Commonwealth legislation

AD/EMB-110/23 - Trim Tab Control Systems - Inspection and Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This airworthiness directive mandates inspections and modifications of the trim tab control system on specified Embraer EMB-110 serial numbers, following Embraer Service Bulletin No. 110-27-062 Parts I & II. It responds to a risk that attaching nuts on trim actuating rods may loosen.

Operators of the affected aircraft must comply within short prescribed timeframes, bearing the cost and managing resulting downtime.

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AD/EMB-110/23 - Trim Tab Control Systems - 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 Embraer EMB-110 (Bandeirante) Series Aeroplanes

AD/EMB-110/23 Trim Tab Control Systems - Inspection

and Modification

Applicability: All models EMB-110 with S/Nos. 110001 to 110364 and 110366 to 110384. Document: Embraer SB No. 110-27-062 Parts I and II.

Note: Brazilian AD 82-11-03 refers.

Compliance: PART 1: Within 25 hours time in service after 25 January 1983.

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PART II: Within 125 hours time in service or one month, whichever occurs first, after 25 January, 1983.

Background: Investigation by the manufacturer revealed that the attaching nuts of the actuating rod ends of the trim cab systems may become loose.

Source text

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