FAA AD 2003-CE-67 To Detect, Correct, And Prevent Future Cracks In The Tubing For The Main Landing Gear Leg - Applicable to Ostmecklenburgische Flugzeugbau GmbH Model OMF-100-160 Airplanes. Формат поставки-PDF. Язык стандарта-Английский
Другие Стандарты FAA
FAA AD 2004-24-02 To Detect, Correct, And Prevent Future Cracks In The Tubing For The Main Landin...
FAA AD 2001-15-08 Ignition of Fuel Vapors Due to the Generation of Sparks and a Potential Ignitio...
FAA AD 1999-NM-56 Detect And Prevent Cracking Of The High Strength H-11 Steel Bolts On The Wing R...
FAA AD 2010-19-05 To Prevent Separation And Loss Of A Stainless Steel Ring (75 Millimeter (mm) In...
FAA AD 1997-NM-65 Prevent chafing of the galley power feeder and static ground wiring on passenge...
FAA AD 2001-NM-394 Broken H-11 Steel Bolts - Applicable to Boeing Model 747 Series Airplanes