AD/BEECH 95/21 - Fuselage Bulkheads FS 257.6 & FS 271.92

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

Legislation au F2006B04293 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

 


Beechcraft 95 (Travelair) Series Aeroplanes

 

AD/BEECH 95/21 Fuselage Bulkheads FS 257.6 & FS 271.92 4/79

Applicability: All models 95, B95, B95A, D95A and E95 with S/Nos TD-2 to TD-721. Requirement:               Action in accordance with Beechcraft SI No 0990.

Compliance: Initially inspect within 100 hours time in service after 30 April 1979 and thereafter at intervals not exceeding 500 hours’ time in service or 1 year, whichever occurs first.

 

Background: Cracks may develop in the subject bulkheads in the areas of the horizontal stabilator attachments.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.