Commonwealth legislation

AD/BN-2/30 - Six Degree Droop Flap Micro-Switch Setting - Inspection

In ForceCTH

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Commonwealth

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legislative instrument

Plain English Summary

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This AD mandates that BN‑2 series aircraft fitted with Modification NB/M/430 have the six‑degree droop‑flap micro‑switch setting inspected per Britten Norman SB No. BN‑2/SB.66 within 100 hours time‑in‑service after 28 February 1974. Operators bear the inspection and any corrective costs; work must be done by qualified maintenance personnel to maintain regulatory compliance.

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AD/BN-2/30 - Six Degree Droop Flap Micro-Switch Setting - Inspection

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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-2/30 Six Degree Droop Flap Micro-Switch

Setting - Inspection Applicability: All models with drooped flaps (Modification NB/M/430). Document: Britten Norman SB No. BN-2/SB.66.

Compliance: Within the next 100 hours time in service after 28 February 1974.

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Source text

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