Commonwealth legislation

AD/AC/59 Amdt 1 - Flap System - Flap Control Bracket - Inspection and Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Airworthiness Directive requires operators of Twin Commander 685, 690 and 690A aeroplanes identified in Rockwell Service Bulletin No. 157A to inspect and, if necessary, modify the flap control bracket in accordance with that service bulletin. Owners/operators and their maintenance organisations must complete the work within 100 hours’ time in service after 31 December 1979 unless it has already been done; the aircraft owner bears the cost and must follow the Rockwell SB technical instructions.

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AD/AC/59 Amdt 1 - Flap System - Flap Control Bracket - Inspection and Modification

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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 Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes

AD/AC/59

Amdt 1

Flap System - Flap Control Bracket - Inspection and Modification

12/79

Applicability: All 685, 690 and 690A with S/Nos. referenced in Rockwell SB No. 157A. Document: Rockwell SB No. 157A.

Compliance: Unless already accomplished, within 100 hours’ time in service after 31 Dec 1979.

Source text

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

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