FAA AD 2004-24-02 To Detect, Correct, And Prevent Future Cracks In The Tubing For The Main Landing Gear Leg - Applicable to Ostmecklenburgische Flugzeugbau GmbH ModelOMF-100-160 Airplanes. Формат поставки-PDF. Язык стандарта-Английский
Другие Стандарты FAA
FAA-E-2391 TRANSMISSOMETER SUPPORT TOWER ASSEMBLY
FAA AD 1998-03-13 Aluminum Oxygen Tubing Bursting and Releasing a High-Pressure Oxygen Flow into ...
FAA AD 2008-NM-193 To Prevent Loss Of The Fairing Panels To Be Due To Failure Of Certain Steel Gro...
FAA AD 1956-19-02 Steel Propeller Blades
FAA AD 2009-SW-34 To Prevent Separation And Loss Of A Stainless Steel Ring (75 Millimeter (mm) In...
FAA AD 2013-03-17 To Prevent Failure Of The HPT Stage 1 And Stage 2 Discs