AD/PA-34/22 - Fuselage Structure Rivets - Inspection
1AD/PA-34/22 - Fuselage Structure Rivets - 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-34/22 Fuselage Structure Rivets - Inspection 3/77
Applicability: All model PA-34-200 with S/Nos. 34-7250001 to 34-7450220. All model PA-34-200T with S/Nos. 34-7570001 to 34-7670292.
Document: Piper SB No. 545.
Compliance: Within 100 hours time in service after 31 May 1977.