AD/AT/13 - Wing Spar Cap Corrosion

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

Legislation au F2006B02542 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Airtractor AT-300, 400 and 500 Series Aeroplanes

 

AD/AT/13 Wing Spar Cap Corrosion 7/92

Applicability: Models AT-300, AT-301, & AT-302 with S/N’s 300-0001 through 301-0688; Model AT-400 with S/N’s 400-0244 through400-0415; & Model AT-400A all S/N’s.

 

Requirement: Action in accordance with Air Tractor Inc. Service Letter No. 90.

 

Note: FAA AD 92-07-14 Amdt 39-8210 refers.

 

Compliance: Prior to 30 September 1992; and thereafter at intervals not to exceed 12 calendar months.

 

Background:  The FAA has received three reports of badly corroded wing spar caps on the affected aircraft. The actions specified by this Directive are intended to prevent failure of the wing structure.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.