Commonwealth legislation

AD/ROBIN/23 - Anti-Tab Control

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD requires owners/operators of Avions Pierre Robin R2000 and HR200 aeroplanes (S/N 250–271) to install a friction lock on the anti‑tab sliding stop tube per Mandatory Service Bulletin 137 within 100 flight hours of 22 June 1995. Maintenance organisations must carry out the work to the manufacturer’s method.

It shifts parts, labour and downtime costs to owners/operators in exchange for an asserted (unquantified) improvement in anti‑tab control operation; the CAA enforces compliance.

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AD/ROBIN/23 - Anti-Tab Control

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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 Robin Aviation Series Aeroplanes

AD/ROBIN/23 Anti-Tab Control 7/95

Applicability: All Model R 2000 and HR 200 aircraft, serial numbers 250 through 271. Requirement: Action in accordance with Avions Pierre Robin Mandatory Service Bulletin 137.

Note: DGAC AD 94-183(A)R1 refers.

Compliance: Unless already accomplished, within 100 hours time in service after 22 June 1995.

Background: The DGAC requires installation of a friction lock device on the sliding stop tube in order to improve the operating condition of the anti-tab control.

Source text

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