AD/PC-6/25 Amdt 1 - Aileron Balance Weight Arms - Inspection
1AD/PC-6/25 Amdt 1 - Aileron Balance Weight Arms - 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 Pilatus Porter PC-6 Series Aeroplanes
AD/PC-6/25
Amdt 1
Aileron Balance Weight Arms - Inspection 11/72
Applicability: All models fitted with aileron mass balance weight assembly P/No. 6106.11. Document: Pilatus SB No. 89A.
Compliance: Within 100 hours time in service after 30 November 1972 and there- after at intervals not exceeding 100 hours time in service until replaced by aileron balance weight assembly P/No. 111.45.08.001.