1AD/PA-32/71 - Aileron Balance Weight Attachment - Inspection and Modification

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

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Piper PA-32 (Cherokee Six) Series Aeroplanes

AD/PA-32/71 Aileron Balance Weight Attachment - Inspection

and Modification

5/81

Applicability: All model PA-32-301 with S/Nos. 32-8006002 to 32-8006106. All model PA-32- 301T with S/Nos. 32-8024001 to 32-8024052 All model PA-32R-301 with S/Nos. 32R-8013001 to 32R-8013139.

All model PA-32R-301T with S/Nos. 32R-8029001 to 32R-8029110.

Document: Piper SB No. 703.

Compliance: Part 1 - Within 25 hours time in service after 7 April 1981 and thereafter at intervals not exceeding 25 hours time in service until modified in accordance with Part II.

Part II - Within 200 hours time in service after 7 April 1981.

Background: The Manufacturer has received reports of aileron balance weights becoming loose in the outboard leading edge of the ailerons.