Commonwealth legislation

AD/SD3-30/32 - Inner Flap Sub-Assembly Lever Bracket

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD requires owners/operators of SD3-30 aeroplanes to inspect the inner flap sub‑assembly lever bracket per the manufacturer’s Mandatory Service Bulletin SD3‑27‑36, with the first inspection due before 27 July 1997 and repeat intervals as set in the bulletin. Issued because corrosion and cracking have been reported, it forces operators to incorporate these inspections into maintenance programmes and bear any inspection and repair costs.

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AD/SD3-30/32 - Inner Flap Sub-Assembly Lever Bracket

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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 Short SD3-30 Series Aeroplanes

AD/SD3-30/32 Inner Flap Sub-Assembly Lever Bracket 5/97

Applicability: All SD3-30 aircraft.

Requirement: Inspect in accordance with Shorts Mandatory Service Bulletin SD3-27-36.

Compliance: Before 27 July 1997 for the initial inspection; thereafter as specified in the Requirement Document for the repeat inspection periods.

This Airworthiness Directive becomes effective on 24 April 1997.

Background: The manufacturer received reports of corrosion and cracking on inner flap sub- assembly lever brackets.

Source text

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