AD/CF6/31 - Fan Stator Case Stiffening Ring and Stage 1 Fan Shroud

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Legislation au F2006B08474 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


General Electric Turbine Engines - CF6 Series

 

AD/CF6/31 Fan Stator Case Stiffening Ring and Stage 1 Fan Shroud

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.


9/94

 

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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.