AD/JETSTREAM/59 - Main Wing Lower Skin and Lower Front Spar Structure

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

Legislation au F2006B10929 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

 


British Aerospace BAe 3100 (Jetstream) Series Aeroplanes

 

AD/JETSTREAM/59  Main Wing Lower Skin and Lower Front Spar Structure

Applicability: All Jetstream Series 3100 aircraft.


9/93

 

Requirement: Action in accordance with British Aerospace Jetstream Mandatory Service Bulletin 57-JA 921203.

 

Note: UK CAA AD 014-05-93 refers.

 

Compliance: As specified in the Requirement Document, with a completion date of 19 February 1994 for Accomplishment Instructions Parts 1 and 2 of the Requirement Document.

 

Background: Reports of exfoliation corrosion damage of the lower main skin at bolts which attach the skin to the front spar structure between Stations 36 and 40, LH and RH.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.