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AD/PA-34/5 - Stabilator Tip Balance Weight - Inspection
1AD/PA-34/5 - Stabilator Tip Balance Weight - Inspection
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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-34 (Seneca) Series Aeroplanes
AD/PA-34/5 Stabilator Tip Balance Weight - Inspection 9/72
Applicability: All models with S/Nos. 34-E4 and 34-7250001 to 34-7250335. Document: Piper SB No. 367.
Compliance: 1. Initial Inspection - prior to further flight after 12 September 1972.
- Hardware Replacement - as detailed in requirement document.