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FAA orders · airworthiness directive · historical

2006-12-09: Inner webs and flanges at frames 15, 18, 41, and 43

FAA order 2006-12-09 is an airworthiness directive in force since July 17, 2006. The FAA's subject line: Inner webs and flanges at frames 15, 18, 41, and 43. It names British Aerospace AVRO 146, British Aerospace BAE 146: about 27 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
BAE Systems (Operations) Limited
Models
Avro 146-RJ100A, Avro 146-RJ70A, Avro 146-RJ85A, BAe 146-100A, BAe 146-200A, BAe 146-300A
On this site
British Aerospace AVRO 146 12 registered
British Aerospace BAE 146 15 registered

Dates and paperwork

In force since
July 17, 2006
Published
June 12, 2006 (signed May 31, 2006)
Docket
FAA-2005-23284
Replaces
2004-01-07
Replaced by
2009-12-10
Status
Historical
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is superseding an existing airworthiness directive (AD), which applies to certain BAE Systems (Operations) Limited Model BAe 146 and Avro 146-RJ airplanes. That AD currently requires one-time inspections of the inner webs and flanges at frames 15, 18, 41, and 43 for evidence of corrosion or cracking; and corrective actions if necessary. This new AD instead requires new repetitive inspections and expands the area to be inspected. This new AD also expands the applicability and provides an optional action that would extend the repetitive inspection interval. This AD results from a report indicating that in some cases the inspections required by the existing AD revealed no damage, yet frame corrosion and cracking were later found during scheduled maintenance in the two forward fuselage frames 15 and 18. We are issuing this AD to prevent reduced structural integrity of the airplane.

The order itself the regulatory text, as published

Show the full text (5,076 characters)
2006-12-09 BAE Systems (Operations) Limited (Formerly British Aerospace Regional Aircraft): Amendment 39-14634. Docket No. FAA- 2005-23284; Directorate Identifier 2005-NM-163-AD. Effective Date (a) This AD becomes effective July 17, 2006. Affected ADs (b) This AD supersedes AD 2004-01-07. Applicability (c) This AD applies to all BAE Systems (Operations) Limited Model BAe 146-100A, -200A, and -300A series airplanes; and Model Avro 146-RJ70A, 146-RJ85A, and 146-RJ100A airplanes; certificated in any category. Unsafe Condition (d) This AD results from a report indicating that in some cases the inspections required by AD 2004-01-07 revealed no damage, yet frame corrosion and cracking were later found during scheduled maintenance in the two forward fuselage frames 15 and 18. We are issuing this AD to prevent reduced structural integrity of the airplane. Compliance (e) You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. Inspections (f) Use high-frequency eddy current and detailed methods to inspect for signs of corrosion (including cracks, blistering, or flaking paint) of frames 15, 18, 41, and 43, in accordance with the Accomplishment Instructions of BAE Systems (Operations) Limited Inspection Service Bulletin ISB.53-182, dated March 16, 2005. Inspect at the applicable time specified in 1.D. "Compliance" of the service bulletin. Application of corrosion-preventive treatment, in accordance with the service bulletin, extends the repetitive inspection interval, as specified in Table 2 in 1.D. "Compliance" of the service bulletin. Note 1: For the purposes of this AD, a detailed inspection is: "An intensive examination of a specific item, installation, or assembly to detect damage, failure, or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirror, magnifying lenses, etc., may be necessary. Surface cleaning and elaborate procedures may be required." Corrective Action (g) If any discrepancy is found during any inspection required by paragraph (f) of this AD: Before further flight, perform applicable related investigative/corrective actions in accordance with the Accomplishment Instructions of BAE Systems (Operations) Limited Inspection Service Bulletin ISB.53-182, dated March 16, 2005, except as required by paragraph (h) of this AD. Exceptions to Service Bulletin Specifications (h) If the service bulletin referenced in this AD specifies to contact the manufacturer for appropriate action, before further flight, repair per a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the Civil Aviation Authority (or its delegated agent). (i) Although the service bulletin referenced in this AD specifies to submit information to the manufacturer, this AD does not include such a requirement. (j) Where the service bulletin specifies a compliance time after the issuance of the service bulletin, this AD requires compliance within the specified compliance time after the effective date of this AD. And where the service bulletin specifies a compliance time "since date of construction" of the airplane, this AD requires compliance since the date of issuance of the original standard airworthiness certificate or the date of issuance of the original export certificate of airworthiness. Alternative Methods of Compliance (AMOCs) (k)(1) The Manager, International Branch, ANM-116, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. (2) Before using any AMOC approved in accordance with Sec. 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office.Related Information (l) British airworthiness directive G-2005-0019, dated July 6, 2005, also addresses the subject of this AD. Material Incorporated by Reference (m) You must use BAE Systems (Operations) Limited Inspection Service Bulletin ISB.53-182, dated March 16, 2005, to perform the actions that are required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approved the incorporation by reference of this document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact British Aerospace Regional Aircraft American Support, 13850 Mclearen Road, Herndon, Virginia 20171, for a copy of this service information. You may review copies at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., Room PL-401, Nassif Building, Washington, DC; on the Internet at http://dms.dot.gov; or at the National Archives and Records Administration (NARA). For information on the availability of this material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/ federal--register/code--of--federal--regulations/ ibr--locations.html.

Related safety bulletins advice on the same designs, not orders

2019-02-19NE-19-03 · Escape Slide Maintenance Tasks and Intervals - JASC 2565
2008-09-03NM-08-43 · Cabin Equipment/Furnishings - Seats
2006-07-27NM-06-57 · Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.

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 3, 2026. Connections as data: /graph/directive/2006-12-09.json · aircraft systems.