AD/JT8D/11 - First Stage Fan Hubs
1AD/JT8D/11 - First Stage Fan Hubs
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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 Pratt and Whitney Turbine Engines - JT8D Series
AD/JT8D/11 First Stage Fan Hubs 4/77
Applicability: All JT8D-1, -1A, -1B, -7, -7A and -7B engines fitted with front compressor front hub P/N 504101 with S/Nos. listed in Table 1 of PWA Alert SB No. 4661 which have accumulated 6000 cycles or more in service.
Document: 1. FAA AD 77-03-06 : Amendment 39-2828; or
- AD/PW-T/42.
Compliance: As detailed in the Requirement Document.