01719nam 2200373 450 991013650760332120231206165421.01-5044-0444-010.1109/IEEESTD.1957.7438704(CKB)3710000000619065(NjHacI)993710000000619065(EXLCZ)99371000000061906520231206d1957 uy 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierAIEE No 803-1957 AIEE Proposed Test Code for Aircraft Equipment Electrical Insulation /IEEE[Place of publication not identified] :IEEE,1957.1 online resourceThe extremes of aircraft environment and rigorous reliability requirements, make special consideration of aircraft insulation testing procedure desirable. Operating temperatures, in some classes of equipment now above 260C (SOOF), are moving upward. Ambient low temperatures below -6SC (-8SF) are currently specified.Vibration conditions producing accelerations in excess of 60 G's exist. Environmental conditions which may deteriorate electrical insulation are present through a range and to a degree uncommon in the environment of non-aircraft electric equipment. These conditions have created problems which commercial insulation test procedures do not always cover adequately.AIEE No 803-1957AstrionicsAvionicsAstrionics.Avionics.629.474NjHacINjHaclDOCUMENT9910136507603321AIEE No 803-19573646538UNINA