AD/PA-28/43 - Rudder Bar Assembly - Inspection and Modification
1AD/PA-28/43 - Rudder Bar Assembly - Inspection and 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-28 Series Aeroplanes
AD/PA-28/43 Rudder Bar Assembly - Inspection and Modification 12/73
Applicability: All model PA-28 and PA-28R. Document: Piper SL No. 671.
Compliance: Inspect within 100 hours time in service after 31 December 1973 and thereafter at intervals not exceeding 100 hours time in service until modified. Modify in accordance with SL No. 671 not later than first major inspection after 31 December 1973.