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2009-05-12: Aileron control system

FAA order 2009-05-12 is an airworthiness directive in force since April 15, 2009. The FAA's subject line: Aileron control system. It names Cessna 208 Caravan: about 1,022 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: flight controls.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Cessna Aircraft Company
Models
208, 208B
On this site
Cessna 208 Caravan 1,022 registered

Dates and paperwork

In force since
April 15, 2009
Published
March 11, 2009 (signed February 27, 2009)
Docket
FAA-2008-1319
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes. This AD requires you to modify the aileron carry-through cable attachment to the aileron upper quadrant with parts of improved design. This AD results from reports of a "catch'' in the aileron control system when the control yoke is turned. We are issuing this AD to prevent the cable attach fitting on the aileron upper quadrant assembly from rotating and possibly contacting or interfering with the aileron lower quadrant assembly, which could result in limited roll control and reduced handling capabilities.

The order itself the regulatory text, as published

Show the full text (3,377 characters)
2009-05-12 Cessna Aircraft Company: Amendment 39-15836; Docket No. FAA-2008-1319; Directorate Identifier 2008-CE-071-AD. Effective Date (a) This AD becomes effective on April 15, 2009. Affected ADs (b) None. Applicability (c) This AD applies to the following airplane models and serial numbers that are certificated in any category: Model Serial Nos. 208 20800001 through 20800415 and 20800417 through 20800419. 208B 208B0001 through 208B1081, 208B1083 through 208B1215, 208B1217 through 208B1257, 208B1259 through 208B1305, 208B1307, and 208B1309 through 208B1310. Unsafe Condition (d) This AD results from reports of a "catch'' in the aileron control system when the control yoke is turned. We are issuing this AD to prevent the cable attach fitting on the aileron upper quadrant assembly from rotating and possibly contacting or interfering with the aileron lower quadrant assembly, which could result in limited roll control and reduced handlingcapabilities. Compliance (e) To address this problem, you must do the following, unless already done: Actions Compliance Procedures Modify the aileron carry-through cable attachment to the aileron upper quadrant with parts of improved design. Within the next 100 hours time-in-service after April 15, 2009 (the effective date of this AD) or within the next 6 months after April 15, 2009 (the effective date of this AD), whichever occurs first. Follow the Accomplishment Instructions in Cessna Caravan Service Bulletin CAB08-6, dated October 27, 2008. Alternative Methods of Compliance (AMOCs) (f) The Manager, Wichita Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Ann Johnson, Aerospace Engineer, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone: 316-946-4105; fax: 316-946-4107; e-mail address: ann.johnson@faa.gov. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. Material Incorporated by Reference (g) You must use Cessna Caravan Service Bulletin CAB08-6, dated October 27, 2008, 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 Cessna Aircraft Company, P.O. Box 7704, Wichita, Kansas 67277; telephone: (800) 423-7762 or (316) 517-6056; Internet: http:// www.cessna.com. (3) You may review copies of the service information incorporated by reference for this AD at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the Central Region, call (816) 329-3768. (4) You may also review copies of the service information incorporated by reference for this AD 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 October 5, 2026. Connections as data: /graph/directive/2009-05-12.json · aircraft systems.