FAA AD 2005-14-08 To Prevent Loss Of The Underwing Fitting Load Path Due To Missing Or Damaged Alloy-steel - Applicable to Boeing Model 747 Airplanes. Формат поставки-PDF. Язык стандарта-Английский
Наименование:
FAA AD 2005-14-08 To Prevent Loss Of The Underwing Fitting Load Path Due To Missing Or Damaged Alloy-steel - Applicable to Boeing Model 747 Airplanes
Разработчик
FAA (Federal Aviation Administration (FAA))
Язык:
Английский
Формат поставки:
PDF
Цена стандарта
по запросу
Срок поставки
по запросу
Другие Стандарты FAA
FAA AD 2005-14-08 To Prevent Loss Of The Underwing Fitting Load Path Due To Missing Or Damaged Al...
FAA AD 2009-20-13 To Ensure Replacement Of The Control Column Rod Ends With High-Strength Steel R...
FAA AD 1976-14-09 Inspection of Hollow Steel Blades
FAA AD 2009-CE-062 To Detect And Correct Inadequate Clearance Of The Brake Reservoir Tubing And Th...
FAA AD 2000-NM-302 Prevent Fatigue Cracking or Fracture of the Steel Attachment Fittings of the Di...
FAA AD 1989-23-07 Steel Bolts