Federal Register of Legislation
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/29 Amdt 5
Flap Torque Tube Universal Joints 13/93
Applicability: All HP137 Mk1, Jetstream Series 200, and Jetstream Series 3100 aircraft.
All Jetstream Series 3200 aircraft up to and including constructors number 956.
Requirement: Action in accordance with British Aerospace Mandatory Service Bulletins 27-A-JA 881041 Revision 2 and 27-JM 5313 Revision 2, or 27-JM 5322.
Note: Accomplishment of Part 1 or Part 2 of BAe SB 27-JA920340, constitutes terminating action for the requirements of this Directive.
Compliance: As specified in the requirement documents, with flying hours to count from previous certified compliance; until accomplishment of Part 1 or Part 2 of British Aerospace Service Bulletin 27-JA920340.
This amendment is effective from 9 December 1993.
Background: A failure of the flap torque shaft universal joint securing rivet occurred.
This condition could have resulted in asymmetric flap deployment. Amendment 1 introduced an alternative modification (JM 5322) to suit a different joint configuration, and required inspection of joints that had already been modified. Amendment 3 upgraded 27-JM5313 to Rev 2 which revised a periodicity. Amendment 4 included the 3200 series.
Amendment 5 is issued to introduce optional terminating action for this directive.
We try to embed the page this law was scraped from. If the site blocks framing, you still get the link and a local excerpt.
Last checked with source on —
Checking whether the official page can be embedded…
Plain-English simplify of this law: a short summary, key points, and both sides of the argument. Generated on first view via Replicate, then cached. Vote on what helps your study.
No study brief is cached for this law yet. Sign up to generate a plain-English brief.
Sign up to generate