 2012 | INSULATION SLEEVING, ELECTRICAL, HEAT SHRINKABLE, POLYOLEFIN, FLEXIBLE, CROSSLINKED |
ASTM D 7111 : 2016 : REDLINE | Standard Test Method for Determination of Trace Elements in Middle Distillate Fuels by Inductively Coupled Plasma Atomic Emission Spectrometry (ICP-AES) |
ASTM D 3701 : 2017 : REDLINE | Standard Test Method for Hydrogen Content of Aviation Turbine Fuels by Low Resolution Nuclear Magnetic Resonance Spectrometry |
SAE AMS QQ A 250/12 : 2013 | ALUMINUM ALLOY 7075, PLATE AND SHEET |
SAE AMS 5737 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS AND TUBING, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1650 DEGREES F (899 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED |
SAE AMS S 8802 : 2015 | SEALING COMPOUND, FUEL RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES |
SAE AMS C 27725 : 2016 | COATING, CORROSION PREVENTATIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS, FOR USE TO 250 DEGREES F (121 DEGREES C) |
AFGS 87233 : B NOTICE 1 | SUPPORT SYSTEMS AND EQUIPMENT |
SAE AMS QQ P 416 : 2016 | PLATING, CADMIUM (ELECTRODEPOSITED) |
ASTM D 5452 : 2012 : REDLINE | Standard Test Method for Particulate Contamination in Aviation Fuels by Laboratory Filtration |
SAE AMS 5525 : 2012 | STEEL, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, 1800 DEGREE F (982 DEGREE C) SOLUTION HEAT TREATED |
MIL-DTL-5624 Revision W:2016 | TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5 |
SAE AMS 3361 : 2012 | SILICONE POTTING COMPOUND, ELASTOMERIC, TWO-PART, GENERAL PURPOSE, 140 TO 400 POISE (15 TO 40 PAS) VISCOSITY |
MIL-PRF-81733 Revision D:1998 | SEALING AND COATING COMPOUND, CORROSION INHIBITIVE |
SAE AMS 3276 : 2016 | SEALING COMPOUND, INTEGRAL FUEL TANKS AND GENERAL PURPOSE, INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C) |
SAE AMS 4027 : 2014 | ALUMINUM ALLOY, SHEET AND PLATE, 1.0MG - 0.60SI - 0.28CU - 0.20CR (6061; -T6 SHEET, -T651 PLATE), SOLUTION AND PRECIPITATION HEAT TREATED |
ASTM D 7170 : 2016 : REDLINE | Standard Test Method for Determination of Derived Cetane Number (DCN) of Diesel Fuel Oils—Fixed Range Injection Period, Constant Volume Combustion Chamber Method |
ASTM D 3227 : 2016 : REDLINE | Standard Test Method for (Thiol Mercaptan) Sulfur in Gasoline, Kerosine, Aviation Turbine, and Distillate Fuels (Potentiometric Method) |
MIL-PRF-370 Revision J:2002 | HOSE AND HOSE ASSEMBLIES, NONMETALLIC: ELASTOMERIC, LIQUID FUEL |
MIL-C-83019 Base Document:1968 | COATING, POLYURETHANE, FOR PROTECTION OF INTEGRAL FUEL TANK SEALING COMPOUND |
MIL-STD-1787 Revision B:1996 | AIRCRAFT DISPLAY SYMBOLOGY |
ASTM D 1414 : 2015 : REDLINE | Standard Test Methods for Rubber O-Rings |
MIL R 6855 : E | RUBBER, SYNTHETIC, SHEETS, STRIPS, MOLDED OR EXTRUDED SHAPES |
SAE AMS 7276H : 2011 | RUBBER: FLUOROCARBON (FKM) HIGH-TEMPERATURE-FLUID RESISTANT LOW COMPRESSION SET FOR SEALS IN FUEL SYSTEMS AND SPECIFIC ENGINE OIL SYSTEMS |
MIL-DTL-83054 Revision C:2003 | BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
AFGS-87139 Revision B:2013 | LANDING GEAR SYSTEMS |
ASTM D 129 : 2013-08 | TEST METHOD FOR SULFUR IN PETROLEUM PRODUCTS (GENERAL HIGH PRESSURE DECOMPOSITION DEVICE METHOD) |
SAE AMS 5643 : 2016 | STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, MECHANICAL TUBING, AND RINGS, 16CR - 4.0NI - 0.30CB (NB) - 4.0CU, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
AWS C3.5 : 1999 | SPECIFICATION FOR INDUCTION BRAZING |
JSSG-2000 Revision B:2004 | AIR SYSTEM |
SAE AMS 6470 : 2014 | STEEL, NITRIDING, BARS, FORGINGS, AND TUBING 1.6CR - 0.35MO - 1.13AL (0.38 - 0.43C) (135 MOD) |
ASTM D 924 : 2015 : REDLINE | Standard Test Method for Dissipation Factor (or Power Factor) and Relative Permittivity (Dielectric Constant) of Electrical Insulating Liquids |
JSSG-2007 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - ENGINES, AIRCRAFT, TURBINE |
GOST 10227 : 1986 AMD 6 2012 | |
SAE AMS 5504 : 2002 | STEEL, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 12.5CR (410), ANNEALED |
SAE AMS R 83485 : 2014 | RUBBER, FLUOROCARBON ELASTOMER, IMPROVED PERFORMANCE AT LOW TEMPERATURES |
EI 1581 : 2016 | SPECIFICATIONS AND LABORATORY QUALIFICATION PROCEDURES FOR AVIATION FUEL FILTER/WATER SEPARATORS |
SAE AMS 4037 : 2014 | ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024; -T3 FLAT SHEET, -T351 PLATE) SOLUTION HEAT TREATED |
JSSG-2010 Base Document:1998 | Crew Systems |
MIL-DTL-26521 Revision L:2014 | Hose Assembly, Nonmetallic, Fuel, Collapsible, Low Temperature with Non-Reusable Couplings |
SAE AMS 3375 : 2012 | ADHESIVE/SEALANT, FLUOROSILICONE AROMATIC FUEL RESISTANT, ONE-PART ROOM TEMPERATURE VULCANIZING |
SAE AMS P 83461 : 1998 | Packing, Preformed, Petroleum Hydraulic Fluid Resistant, Improved Performance at 275°F (135°C) |
ASTM D 5304 : 2015 : REDLINE | Standard Test Method for Assessing Middle Distillate Fuel Storage Stability by Oxygen Overpressure |
SAE AIR 4170 : 2016 | RETICULATED POLYURETHANE FOAM EXPLOSION SUPPRESSION MATERIAL FOR FUEL SYSTEMS AND DRY BAYS |
MIL-STD-2105 Revision D:2011 | HAZARD ASSESSMENT TESTS FOR NON-NUCLEAR MUNITIONS |
ASTM F 146 : 2012 : REDLINE | TEST METHODS FOR FLUID RESISTANCE OF GASKET MATERIALS |
SAE AMS 6345 : 2015 | STEEL, SHEET, STRIP, AND PLATE, 0.95CR - 0.20MO (0.28 - 0.33C) (SAE 4130), NORMALIZED OR OTHERWISE HEAT TREATED |
SAE AMS 3215 : 2012 | ACRYLONITRILE BUTADIENE (NBR) RUBBER - AROMATIC FUEL RESISTANT - 65-75 |
SAE AS 5127/1 : 2014 | AEROSPACE STANDARD TEST METHODS FOR AEROSPACE SEALANTS TWO-COMPONENT SYNTHETIC RUBBER COMPOUNDS |
SAE ARP 1256 : 2011 | PROCEDURE FOR THE CONTINUOUS SAMPLING AND MEASUREMENT OF GASEOUS EMISSIONS FROM AIRCRAFT TURBINE ENGINES |
ASTM D 156 : 2015 : REDLINE | Standard Test Method for Saybolt Color of Petroleum Products (Saybolt Chromometer Method) |
MIL-PRF-32233 Revision B:2015 | TANKS, COLLAPSIBLE, 3,000, 10,000, 20,000, 50,000, & 210,000 U.S. GALLONS, FUEL |
MIL-T-52983 Revision G:1994 | TANK, FABRIC, COLLAPSIBLE, 3,000 10,000 20,000 AND 50,000 GALLON, FUEL |
ASTM D 86 : 2017-06 | TEST METHOD FOR DISTILLATION OF PETROLEUM PRODUCTS AND LIQUID FUELS AT ATMOSPHERIC PRESSURE |
MIL-DTL-24441 Revision D:2009 | PAINT, EPOXY-POLYAMIDE, GENERAL SPECIFICATION FOR |
ASTM D 3343 : 2016 : REDLINE | Standard Test Method for Estimation of Hydrogen Content of Aviation Fuels |
API 5L : 2012 | LINE PIPE |
MIL-PRF-25017 Revision H:2011 | INHIBITOR, CORROSION/LUBRICITY IMPROVER, FUEL SOLUBLE (NATO S-1747) |
AWS C3.4 : 1999 | SPECIFICATION FOR TORCH BRAZING |
SAE AMS 3277 : 2015 | SEALING COMPOUND, POLYTHIOETHER RUBBER, FAST CURING FOR INTEGRAL FUEL TANKS AND GENERAL PURPOSE, INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C) |
MIL-HDBK-515 Base Document:2002 | WEAPON SYSTEM INTEGRITY GUIDE (WSIG) |
ASTM D 6272 : 2017 : REDLINE | Standard Test Method for Flexural Properties of Unreinforced and Reinforced Plastics and Electrical Insulating Materials by Four-Point Bending |
SAE AMS 6415 : 2016 | STEEL, BARS, FORGINGS, AND TUBING 0.80CR - 1.8NI - 0.25MO (0.38 - 0.43C) (SAE 4340) |
MIL-DTL-5541 Revision F:2006 | Chemical Conversion Coatings on Aluminum and Aluminum Alloys |
MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
ASTM D 5363 : 2016 : REDLINE | Standard Specification for Anaerobic Single-Component Adhesives (AN) |
SAE AMS R 25988 : 1998 | RUBBER, FLUOROSILICONE ELASTOMER, OIL-AND-FUEL-RESISTANT, SHEETS, STRIPS, MOLDED PARTS AND EXTRUDED SHAPES |
ASTM D 2624 : 2015 : REDLINE | Standard Test Methods for Electrical Conductivity of Aviation and Distillate Fuels |
SAE AMS 7257 : 2014 | PERFLUOROCARBON (FFKM) ENGINE OIL, FUEL AND HYDRAULIC FLUID RESISTANT 70 TO 80 HARDNESS FOR HIGH TEMPERATURE SEALS IN ENGINE OIL SYSTEMS, FUEL SYSTEMS AND HYDRAULIC SYSTEMS |
SAE AMS S 4383 : 2015 | SEALING COMPOUND, TOPCOAT, FUEL TANK BUNA-N TYPE |
SAE AMS 5688 : 2012 | STEEL, CORROSION-RESISTANT, WIRE, 18CR - 9.0NI (SAE 30302), SPRING TEMPER |
ASTM D 4529 : 2017 : REDLINE | Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels |
JSSG-2001 Revision B:2004 | Air Vehicle |
SAE AMS 3283 : 2011 | SEALING COMPOUND, POLYSULFIDE NON-CURING, GROOVE INJECTION, TEMPERATURE AND FUEL RESISTANT |
SAE AMS 7271 : 2010 | RINGS, SEALING, BUTADIENE-ACRYLONITRILE (NBR) RUBBER FUEL AND LOW TEMPERATURE RESISTANT 60 - 70 |
DEFSTAN 91-91/7(2011) : 2011 | TURBINE FUEL, KEROSINE TYPE, JET A-1 NATO CODE: F-35 JOINT SERVICE DESIGNATION: AVTUR |
SAE AMS 5613 : 2013 | STEEL, CORROSION AND HEAT RESISTANT, BARS, WIRE, FORGINGS, TUBING, AND RINGS 12.5CR (SAE 51410) ANNEALED |
ISO 20823:2003 | Petroleum and related products Determination of the flammability characteristics of fluids in contact with hot surfaces Manifold ignition test |
MIL-STD-3004 Revision D:2014 | QUALITY ASSURANCE/SURVEILLANCE FOR FUELS, LUBRICANTS AND RELATED PRODUCTS |
ASTM D 3240 : 2015 : REDLINE | Standard Test Method for Undissolved Water In Aviation Turbine Fuels |
MIL-STD-882 Revision E:2012 | System Safety |
ASTM D 4066 : 2013 | Standard Classification System for Nylon Injection and Extrusion Materials (PA) |
QQ-S-571 Revision F:1994 | SOLDER, ELECTRONIC (96 TO 485 DEGREES C) |
SAE AMS 3281 : 2016 | SEALING COMPOUND, POLYSULFIDE (T) SYNTHETIC RUBBER FOR INTEGRAL FUEL TANK AND FUEL CELL CAVITIES LOW DENSITY FOR INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C) |
SAE AMS 4750 : 2017 | SOLDER, TIN-LEAD, 45SN - 55PB |
MIL-DTL-5578 Revision D:2008 | TANKS, FUEL, AIRCRAFT, SELF-SEALING |
ASTM D 93 : 2016-07 | TEST METHODS FOR FLASH POINT BY PENSKY-MARTENS CLOSED CUP TESTER |
MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
ASTM D 2386 : 2015 | Standard Test Method for Freezing Point of Aviation Fuels |
AWS C3.6 : 1999 | SPECIFICATION FOR FURNACE BRAZING |
SAE AMS 6472 : 2014 | STEEL, BARS AND FORGINGS, NITRIDING 1.6CR - 0.35MO - 1.1AL (0.38 - 0.43C) (135 MOD) HARDENED AND TEMPERED, 112 KSI (772 MPA) TENSILE STRENGTH |
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) |
SAE ARP 1247 : 2010 | AIRCRAFT GROUND SUPPORT EQUIPMENT - GENERAL REQUIREMENTS |
SAE AMS 6277 : 2016 | STEEL BARS, FORGINGS, AND TUBING, 0.50CR - 0.55NI - 0.20MO (0.18 - 0.23C) (SAE 8620), VACUUM ARC OR ELECTROSLAG REMELTED |
MIL F 24385 : F | FIRE EXTINGUISHING AGENT, AQUEOUS FILM FORMING FOAM, (AFFF) LIQUID CONCENTRATE, FOR FRESH AND SEA WATER |
MIL H 17902 : F | HOSE, END FITTINGS AND HOSE ASSEMBLIES, SYNTHETIC RUBBER, AIRCRAFT FUELS |
JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
API 6D :2015 | SPECIFICATION FOR PIPELINE AND PIPING VALVES |
API 610 : 2010 | CENTRIFUGAL PUMPS FOR PETROLEUM, PETROCHEMICAL AND NATURAL GAS INDUSTRIES |
AWS C3.7 : 1999 | SPECIFICATION FOR ALUMINUM BRAZING |
ASME B16.21 : 2016 | NONMETALLIC FLAT GASKETS FOR PIPE FLANGES |
MIL-PRF-87260 Revision B:2006 | Foam Material, Explosion Suppression, Inherently Electrostatically Conductive, for Aircraft Fuel Tanks |
ASTM D 6379 : 2011 : REDLINE | TEST METHOD FOR DETERMINATION OF AROMATIC HYDROCARBON TYPES IN AVIATION FUELS AND PETROLEUM DISTILLATES - HIGH PERFORMANCE LIQUID CHROMATOGRAPHY METHOD WITH REFRACTIVE INDEX DETECTION |
MIL F 16884 : J | FUEL, NAVAL DISTILLATE |
MIL-R-46082 Revision B:1983 | RETAINING COMPOUNDS, SINGLE COMPONENT, ANAEROBIC |
ASTM D 257 : 2014 : REDLINE | Standard Test Methods for DC Resistance or Conductance of Insulating Materials |
MIL-DTL-38219 Revision D:1998 | TURBINE FUEL, LOW VOLATILITY, JP-7 |
MIL-PRF-8516 Revision G:1997 | SEALING COMPOUND, SYNTHETIC RUBBER, ELECTRIC CONNECTORS AND ELECTRIC SYSTEMS, CHEMICALLY CURED |
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) |
MMM-A-132 Revision B:1994 | ADHESIVES, HEAT RESISTANT, AIRFRAME STRUCTURAL, METAL TO METAL |
ASTM D 7171 : 2016 : REDLINE | Standard Test Method for Hydrogen Content of Middle Distillate Petroleum Products by Low-Resolution Pulsed Nuclear Magnetic Resonance Spectroscopy |
SAE AMS 2410 : 2010 | PLATING, SILVER, NICKEL STRIKE, HIGH BAKE |
ASTM D 1322 : 2015-06 | TEST METHOD FOR SMOKE POINT OF KEROSINE AND AVIATION TURBINE FUEL |
EI 1570 : 2012 | HANDBOOK ON ELECTRONIC SENSORS FOR THE DETECTION OF PARTICULATE MATTER AND/OR FREE WATER DURING AIRCRAFT REFUELLING |
SAE AMS P 5315 : 2013 | ACRYLONITRILE-BUTADIENE (NBR) RUBBER FOR FUEL-RESISTANT SEALS 60 TO 70 |
SAE AMS 3376 : 2015 | SEALING COMPOUND, NON-CURING, FLUOROSILICONE GROOVE INJECTION TEMPERATURE AND FUEL RESISTANT |
ASTM D 240 : 2017 : REDLINE | Standard Test Method for Heat of Combustion of Liquid Hydrocarbon Fuels by Bomb Calorimeter |
FED-STD-791 Revision D:2007 | TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS |
ASTM E 659 : 2015 : REDLINE | Standard Test Method for Autoignition Temperature of Chemicals |
MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
MIL-DTL-25988 Revision C:2006 | RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, SHEETS, STRIPS, MOLDED PARTS, AND EXTRUDED SHAPES |
MIL-DTL-27422 Revision F:2014 | TANK, FUEL, CRASH-RESISTANT, BALLISTIC-TOLERANT, AIRCRAFT |
ASTM D 2622 : 2016 : REDLINE | Standard Test Method for Sulfur in Petroleum Products by Wavelength Dispersive X-ray Fluorescence Spectrometry |
SAE AMS 2427 : 2012 | ALUMINUM COATING, ION VAPOR DEPOSITION |
SAE AMS 4029 : 2012 | ALUMINUM ALLOY SHEET AND PLATE (2014; -T6 SHEET, -T651 PLATE) SOLUTION AND PRECIPITATION HEAT TREATED (COMPOSITION SIMILAR TO UNS A92014) |
SAE AMS 4107 : 2012 | ALUMINUM ALLOY DIE FORGINGS (7050-T74) SOLUTION HEAT TREATED AND OVERAGED |
MIL-S-85334 Base Document:1980 | SEALING COMPOUND, NONCURING LOW CONSISTENCY, SILICONE, GROOVE INJECTION, FOR INTEGRAL FUEL TANKS |
EI 1598 : 2012 | DESIGN, FUNCTIONAL REQUIREMENTS AND LABORATORY TESTING PROTOCOLS FOR ELECTRONIC SENSORS TO MONITOR FREE WATER AND/OR PARTICULATE MATTER IN AVIATION FUEL |
FED-STD-141 Revision D:2001 | PAINT, VARNISH, LACQUER AND RELATED MATERIALS, METHODS OF INSPECTION, SAMPLING AND TESTING |
SAE AMS 5604 : 2016 | STEEL, CORROSION RESISTANT, SHEET, STRIP, AND PLATE, 16.5CR - 4.0NI - 4.0CU - 0.30CB, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
MIL-H-4495 Revision D:1985 | HOSE ASSEMBLY, RUBBER, AERIAL REFUELING |
ASTM D 471 : 2016-02 | TEST METHOD FOR RUBBER PROPERTY - EFFECT OF LIQUIDS |
JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
ASTM D 3359 : 2017 : REDLINE | Standard Test Methods for Rating Adhesion by Tape Test |
SAE AMS 6444 : 2015 | STEEL, BARS, FORGINGS, AND TUBING, 1.45CR (0.93 - 1.05C) (SAE 52100), PREMIUM AIRCRAFT-QUALITY, CONSUMABLE ELECTRODE VACUUM REMELTED |
EI 1540 : 2014 | DESIGN, CONSTRUCTION, COMMISSIONING, MAINTENANCE AND TESTING OF AVIATION FUELLING FACILITIES |
SAE AMS 7902 : 2015 | BERYLLIUM SHEET AND PLATE, 98BE |
DOD-L-85645 Revision A:1988 | LUBRICANT, DRY THIN FILM, MOLECULAR BONDED (METRIC) |
SAE AMS 3265 : 2015 | SEALING COMPOUND, POLYSULFIDE (T) RUBBER, FUEL RESISTANT, NON-CHROMATED CORROSION INHIBITING, FOR INTERMITTENT USE TO 360 DEGREES F (182 DEGREES C) |
A-A-3097 Base Document:1997 | ADHESIVES, CYANOACRYLATE, RAPID ROOM TEMPERATURE-CURING, SOLVENTLESS |
MIL-PRF-46010 Revision H:2013 | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING NATO CODE S-1738 |
SAE AMS 3278 : 2016 | SEALING AND COATING COMPOUND, POLYURETHANE (PUR), FUEL RESISTANT, HIGH TENSILE STRENGTH/ELONGATION, FOR INTEGRAL FUEL TANKS/FUEL CAVITIES/GENERAL PURPOSE |
ASTM D 5191 : 2015-10 | TEST METHOD FOR VAPOR PRESSURE OF PETROLEUM PRODUCTS (MINI METHOD) |
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