Airworthiness Directive

AD 2002-24-01 67 FR 71101

Federal Aviation Administration · 14 CFR part 39

FR document
02-30023
Amendment
39-12966
Published
2002-11-29
Models covered
1
Last live check
2026-08-17
AD

2002-24-01

FR doc 02-30023 · 67 FR 71101

AD 2002-24-01Published 2002-11-29Effective 2003-01-21

Requires you to repetitively inspect the rear 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 Britten Norman (Bembridge) Limited (Britten Norman) BN2A Mk. III series airplanes. This AD requires you to repetitively inspect the rear 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 rear engine-mounting frame, which could lead to engine mount failure. Such failure could result in separation of the engine from the airplane.

Applies to 1 model in our index