AD/BEECH 90/62 - Horizontal Stabiliser Forward Spar Web Rivets - Inspection

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

Legislation au F2006B04251 Not 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 90 and 65-90 (King Air) Series Aeroplanes

 

AD/BEECH 90/62 Horizontal Stabiliser Forward Spar

Web Rivets - Inspection

Applicability: All model F90 with S/Nos. LA-2 to LA-101. Document:  Beechcraft SI No. 1192.


10/81

Compliance: 1. For those aeroplanes which have achieved 2000 hours’ time in service inspect within 100 hours’ time in service after 31 October 1981 and thereafter at intervals not exceeding 500 hours’ time in service.

 

2. For those aeroplanes which have not achieved 2000 hours’ time in service, inspect before achieving 2000 hours’ time in service and thereafter at intervals not exceeding 500 hours’ time in service.

 

Background: It is possible that looseness could develop in the horizontal stabiliser forward spar web rivets during normal 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.