Gives electrical output characteristics, and interface requirements, between an aircraft and ground support electrical supplies. Requirements for safety features are also included. The facilities covered by this International Standard are intended to supply power to an aircraft. In some cases the facility may also be capable of being used for aircraft engine starting.
Текущий статус : WithdrawnДата публикации : 1982-08
Версия : 1Число страниц : 7
Технический комитет:Aerospace electrical requirements