Document ID: chunk:federal_register_of_legislation:F2006B10932:body:0
Version: federal_register_of_legislation:F2006B10932
Segment Type: other
Provision Reference: 
Character Range: 0–1167

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/61
 Amdt 2

 Wing/Fuselage Attachment 2/95

 Applicability: Model HP137 Mk1, Jetstream Series 200, and Jetstream Series 3100 aircraft.

            Requirement: Action in accordance with British Aerospace Mandatory Service Bulletin 57-JA 930941 Revision 2.
 Compliance: As specified in the requirement document with an effective date of 2 February 1995. Background:               Cracks and corrosion on the spigot housing plate at the wing/fuselage forward-
            attachment sliding-joint, have been reported on an in-service Jetstream 3100 aircraft. Amendment 1 split the inspection of the spigot from the inspection of the spigot housing plate in order to ease operator workload, and added new compliance instructions for repeat inspections.

            Amendment 2 is issued in response to a revision of the Requirement document which introduces several changes including an optional ultrasonic test and an extension of compliance.