Commonwealth legislation

AD/F28/62 - Aileron Dual Input Quadrant Bracket

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

Applies to specific Fokker F28 aircraft (serials 11003–11241, 11991–11992): owners/operators must perform the inspections and corrective work described in Fokker Service Bulletin F28/27-177, addressing severe pitting corrosion on aileron dual input quadrant brackets and incorrect bushing installations.

Work must be completed by 30 April 1991 (unless already done). The directive creates a one‑time compliance task and is enforced by the Civil Aviation Safety Authority; operators bear cost and scheduling responsibility.

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AD/F28/62 - Aileron Dual Input Quadrant 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 Fokker F28 Series Aeroplanes

AD/F28/62 Aileron Dual Input Quadrant Bracket 13/90

Applicability: F28 aircraft with S/Nos 11003 through 11241, 11991 and 11992. Requirement: Action in accordance with Fokker SB F28/27-177.

Note: AD BLA 90-097 refers.

Compliance: Prior to 30 April 1991, unless previously accomplished.

Background: Country of origin AD. Severe pitting corrosion on the mounting brackets has been reported, together with incorrect installation of bushings.

Source text

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