Commonwealth legislation

AD/SD3-60/46 - Inner Flap Sub-Assembly Lever Bracket

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This directive mandates inspections of the inner flap sub‑assembly lever bracket on all Short SD3‑60 aeroplanes, to be carried out exactly as specified in Shorts Mandatory Service Bulletin SD360‑27‑26, with an initial inspection by 19 September 1997 and recurring checks per the bulletin.

Issued after reports of corrosion and cracking, it affects all SD3‑60 owners/operators who must bear inspection and any corrective costs.

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AD/SD3-60/46 - 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 SD3-60 Series Aeroplanes

AD/SD3-60/46 Inner Flap Sub-Assembly Lever Bracket 7/97

Applicability: All SD3-60 aircraft.

Requirement: Inspect in accordance with Shorts Mandatory Service Bulletin SD360-27-26.

Note: UK CAA AD 011-01-97 refers.

Compliance: Unless already accomplished, before 19 September 1997 for the initial inspection; thereafter as specified in the requirement document.

This airworthiness directive becomes effective on 19 June 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.