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2008-17-07: Flight controls tie rod

FAA order 2008-17-07 is an airworthiness directive in force since September 23, 2008. The FAA's subject line: Flight controls tie rod. It names Avions Mudry Et Cie CAP 10: about 22 aircraft on the U.S. register today, 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
APEX Aircraft
Models
CAP 10 B
On this site
Avions Mudry Et Cie CAP 10 22 registered

Dates and paperwork

In force since
September 23, 2008
Published
August 19, 2008 (signed August 7, 2008)
Docket
FAA-2008-0470
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 the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: An internal review evidenced that the flight controls tie rod bolts currently installed on the airplane are not in accordance with the design data. Indeed the bolt shank length has been determined too short and the material properties of the spacers have been found inadequate according to the prescribed torque value. Therefore, bolts' threads could be subject to excessive wear, which might induce play in flight controls and consequently, induce vibrations in the control surfaces and reduce the airplane handling. We are issuing this AD to require actions to correct the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (4,391 characters)
2008-17-07 APEX Aircraft: Amendment 39-15645; Docket No. FAA-2008- 0470; Directorate Identifier 2008-CE-026-AD. Effective Date (a) This airworthiness directive (AD) becomes effective September 23, 2008. Affected ADs (b) None. Applicability (c) This AD applies to the following Model CAP 10 B airplanes, certificated in any category: (1) Serial numbers 300 through 317; and (2) All other serial numbers that incorporate APEX change 000302 (fibre carbon wing spars). Subject (d) Air Transport Association of America (ATA) Code 27: Flight Controls. Reason (e) The mandatory continuing airworthiness information (MCAI) states: An internal review evidenced that the flight controls tie rod bolts currently installed on the airplane are not in accordance with the design data. Indeed the bolt shank length has been determined too short and the material properties of the spacers have been found inadequate according to the prescribed torque value.Therefore, bolts' threads could be subject to excessive wear, which might induce play in flight controls and consequently, induce vibrations in the control surfaces and reduce the airplane handling. To prevent this condition, the present Airworthiness Directive (AD) mandates replacement of the tie rod bolts and spacers. Actions and Compliance (f) Unless already done, do the following actions: (1) Within 50 hours time-in-service after September 23, 2008 (the effective date of this AD), remove tie rod bolts part number (P/N) 95.56.11.066 and spacers P/N 11.56.27.038 and replace them with tie rod bolts P/N 95.56.11.418 and spacers P/N 11.56.27.138, following APEX Aircraft Service Bulletin No. 040206, dated September 21, 2007. (2) As of September 23, 2008 (the effective date of this AD), do not install any tie rod bolt P/N 95.56.11.066 or spacer P/N 11.56.27.038. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Office, 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: Sarjapur Nagarajan, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4145; fax: (816) 329-4090. 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. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act (44 U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (h) Refer to MCAI European Aviation Safety Agency (EASA) AD No. 2008-0060, dated April 1, 2008; and APEX Aircraft Service Bulletin No. 040206, dated September 21, 2007, for related information. Material Incorporated by Reference (i) You must use APEX Aircraft Service Bulletin No. 040206, dated September 21, 2007, 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 thisAD, contact Apex Aircraft, Bureau de Navigabilite, 1 route de Troyes, 21121 DAROIS, France. (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, 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/cfr/ibr-locations.html.

Related safety bulletins advice on the same designs, not orders

2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
2013-11-04CE-14-01 · Placards and Markings: Flat Spin Recovery and Aircraft Flight Manual (AFM) Revision of CAP 10B Aeroplanes
2005-05-24CE-05-54 ·
2005-05-09CE-05-52 ·
2004-08-27CE-04-82 ·

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/2008-17-07.json · aircraft systems.