AD/PA-38/14 - Control Column Installation - Modification
1AD/PA-38/14 - Control Column 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-38 (Tomahawk) Series Aeroplanes
AD/PA-38/14 Control Column Installation - Modification 11/79
Applicability: All models PA-38-112 with S/Nos. 38-78A0001 to 38-79A1160. Document: Piper SB No. 661.
Compliance: Unless already accomplished, within 100 hours time in service after 30 November 1979.
Background: It has been reported to the manufacturer that roughness or binding of the control shaft in the instrument panel can occur at the extremes of control movement.