AD/PC-6/30 - Anti-Reverse System - Modification
1AD/PC-6/30 - Anti-Reverse System - 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 Pilatus Porter PC-6 Series Aeroplanes
AD/PC-6/30 Anti-Reverse System - Modification 11/70
Applicability: All model PC-6/B1-H2 with S/Nos prior to 726.
Requirement: 1. Modify anti-reversing circuit as per para 2.21 of Pilatus SB No. 101.
2. Test anti-reversing valve as per para 2.1 of Pilatus SN No. 101.
3. Function test anti-reversing system as per para 2.22 of Pilatus SB No. 101. Compliance: For Para. 1 - within 100 hours time in service after 31 December 1970.
For Paras. 2 and 3 - Within 100 hours time in service after 31 December 1970 and thereafter at intervals not exceeding 100 hours time in service.