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2006-23-03: Horizontal stabilizer attachment bolts

FAA order 2006-23-03 is an airworthiness directive in force since December 14, 2006. The FAA's subject line: Horizontal stabilizer attachment bolts. It names Britten-Norman BN-2, Pilatus Britten-Norman Ltd. BN-2: about 67 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: airframe structure.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
B-N Group Ltd.
Models
BN-2, BN-2A, BN-2A-2, BN-2A-20, BN-2A-21, BN-2A-26, BN-2A-27, BN-2A-3, BN-2A-6, BN-2A-8, BN-2A-9, BN-2B-20, BN-2B-21, BN-2B-26, BN-2B-27, BN-2T, BN-2T-4R
On this site
Britten-Norman BN-2 54 registered
Pilatus Britten-Norman Ltd. BN-2 13 registered

Dates and paperwork

In force since
December 14, 2006
Published
November 9, 2006 (signed October 30, 2006)
Docket
FAA-2006-25668
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

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.

The order itself the regulatory text, as published

Show the full text (4,669 characters)
2006-23-03 B-N Group Ltd: Amendment 39-14815; Docket No. FAA-2006- 25668; Directorate Identifier 2006-CE-44-AD. Effective Date (a) This AD becomes effective on December 14, 2006. Affected ADs (b) None. Applicability (c) This AD applies to all 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; that are certificated in any category. Unsafe Condition (d) This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the United Kingdom. The actions specified in this AD are intended 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. Compliance (e) To address this problem, you must do the following, unless already done: Actions Compliance Procedures (1) Inspect the horizontal stabilizer attachment bolts and anchor nuts for damage and wear. Within the next 50 hours time-in-service (TIS) or 2 months, whichever occurs first, after December 14, 2006 (the effective date of this AD). Follow B-N Britten-Norman Aircraft Limited Service Bulletin number SB 302, Issue 2, dated April 12, 2005. (2) If you find any damaged or worn horizontal stabilizer attachment bolts and/or anchor nuts during the inspection required in paragraph (e)(1) of this AD, replace with new, modified horizontal stabilizer attachment bolts as specified in the service information (or FAA-approved equivalent part). Before further flight after the inspection required in paragraph (e)(1) of this AD. Follow B-N Britten-Norman Aircraft Limited Service Bulletin number SB 302, Issue 2, dated April 12, 2005. Do any necessary replacements following B-N Group Ltd. Modification Leaflet for Mod NB-M-1787, Issue 1, dated August 1, 2005.(3) If you do not find damaged or worn horizontal stabilizer attachment bolts and/or anchor nuts during the inspection required in paragraph (e)(1) of this AD, replace the horizontal stabilizer attachment bolts and anchor nuts with new, modified horizontal stabilizer attachment bolts as specified in the service information (or FAA-approved equivalent part). Upon accumulating 1,000 hours TIS after the inspection required in paragraph (e)(1) of this AD. Follow B-N Group Ltd. Modification Leaflet for Mod NB-M-1787, Issue 1, dated August 1, 2005. (4) You may replace the horizontal stabilizer attachment bolts and anchor nuts with the new, modified horizontal stabilizer attachment bolts as specified in the service information (or FAA-approved equivalent part) at any time, but no later than the applicable times specified in paragraphs (e)(2) and (e)(3) of this AD. After installing the new, modified horizontal stabilizer attachment bolts, no further action is required. As of December 14,2006 (the effective date of this AD). Follow B-N Group Ltd. Modification Leaflet for Mod NB-M-1787, Issue 1, dated August 1, 2005. Alternative Methods of Compliance (AMOCs) (f) The Manager, Standards Staff, FAA, Small Airplane Directorate, ATTN: Albert J. Mercado, Aerospace Engineer, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329- 4119; fax: (816) 329-4090, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Related Information (g) MCAI United Kingdom Civil Aviation Authority AD No. G-2004- 0014 R1, Effective Date: July 29, 2005, also addresses the subject of this AD. Material Incorporated by Reference (h) You must use B-N Britten-Norman Aircraft Limited Service Bulletin number SB 302, Issue 2, dated April 12, 2005, and B-N Group Ltd. Modification Leaflet for Mod NB-M-1787, Issue 1, dated August 1, 2005, to do the actions required by this AD, unless the AD specifies otherwise.(1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact B-N Group Ltd., Bembridge Airport, Isle of Wight, PO35 5PR, United Kingdom; telephone: +44 (0) 1983 872511; fax: +44 (0) 1983 873246. (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202- 741-6030, or go to: http://www.archives.gov/federal--register/code--of--federal--regulations/ ibr--locations.html.

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Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/2006-23-03.json · aircraft systems.