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
Наименование:
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
Разработчик
FAA (Federal Aviation Administration (FAA))
Язык:
Английский
Формат поставки:
PDF
Цена стандарта
по запросу
Срок поставки
по запросу
Другие Стандарты FAA
FAA-C-2624 CONSTRUCTION OF AN AIRPORT SURVEILLANCE RADAR FACILITY (PREFABRICATED METAL BUILDING)
FAA AD 1995-ANE-45 Steel High Pressure Compressor (HPC) Disk
FAA AD 1958-24-01 Hollow Steel Propeller Blades
FAA AD 2011-NM-252 To Prevent Pitot-Static Tubing From Becoming Partially Or Completely Blocked By...
FAA AD 1998-03-13 Aluminum Oxygen Tubing Bursting and Releasing a High-Pressure Oxygen Flow into ...
FAA AD 1998-09-24 Failure Of Either The Shoulder Harness Fittings, Elevator Rib, Or The Wheel Axl...