FAA AD 2012-23-11 To Prevent Cracking In The Rotary Rudder Boom Or Pylon Due To Fatigue, Failure From Static Overload, And Subsequent Loss Of Control Of The Helicopter. Формат поставки-PDF. Язык стандарта-Английский
Наименование:
FAA AD 2012-23-11 To Prevent Cracking In The Rotary Rudder Boom Or Pylon Due To Fatigue, Failure From Static Overload, And Subsequent Loss Of Control Of The Helicopter
Разработчик
FAA (Federal Aviation Administration (FAA))
Язык:
Английский
Формат поставки:
PDF
Цена стандарта
по запросу
Срок поставки
по запросу
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