AD/PA-32/53 - Engine Control Rod End Bearings - Inspection and Replacement
1AD/PA-32/53 - Engine Control Rod End Bearings - Inspection and Replacement
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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Piper PA-32 (Cherokee Six) Series Aeroplanes
AD/PA-32/53 Engine Control Rod End Bearings - Inspection
and Replacement
12/77
Applicability: Models PA32-260 with S/Nos. 32-1111 to 32-7700013. PA32-300 with S/Nos. 32- 40566 to 32-7740040. PA32R-300 with S/Nos. 32R-7680001 to 32R-7780215.
Requirement: 1. Inspect the rod end bearing assemblies attached to the mixture, throttle and propeller governor control cables for comparison with the illustration.
- If a rod end bearing is installed as identified in the illustration as number one (1), it should be replaced with a rod end bearing corresponding to number two (2) or number three (3) of the illustration.
Compliance: Within 25 hours time in service after 22 November 1977.
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES