|
SAE AMS 2447 : 2012
|
COATING, THERMAL SPRAY, HIGH VELOCITY OXYGEN/FUEL PROCESS
|
|
MIL-PRF-7024 Revision F:2012
|
CALIBRATING FLUIDS, AIRCRAFT FUEL SYSTEM COMPONENTS
|
|
SAE AMS 1424 : 2016
|
FLUID, AIRCRAFT DEICING/ANTI-ICING, SAE TYPE 1
|
|
MIL-I-8500 Revision D:1980
|
INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES
|
|
MIL-STD-129 Revision R:2014
|
Military Marking for Shipment and Storage
|
|
SAE AMS 1428 : 2017
|
FLUID, AIRCRAFT DEICING/ANTI-ICING, NON-NEWTONIAN, (PSEUDOPLASTIC), SAE TYPES 2, 3 AND 4
|
|
MS24356 Revision E:2016
|
NOZZLE - TYPE MA-2, FLIGHT PRESSURE REFUELING
|
|
MIL-STD-130 Revision N:2007
|
IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
|
|
MIL-DTL-5624 Revision W:2016
|
TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5
|
|
NASM33588:2010
|
NUT, SELF-LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR
|
|
SAE AMS 2175 : 2010
|
CASTINGS, CLASSIFICATION AND INSPECTION OF
|
|
SAE ARP 868 : 2013
|
METHOD - PRESSURE DROP TESTS FOR FUEL SYSTEM COMPONENTS
|
|
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
|
|
MS24355 Revision C:2016
|
COUPLING, RECEPTION - TYPE MA-2, FLIGHT-PRESSURE-REFUELING, ASSEMBLY OF
|
|
MIL-PRF-85285 Revision E:2012
|
COATING: POLYURETHANE, AIRCRAFT AND SUPPORT EQUIPMENT
|
|
GOST 10227 : 1986 AMD 6 2012
|
|
|
MIL-PRF-81352 Revision C:2005
|
COATINGS, AIRCRAFT TOUCH-UP
|
|
SAE AMS R 83485 : 2014
|
RUBBER, FLUOROCARBON ELASTOMER, IMPROVED PERFORMANCE AT LOW TEMPERATURES
|
|
MIL-PRF-23377 Revision K:2012
|
PRIMER COATINGS: EPOXY, HIGH-SOLIDS
|
|
ASME B46.1 : 2009
|
SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY)
|
|
SAE AS 568 : 2014
|
AEROSPACE SIZE STANDARD FOR O-RINGS
|
|
NASM25027:2012
|
NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F
|
|
MIL-STD-889 Revision C:2016
|
DISSIMILAR METALS
|
|
NASM33540:2003
|
SAFETY WIRING, SAFETY CABLING, COTTER PINNING, GENERAL PRACTICES FOR
|
|
MIL-DTL-5541 Revision F:2006
|
Chemical Conversion Coatings on Aluminum and Aluminum Alloys
|
|
SAE AMS R 25988 : 1998
|
RUBBER, FLUOROSILICONE ELASTOMER, OIL-AND-FUEL-RESISTANT, SHEETS, STRIPS, MOLDED PARTS AND EXTRUDED SHAPES
|
|
ASTM D 910 : 2017-05
|
SPECIFICATION FOR LEADED AVIATION GASOLINES
|
|
SAE AMS 7259 : 2013
|
RUBBER: FLOUROCARBON (FKM), HIGH TEMPERATURE/FLUID RESISTANT, LOW COMPRESSION SET/85 TO 95 HARDNESS, FOR SEALS IN FUEL SYSTEMS AND SPECIFIC ENGINE OIL SYSTEMS
|
|
MS24358 Revision B:2016
|
FITTING, HOSE END - TYPE MA-2, FLIGHT PRESSURE REFUELING, RECEPTION COUPLING, OUTLINE DIMENSIONS FOR
|
|
NASM20995:2012
|
WIRE, SAFETY OR LOCK
|
|
SAE AS 8879 : 2004
|
SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER
|
|
MIL-N-25161 Revision C:1969
|
NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2
|
|
MIL A 8625 : F
|
ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
|
|
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)
|
|
MIL-DTL-27426 Revision C:1998
|
RINGS, RETAINING, SPIRAL (UNIFORM CROSS SECTION)
|
|
MS24361 Revision C:2016
|
RING, SPLIT - TYPE MA-2, FLIGHT PRESSURE REFUELING, RECEPTION COUPLING
|
|
MS24362 Revision A:1961
|
SLEEVE, TYPE MA-2, FLIGHT PRESSURE REFUELING, RECEPTION COUPLING
|
|
ASME Y14.100 : 2017
|
ENGINEERING DRAWING PRACTICES - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES
|
|
ASTM D 471 : 2016-02
|
TEST METHOD FOR RUBBER PROPERTY - EFFECT OF LIQUIDS
|
|
SAE AS 5202 : 2005
|
PORT OR FITTING END, INTERNAL STRAIGHT THREAD, DESIGN STANDARD
|
|
FED-STD-595 Revision C:2008
|
COLORS USED IN GOVERNMENT PROCUREMENT
|
|
SAE AS 29513 : 2016
|
PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT, 'O' RING
|
|
MIL-S-7742 Revision D:1991
|
SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR
|
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