Commonwealth legislation

AD/HS 125/108 - Flap Inboard Hinge

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Civil Aviation Safety Authority airworthiness directive requires British Aerospace BAe 125 aeroplanes listed in a separate Requirement Document to carry out the action specified in Hawker Siddeley Service Bulletin SB 27-112.

It aims to reduce flap damage from landings on heavily watered or slush‑covered runways; applicability, compliance timing and practical details are defined in the Requirement Document and the service bulletin.

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Current sections

Direct links to the current provisions in AD/HS 125/108 - Flap Inboard Hinge.

AD/HS 125/108 - Flap Inboard Hinge

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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 British Aerospace BAe 125 Series Aeroplanes

AD/HS 125/108 Flap Inboard Hinge 8/90

Applicability: As listed in the Requirement Document.

Requirement: Action in accordance with Hawker Siddeley SB 27-112. Compliance: In accordance with the Requirement Document.

Background: This Directive is to reduce the possibility of flap damage when landing on heavily watered or slush covered runways.

Source text

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