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AD/CHA/17 - Wing Strut and Spar Attachment Bolt
1AD/CHA/17 - Wing Strut and Spar Attachment Bolt
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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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American Champion (Aeronca, Bellanca) Series Aeroplanes
| AD/CHA/17 | Wing Strut and Spar Attachment Bolt | 11/77 |
|---|---|---|
| Applicability: | All model 8GCBC and 8KCAB. | |
| Requirement: | Retire from service: |
The front and rear wing strut upper and lower attachment bolts.
2. The front and rear wing spar to fuselage attachment bolts.
Compliance: 1. For aircraft which have achieved 1000 hours time in service: within 200 hours time in service after 30 November 1977 and thereafter at intervals not exceeding 1200 hours time in service.
- For all other Aircraft: at intervals not exceeding 1200 hours time in service.
Note: For 8KCAB aircraft each hour engaged in aerobatics shall be counted as equivalent to 10 hours normal flight.