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2013-25-01: Flight controls

FAA order 2013-25-01 is an airworthiness directive in force since December 24, 2013. The FAA's subject line: Flight controls. It names Dassault FALCON 10: about 57 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
Dassault Aviation
Models
Falcon 10
On this site
Dassault FALCON 10 57 registered

Dates and paperwork

In force since
December 24, 2013
Published
December 9, 2013 (signed November 26, 2013)
Docket
FAA-2013-0979
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 all DASSAULT AVIATION Model Falcon 10 airplanes. This AD requires a one- time inspection for cracking of the right-hand (RH) and left-hand (LH) inboard flaps, and replacement if necessary. This AD was prompted by reports of cracking found on the inboard end plate (rib) of the RH inboard flap. We are issuing this AD to detect and correct such cracking, which could lead to complete fracture of the rib and loss of integrity of the flap structure, resulting in loss of control of the airplane.

The order itself the regulatory text, as published

Show the full text (4,885 characters)
Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39--AIRWORTHINESS DIRECTIVES 0 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): 2013-25-01 DASSAULT AVIATION: Amendment 39-17697. Docket No. FAA- 2013-0979; Directorate Identifier 2013-NM-223-AD. (a) Effective Date This AD becomes effective December 24, 2013. (b) Affected ADs None. (c) Applicability This AD applies to DASSAULT AVIATION Model Falcon 10 airplanes, certificated in any category, all serial numbers. (d) Subject Air Transport Association (ATA) of America Code 27, Flight controls. (e) Reason This AD was prompted by reports of cracking found on the inboard end plate (rib)of the right-hand inboard flap. We are issuing this AD to detect and correct such cracking, which could lead to complete fracture of the rib and loss of integrity of the flap structure, resulting in loss of control of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Inspection and Replacement Within 65 days after the effective date of this AD, do a detailed inspection for cracking of ribs 1 and 3 of the left- and right-hand inboard flaps, in accordance with the Accomplishment Instructions of Dassault Mandatory Service Bulletin F10-318, dated October 30, 2013. If any cracking is found, before further flight, replace the inboard flap with a crack-free serviceable flap, in accordance with the Accomplishment Instructions of Dassault Mandatory Service Bulletin F10-318, dated October 30, 2013. [[Page 73689]] (h) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Branch, send it to ATTN: Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-1149. Information may be emailed to: [email protected]. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/ certificate holding district office. The AMOC approval letter must specifically reference this AD. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they were approved by the State of Design Authority (or its delegated agent, or the DAH with a State of Design Authority's design organization approval). For a repair method to be approved, the repair approval must specifically refer to this AD. You are required to ensure the product is airworthy before it is returned to service. (i) Related Information Refer to Mandatory Continuing Airworthiness Information (MCAI) European Aviation Safety Agency Airworthiness Directive 2013-0262, dated October 30, 2013, for related information. You may examine the MCAI on the Internet at http://www.regulations.gov by searching for and locating it in Docket No. FAA-2013-0979. (j) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. (i) Dassault Mandatory Service Bulletin F10-318, dated October 30, 2013. (ii) Reserved. (3) For service information identified in this AD, contact Dassault Falcon Jet, P.O. Box 2000, South Hackensack, NJ 07606; telephone 201-440-6700; Internet http://www.dassaultfalcon.com. (4) You may view this service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. (5) You may view this service information that is incorporated by reference 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.

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/2013-25-01.json · aircraft systems.