CTHIn ForceLegislation
AD/CF6/31 - Fan Stator Case Stiffening Ring and Stage 1 Fan Shroud
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AD/CF6/31 - Fan Stator Case Stiffening Ring and Stage 1 Fan Shroud
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text General Electric Turbine Engines - CF6 Series
Applicability: General Electric CF6-45/-50 series engines.
Requirement: Action in accordance with the technical requirements of FAA AD 94-08-05.
Note: General Electric CF6-50 Service Bulletin 72-573 refers.
Compliance: As specified in the FAA AD with an effective date of 18 August 1994.
Background: The FAA AD was raised as a result of an uncontained stage one fan blade failure which resulted in an inflight engine shutdown and damage to the aircraft.