AD/CESSNA 185/7 Amdt 1 - Wing Main Spar and Lower Skin

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

Legislation au F2006B05142 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

 


Cessna 185 Series Aeroplanes

 

AD/CESSNA 185/7

Amdt 1


Wing Main Spar and Lower Skin 10/67

 

Applicability: All models in agricultural category.

 

Requirement: Carry out a visual inspection for cracking of the wings in the following areas:

 

  1. The corners of the skin cutouts through which the lift strut fork passes.

 

2.    All visable elements of the main spar lower flange front and rear faces in the region of the lift strut attachment.

 

Pay particular attention to the areas around the spar to skin rivets. The affected areas must be thoroughly cleaned before inspection.

 

Compliance: Before 4000 hours total time in service on wings and thereafter at intervals not exceeding 100 hours time in service.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.