AD/PA-34/24 - Engine Control Rod End Bearings - Inspection and Replacement
1AD/PA-34/24 - 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-34 (Seneca) Series Aeroplanes
AD/PA-34/24 Engine Control Rod End Bearings - Inspection
and Replacement
11/77
Applicability: Models PA34-200 with S/Nos. 34-7250001 to 34-7450220. PA34-200T with S/Nos.
34-7570001 to 34-7770163.
Requirement: 1. Inspect the rod end bearing assemblies attached to the mixture, throttle and propeller governor control cables for comparison.
- If a rod end bearing is installed as identified in the illustration as number one (1), it shall 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.
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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