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Airworthiness Directive

AD 2002-24-09 67 FR 75812 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to repetitively inspect the left and right engine-mounting frame for cracks and replace the frame if cracks are found.

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FR document
02-30686
Amendment
39-12974
Published
2002-12-10
Effective
2003-01-27
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2002-24-09 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2002-24-09

FR doc 02-30686 · 67 FR 75812

AD 2002-24-09Published 2002-12-10Effective 2003-01-27

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires you to repetitively inspect the left and right engine-mounting frame for cracks and replace the frame if cracks are found.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Pilatus Britten-Norman Limited (Pilatus Britten-Norman) BN2T and BN2T-4R series airplanes. This AD requires you to repetitively inspect the left and right engine-mounting frame for cracks and replace the frame if cracks are found. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the United Kingdom. The actions specified by this AD are intended to detect and correct cracks in the left and right engine- mounting frame, which could lead to engine mount failure. Such failure could result in separation of the engine from the airplane.

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All Britten-Norman BN-2 Islander directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index