AD/PA-32/2 - Rudder Trim Installation - Modification
1AD/PA-32/2 - Rudder Trim Installation - Modification
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Piper PA-32 (Cherokee Six) Series Aeroplanes
| AD/PA-32/2 | Rudder Trim Installation - Modification | 1/67 |
|---|---|---|
| Applicability: | All model PA-32-260 with S/Nos. 32-1 to 32-824. | |
| Document: | Piper SB No. 237. |
Compliance: Within 200 hours time in service after 15 January 1967 or before 31 March 1967 whichever occurs first.