Commonwealth legislation

AD/DO-27/12 - Horizontal Tail Bearing Fitting Rivets

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

Owners/operators of all Dornier DO‑27 aircraft must, within 30 days of 9 Oct 1996, carry out the inspections/repairs specified in Daimler Benz Aerospace/Dornier Service Bulletin SB1140‑0000 addressing possible loosening of rivets at the horizontal tail bearing fitting. The operator arranges and pays for the work and downtime. The AD’s purpose is to mitigate rivet‑loosening risk and it cross‑references the related German LBA AD.

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AD/DO-27/12 - Horizontal Tail Bearing Fitting Rivets

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Dornier DO-27 Series Aeroplanes

AD/DO27/12 Horizontal Tail Bearing Fitting Rivets 13/96 DM

Applicability: All Series all Serial Numbers.

Requirement: Action in accordance with Daimler Benz Aerospace/Dornier SB1140-0000 dated 29 September 1995.

Note: LBA AD 96-271 refers.

Compliance: Within 30 days after 09 October 1996.

Background: Loosening of rivets is possible at the bearing flange, and “L” profile and profile of the frame.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.