SAE AS406A
Flight Directors (Turbine-Powered Subsonic Aircraft) (Stabilized: Aug 2012)
standard by SAE International, 08/22/2012
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Flight Directors (Turbine-Powered Subsonic Aircraft) (Stabilized: Aug 2012)
standard by SAE International, 08/22/2012
HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 ¿¿F, 45¿¿ TO 45¿¿, FLARED, LIGHTWEIGHT
standard by SAE International, 03/18/2018
Fitting Assembly, Cap, Flareless, Protective Closure, Low Pressure
standard by SAE International, 05/27/2009
HOSE ASSEMBLY, CONVOLUTED, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED CONDUCTIVE, FLARELESS, 45° TO 90°
standard by SAE International, 11/20/2014
SLEEVE, TUBE END, ACORN TO WELD, SHORT FLARELESS
standard by SAE International, 10/20/2013
CONNECTOR, AIR DUCT HOSE, GROUND COOLING, FEMALE
standard by SAE International, 01/07/2013
Contacts, Electrical Connector, General Specification For
standard by SAE International, 11/22/2011
Wire, Eelectrical, Polytetrafluoroethylene/Polyimide Insulated, Normal Weight, Nickel Coated, Copper Conductor, 260°C, 600 Volts
standard by SAE International, 12/05/2006
BEARING, PLAIN, SELF-ALIGNING, CHAMFERED OUTER RING
standard by SAE International, 12/15/2011