AD/BEECH 400/4 - Fuselage Rivets

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

Legislation au F2006B03931 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

 


Beechcraft 400 Series Aeroplanes

 

AD/BEECH 400/4 Fuselage Rivets 13/93

Applicability: Model 400A with serial numbers RK-1 through RK-41. Model 400T with serial numbers TT-3 through TT-20.

Requirement: Action in accordance with Beechcraft Mandatory Service Bulletin 2482.

 

Note: FAA AD 93-16-12 Amdt 39-8670 refers.

 

Compliance: Within 100 hours time in service after 9 December 1993.

 

Background: The FAA received reports that during manufacture, rivets may have been inadvertently omitted from the area adjacent to the upper edge of the emergency exit door.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.