Airworthiness Directive

AD 2006-23-03 71 FR 65714 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E6-18723
Amendment
39-14815
Published
2006-11-09
Effective
2006-12-14
Models covered
1
Last live check
2026-10-01
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AD

2006-23-03

FR doc E6-18723 · 71 FR 65714

AD 2006-23-03Published 2006-11-09Effective 2006-12-14

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 inspect the horizontal stabilizer attachment bolts and anchor nuts for damage and wear and replace damaged and/or worn parts with new, modified parts.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for all B-N Group Ltd. BN-2, BN-2A, BN-2B, BN-2T, and BN-2T-4R series (all individual models included in Type Certificate Data Sheet (TCDS) A17EU, Revision 16, dated December 9, 2002) airplanes. This AD requires you to inspect the horizontal stabilizer attachment bolts and anchor nuts for damage and wear and replace damaged and/or worn parts with new, modified parts. If no damaged or worn parts are found during the inspection, this AD requires you to replace the horizontal stabilizer attachment bolts and anchor nuts at a specified time with new, modified parts. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the United Kingdom. We are issuing this AD to detect and correct damaged and/or worn horizontal stabilizer attachment bolts and anchor nuts, which could result in failure of the horizontal stabilizer. This failure could result in loss of control.

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  3. AD 2021-18-01 Airworthiness Directives; B-N Group Ltd. Airplanes 2021-09-09
  4. AD 2016-26-09 Airworthiness Directives; B-N Group Ltd. Airplanes 2017-01-05
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All Britten-Norman BN-2 Islander directives

Applies to 1 model in our index