FAA AD 2000-08-14 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, which could Result in Reduced Structural Integrity of the Wing-to-Body Jo
Наименование:
FAA AD 2000-08-14 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, which could Result in Reduced Structural Integrity of the Wing-to-Body Jo
Разработчик
FAA (Federal Aviation Administration (FAA))
Язык:
Английский
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