AD/CHA/17 - Wing Strut and Spar Attachment Bolt

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B08543 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


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:

 

 

  1. 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.

 

2. 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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.