Airworthiness Directive

AD 2002-02-10 67 FR 6388 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-2946
Amendment
39-12638
Published
2002-02-12
Effective
2002-03-25
Models covered
1
Last live check
2026-10-01
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AD

2002-02-10

FR doc 02-2946 · 67 FR 6388

AD 2002-02-10Published 2002-02-12Effective 2002-03-25

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 inboard brackets of the elevator outboard hinge for loose rivets, structural damage, or cracks and replace any suspect bracket.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Pilatus Britten-Norman Limited (Pilatus Britten- Norman) BN-2, BN-2A, BN-2B, and BN-2T series airplanes. This AD requires you to repetitively inspect the inboard brackets of the elevator outboard hinge for loose rivets, structural damage, or cracks and replace any suspect bracket. This AD also requires you to replace the hinge bracket at a certain time period if no discrepancies are found. This replacement includes modifying this area and installing modified brackets. This replacement allows you to increase the time period between inspections (reduce the number of repetitive inspections). 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 inboard brackets of the elevator outboard hinge with loose rivets, structural damage, or cracks. Such conditions could cause the outboard elevator to become loose with a consequent reduction in elevator and airplane control.

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All Britten-Norman BN-2 Islander directives

Applies to 1 model in our index