AD/BEECH 200/17 - Nacelle Wheel Well Fender Installation
1AD/BEECH 200/17 - Nacelle Wheel Well Fender Installation
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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 Beechcraft 200 (Super King Air) Series Aeroplanes
AD/BEECH 200/17 Nacelle Wheel Well Fender Installation 7/77
Applicability: All model 200 with high flotation landing gear installations up to S/No BB-188. Requirement: Action in accordance with Beechcraft SI No 0897.
Compliance: 1. Inspect within 100 hours time in service after 31 July 1977 and thereafter at intervals not exceeding 100 hours time in service until modified.
- Modify before achieving 500 hours time in service.