AD/CF6/33 - HPT Stage 2 Disk Life Limits
1AD/CF6/33 - HPT Stage 2 Disk Life Limits
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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
AD/CF6/33 HPT Stage 2 Disk Life Limits 11/95
Applicability: CF6-50/-45 series.
Requirement: Action in accordance with the technical requirements of FAA AD 95-08-03.
Note: Refer to GE SB 72-1069.
Compliance: As specified in the Requirement Document.
Background: This AD is issued to reflect the manufacturer’s requirement to reduce the certified life of the HPT Stage 2 disk.