AD/AT/6 Amdt 1 - Fuselage Fittings - Vertical Fin Front Spar Attachments - Inspection and Modification

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

Legislation au F2006B02555 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

 


Airtractor AT-300, 400 and 500 Series Aeroplanes

 

AD/AT/6

Amdt 1


Fuselage Fittings - Vertical Fin Front Spar Attachments - Inspection and Modification


11/83

 

Applicability: All models AT-300, AT-301, AT-302 with S/Nos. 0001 to 0240. Document:  1. Snow Engineering Co. Service Letter No. 26 and

2. Snow Engineering Co. Service Letter No. 47.

 

Note: FAA AD 83-18-01 refers.

 

Compliance: 1. Within 100 hours time in service after 31st July 1983 and thereafter at intervals not exceeding 100 hours time in service.

 

2. Modification - prior to 2000 hours time in service.

 

Background: The manufacturer reports that service history indicates cracking of attachment fittings. Amendment 1 of this AD details Snow Engineering Co. Service Letter No. 26 for the repetitive inspection and notes the issue of FAA AD 83-18-01.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.