AD/JETSTREAM/16 Amdt 2 - Main Landing Gear Doors

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

Legislation au F2006B10883 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/16

Amdt 2


Main Landing Gear Doors 7/95

 

Applicability: HP 137 Mk 1, Jetstream Series 200 and Jetstream Series 3100 aircraft, constructors numbers 601 through 695.

 

Requirement: Action in accordance with Jetstream Alert Service Bulletin 32-A-JA840318 Revision 2.

 

Compliance: Within 200 landings after 30 November 1986, and thereafter at intervals not to exceed 1000 landings, until modified in accordance with Jetstream Service Bulletin

32-JM5280.

 

The compliance of the previous issue of this directive remains unchanged. This amendment is effective from 22 June 1995.

Background: Cases have been reported of the failure of rod end bearings, bending of rod shanks, cracking of rod threads, cracking of door hinges and door loss. Amendment 1 provided for terminating action.

 

Amendment 2 is issued in response to a revision of the requirement document which amends the instructions for non-destructive testing of the hinges on the main landing gear doors.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.