Commonwealth legislation

AD/BN-2/14 Amdt 2 - Flap Operating Lever - Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This airworthiness directive mandates modification of the flap operating lever on all Pilatus Britten‑Norman BN‑2 series aeroplanes per Britten‑Norman Modification Leaflet BN‑2/NB/M/417, to be completed within 100 hours' time‑in‑service after 30 November 1970. It obliges owners/operators to arrange the work (and bear related costs/downtime) but does not state the safety defect being corrected.

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Current sections

Direct links to the current provisions in AD/BN-2/14 Amdt 2 - Flap Operating Lever - Modification.

AD/BN-2/14 Amdt 2 - Flap Operating Lever - 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 Pilatus Britten-Norman BN-2 Series Aeroplanes

AD/BN-2/14

Amdt 2

Applicability: All models.

Flap Operating Lever - Modification NK

Document: Britten-Norman Modification Leaflet BN-2/NB/M/417. Compliance: Within 100 hours time in service after 30 November 1970.

Source text

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