AD/CESSNA 188/33 - Wing Front Spar, Boom Attach Holes

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

Legislation au F2006B05169 Not in force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Cessna 188 (Agwagon) Series Aeroplanes

 

AD/CESSNA 188/33 Wing Front Spar, Boom Attach Holes 4/80

Applicability: All model 188 with S/Nos. 18801178 to 18802057. Requirement:  Action in accordance with Cessna SIL No. SE80-18. Compliance:               Within 100 hours time in service after 30 April 1980.

Background: The boom attach holes in the front spar lower front flange may wear in service causing elongation and/or oversizing of the holes.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Interactions

Authorises

All Versions

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.