AD/JETSTREAM/66 - Wing - Main Spar Fuel Fitting Attachment Holes

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Legislation au F2006B10936 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/66  Wing - Main Spar Fuel Fitting Attachment Holes

Applicability: Jetstream 3200 Series aircraft up to and including constructor’s number 950.


10/94

 

Requirement: Modify the fuel tank drainage hole at wing station 64.8 on the left and right hand sides in accordance with British Aerospace SB 57-JM 8175 revision 1.

 

Compliance: Prior to 6000 landings or before 15 March 1995 whichever is the later.

 

Background: Cracking of the wing main spar webs has been found at this location on the Jetstream 3200 series wing test specimen.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.