|
MIL-PRF-94-3 Revision M:2006
|
RESISTOR, VARIABLE, COMPOSITION, STYLE RV6
|
|
MIL-A-25896 Revision E:1983
|
ADAPTER, PRESSURE FUEL SERVICING, NOMINAL 2.5 INCH DIAMETER
|
|
MIL-L-3661-35 Base Document:1967
|
LENSES, INDICATOR-LIGHT, WATERTIGHT, STYLE LC35
|
|
MIL-PRF-7024 Revision F:2012
|
CALIBRATING FLUIDS, AIRCRAFT FUEL SYSTEM COMPONENTS
|
|
MS90310 Revision J:2011
|
Switch, Toggle, Positive Break, Miniature, Toggle Sealed, Solder Lug, Single Pole, .469 Mounting Bushing
|
|
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
|
|
MIL-DTL-3661-47 Revision B:2009
|
Lampholders, Housings, Indicator-Light, Watertight Style LH89
|
|
SAE ARP 8615 : 2011
|
FUEL SYSTEM COMPONENTS: GENERAL SPECIFICATION FOR
|
|
SAE ARP 868 : 2013
|
METHOD - PRESSURE DROP TESTS FOR FUEL SYSTEM COMPONENTS
|
|
MIL-PRF-85285 Revision E:2012
|
COATING: POLYURETHANE, AIRCRAFT AND SUPPORT EQUIPMENT
|
|
MIL-DTL-83413-7 Revision F:2015
|
Connectors and Assemblies, Electrical, Aircraft Grounding: Grounding Clamp Connector for Types I and III Grounding Assemblies, Aluminum Clip, Electrical
|
|
SAE AS 5877 : 2016
|
DETAILED SPECIFICATION FOR AIRCRAFT PRESSURE REFUELING NOZZLE
|
|
MIL-DTL-8834 Revision K:2016
|
Switches, Toggle, Positive Break, General Specification for
|
|
MIL-PRF-23377 Revision K:2012
|
PRIMER COATINGS: EPOXY, HIGH-SOLIDS
|
|
MIL-DTL-38449 Revision D:2010
|
SIGNAL AND SIGNAL/INTERCOMMUNICATION AMPLIFIERS, UNIVERSAL, AERIAL REFUELING
|
|
MIL-DTL-83413-10 Revision C:2010
|
Connectors and Assemblies, Electrical, Aircraft Grounding: Jumper Cable Assembly, Aircraft to Fuel Nozzle, Discharger, Electrostatic
|
|
MS8005 Revision E:2016
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PERMANENTLY ATTACHED FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARE-TO-FLARE
|
|
MIL-DTL-3661 Revision D:2013
|
Lampholders, Indicator Lights, Indicator Light Housings, and Indicator Light Lenses, General Specification for
|
|
SAE AS 31061 : 2017
|
CONNECTOR, PLUG, ELECTRIC, STRAIGHT, SOLDER CONTACTS, AN TYPE
|
|
MS29520 Revision H:1992
|
ENVELOPE DIMENSIONS NOZZLE, PRESSURE FUEL SERVICING LOCKING AIRCRAFT, TYPE D-1 AND D-2
|
|
MIL-STD-464 Revision C:2010
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
|
|
SAE AS 50151 : 2015
|
CONNECTORS, ELECTRICAL, CIRCULAR THREADED, AN TYPE, GENERAL SPECIFICATION FOR
|
|
MIL-DTL-83511-2 Revision A:2004
|
Headset-Microphone H-157A/AIC
|
|
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)
|
|
JSSG-2009 Revision A:2013
|
Air Vehicle Subsystems
|
|
MS29526 Revision E:1991
|
CAP PRESSURE FUEL SERVICING, NOMINAL 2 1/2 INCH DIAMETER NON FLUSH TYPE
|
|
MIL-C-8605 Revision B:1990
|
CAP, PRESSURE FUEL SERVICING
|
|
MIL-PRF-10304-32 Revision A:1999
|
METERS, ELECTRICAL INDICATING, PANEL TYPE, RUGGEDIZED: VOLTMETER, DC (FLUSH MOUNTING, ROUND FLANGE, 1 INCH), STYLES 05, 06, AND 07
|
|
ASTM D 471 : 2016-02
|
TEST METHOD FOR RUBBER PROPERTY - EFFECT OF LIQUIDS
|
|
MIL-R-27521 Revision A:1971
|
RECEPTACLE, FLYING BOOM, AERIAL REFUELING GENERAL SPECIFICATION FOR
|
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