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
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
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PDF
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