FAA AD 2001-16-08 Fatigue Cracking Or Fracture Of The Steel Attachment Fittings Of The Diagonal Brace To The Nacelle Struts - Applicable to Boeing Model 747 Series Airplanes Equipped With General Electric Model CF6-45 Or -50 Series Engines Or Pratt And Wh. Формат поставки-PDF. Язык стандарта-Английский
Другие Стандарты FAA
FAA-E-2308 CONSOLE, AIR/GROUND, LOW PROFILE, MODULAR
FAA AD 2005-20-39 To Prevent Collapse Of The Mlg, Or Damage To Hydraulic Tubing Or The Aileron Co...
FAA AD 2009-20-13 To Ensure Replacement Of The Control Column Rod Ends With High-Strength Steel R...
FAA AD 2000-NM-52 Prevent Electrical Arcing Between the Oxygen Tubing and an Electrical Source Wh...
FAA AD 1999-07-02 Detect a Mislocated or Improperly Bonded Main Rotor Blade (Blade) Leading Edge ...
FAA AD 1997-07-06 Failure of the Steel Swashplate Support Assembly