1AD/PA-34/35 - Fuselage Structure, LH Side Sta.108 - 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-34 (Seneca) Series Aeroplanes

 

AD/PA-34/35  Fuselage Structure, LH Side Sta.108 - Inspection and Modification

5/81

 

Applicability: All models PA-34-220T Seneca 111 with S/Nos. as listed in Piper SB No. 711. Document:               Piper SB No. 711.

Compliance: Part 1 - Unless already accomplished, within 5 hours time in service after 28 May 1981.

 

Part 2 - Within 100 hours time in service after 28 May 1981.

 

Background: It has been determined by the manufacturer that during assembly twelve (12) rivets were deleted at the subject fuselage location.