Document ID: chunk:federal_register_of_legislation:F2006B06015:body:0
Version: federal_register_of_legislation:F2006B06015
Segment Type: other
Provision Reference: 
Character Range: 0–1034

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

 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.