AD/BEECH 90/61 - Pilot and Co-Pilot Seatback Pan - Modification

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

Legislation au F2006B04250 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 90 and 65-90 (King Air) Series Aeroplanes

 

AD/BEECH 90/61 Pilot and Co-Pilot Seatback Pan - Modification 7/81

Applicability: All models C90 with S/Nos. LJ-803 to LJ-956. All models E90 with S/Nos. LW-301 to LW-347. All models F90 with S/Nos. LA-2 to LA-125.

 

Document: Beechcraft SI No. 1176.

 

Compliance: Unless already accomplished, within 100 hours time in service after 31 July 1981.

 

Background:  There is a possibility that the shoulder harness could jam and cause slack in the assembly due to insufficient clearance in the seat 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.