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FAA orders · airworthiness directive · historical

2006-23-02: Flight controls for improper assembly or damage

FAA order 2006-23-02 is an airworthiness directive in force since December 13, 2006. The FAA's subject line: Flight controls for improper assembly or damage. It names Beechcraft B200 King Air B200, Beechcraft B300 King Air 350, Beechcraft C90 King Air C90: about 2,109 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Raytheon Aircraft Company; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation
Models
B200, B200C, B300, B300C, C90A
On this site
Beechcraft B200 King Air B200 718 registered
Beechcraft B300 King Air 350 784 registered
Beechcraft C90 King Air C90 607 registered

Dates and paperwork

In force since
December 13, 2006
Published
December 21, 2006 (signed October 27, 2006)
Docket
FAA-2006-25157
Replaced by
2007-12-06
Status
Historical
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 certain Raytheon Aircraft Company (RAC) (formerly Beech) Models C90A, B200, B200C, B300, and B300C airplanes. This AD requires you to inspect the flight controls for improper assembly or damage, and if any improperly assembled or damaged flight controls are found, take corrective action. This AD results from a report of inspections of several affected airplanes with improperly assembled or damaged flight controls. We are issuing this AD to detect and correct improperly assembled or damaged flight controls, which could result in an unsafe condition by reducing capabilities of the flight controls and lead to loss of control of the airplane.

The order itself the regulatory text, as published

Show the full text (3,266 characters)
2006-23-02 Raytheon Aircraft Company (Formerly Beech): Amendment 39- 14814; Docket No. FAA-2006-25157; Directorate Identifier 2006-CE-34- AD. Effective Date (a) This AD becomes effective on December 13, 2006. Affected ADs (b) None. Applicability (c) This AD affects the following airplane models and serial numbers that are certificated in any category: Model Serial Numbers C90A LJ-1697 through LJ-1726, LJ-1728, LJ-1729, and LJ-1731 through LJ-1739 B200 BB-1827 through BB-1912 B200C BL-148 and BL-149 B300 FL-379 through FL-423, FL-426, FL-428 through FL-450, and FL-452 B300C FM-11 Unsafe Condition (d) This AD results from a report of inspections of several affected airplanes with improperly assembled or damaged flight controls. We are issuing this AD to detect and correct improperly assembled or damaged flight controls, which could result in an unsafe condition by reducing capabilities of the flight control and lead to loss of control of the airplanes. Compliance (e) To address this problem, you must do the following, unless already done: Actions Compliance Procedures (1) Inspect the entire flight control system for improper assembly and any damage. At whichever of the following occurs first: (i) Within 100 hours time-in-service after December 13, 2006 (the effective date of this AD); or (ii) At the next annual inspection that occurs at least 30 days after December 13, 2006 (the effective date of this AD). Follow Raytheon Aircraft Company Mandatory Service Bulletin Number SB 27-3761, Issued: February 2006. (2) If you find any improperly assembled or damaged flight controls as a result of the inspection required by paragraph (e)(1) of this AD, take corrective action as specified in the service information. Before further flight after the inspection required by paragraph (e)(1) of this AD. Follow Raytheon Aircraft Company Mandatory Service Bulletin Number SB 27-3761, Issued: February 2006. Alternative Methods of Compliance (AMOCs) (f) The Manager, Wichita Aircraft Certification Office (ACO), FAA, ATTN: Chris B. Morgan, Aerospace Engineer, FAA, Wichita ACO, 1801 Airport Road, Wichita, Kansas 67209; telephone: (316) 946-4154; facsimile: (316) 946-4107, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Material Incorporated by Reference (g) You must use Raytheon Aircraft Company Mandatory Service Bulletin Number SB 27-3761, Issued: February 2006, 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 Raytheon Aircraft Company, P.O. Box 85, Wichita, Kansas 67201-0085; telephone: (800) 429-5372 or (316) 676-3140. (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 .

Related safety bulletins advice on the same designs, not orders

2015-04-20CE-15-15 · Empennage Horizontal & Vertical Stabilizer Structure
2013-08-30CE-10-34R2 · Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and 89-25-08
2013-08-20CE-10-34R1 · Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and 89-25-08
2012-06-19CE-12-36 · Flight Controls: Aileron
2010-12-02CE-11-04 · Wings Wing Spar

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 October 5, 2026. Connections as data: /graph/directive/2006-23-02.json · aircraft systems.