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AD/PA-44/9 - Aileron Balance Weight Attachment Inspection and Modification
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AD/PA-44/9 - Aileron Balance Weight Attachment 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
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Piper PA-44 (Seminole) Series Aeroplanes
AD/PA-44/9 Aileron Balance Weight Attachment
Inspection and Modification
10/81
Applicability: All models PA-44-180 with serial numbers 44-7995001 to 44-8195016. All models PA-44-180T with serial numbers 44-8107001 to 44-8107044.
Document: Piper S.B. No. 725A. FAA AD 81-16-10 refers.
Compliance: Part I: Initially inspect before further flight and thereafter at intervals not exceeding 25 hours time in service until modified in accordance with Piper S.B. No.
725A.
Note: The pilot in command may perform and certify for this inspection.
Part II: Within 200 hours time in service after 21 August 1981.
Background: It is possible that the aileron balance weights may become loose in the outboard leading edge of the aileron.