CTHRepealedLegislation
AD/PA-42/3 - Tail Fin/Fuselage, Rivet Installation - Replacement
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AD/PA-42/3 - Tail Fin/Fuselage, Rivet Installation - Replacement
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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-42 (Cheyenne III) Series Aeroplanes
AD/PA-42/3 Tail Fin/Fuselage, Rivet Installation - Replacement 9/83
Applicability: All model PA-42 with S/Nos. listed in Piper Service Bulletin No. 765. Document: Piper S.B. No. 765.
Compliance: Within 100 hours time in service after 30th September 1983.
Background: Field reports indicate that the rivets at the intersection of the tail fin/fuselage drag angle and tail fin front spar are working loose.