AD/PT6A/12 - Improved Wire Rope Reversing Cable
1AD/PT6A/12 - Improved Wire Rope Reversing Cable
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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 Canada Turbine Engines - PT6A Series
AD/PT6A/12 Improved Wire Rope Reversing Cable 10/85
Applicability: All PT6A-27 engines prior to S/N PC-E40273 except E40028, 40029, 40144, 40157, 40186, 40187, 40226, 40228, 40229 and 40241 to 40247, and PT6A-28 engines prior to S/No. PC-E50027.
Document: 1. UACL SB No. 173, Rev. 2; or
2. UACL SB No. 1126; or
3. AD/UAC-T/10A.
Compliance: Before installation in an aircraft following next reconditioning completed after 31 December 1971.
Note: The above AD number has been corrected with the addition of the letter “A” which had been inadvertently omitted from previous up-dates.