FAA AD 1999-NM-56 Detect And Prevent Cracking Of The High Strength H-11 Steel Bolts On The Wing Rear Spar Side-of-body On The Lower Chord Splice Plate And Kick Fitting Due To Stress Corrosion
Наименование:
FAA AD 1999-NM-56 Detect And Prevent Cracking Of The High Strength H-11 Steel Bolts On The Wing Rear Spar Side-of-body On The Lower Chord Splice Plate And Kick Fitting Due To Stress Corrosion
Разработчик
FAA (Federal Aviation Administration (FAA))
Язык:
Английский
Формат поставки:
PDF
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