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2016-04-19: Flight Controls

FAA order 2016-04-19 is an airworthiness directive in force since March 14, 2016. The FAA's subject line: Flight Controls. It names Airbus Defense And Space S A C-295, Construcciones Aeronauticas Sa CN-235: about 15 aircraft on the U.S. register today across them, 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
Airbus Defense and Space S.A.
Models
C-295, CN-235, CN-235-100, CN-235-200, CN-235-300
On this site
Airbus Defense And Space S A C-295 5 registered
Construcciones Aeronauticas Sa CN-235 10 registered

Dates and paperwork

In force since
March 14, 2016
Published
February 26, 2016 (signed February 15, 2016)
Docket
FAA-2016-3704
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 Airbus Defense and Space S.A. Model CN-235, CN-235-100, CN-235-200, CN- 235-300, and C-295 airplanes. This AD requires a general visual inspection of the rudder control system to confirm correct alignment and installation of the adjustment device, and repair if necessary. This AD was prompted by a report of disconnection of the kinematic chain from the co-pilot rudder pedals to the rudder control bars located under the cockpit floor; subsequent investigation revealed that the failure was caused by disconnection of the pedal adjustment device from the adjustment actuator. We are issuing this AD to detect and correct incorrect alignment and incorrect installation of the adjustment device, which could lead to loss of the rudder control from the affected side and possibly result in reduced control of the airplane.

The order itself the regulatory text, as published

Show the full text (6,607 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): 2016-04-19 Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.): Amendment 39-18413. Docket No. FAA-2016-3704; Directorate Identifier 2016-NM-005-AD. (a) Effective Date This AD becomes effective March 14, 2016. (b) Affected ADs None. (c) Applicability This AD applies to Airbus Defense and Space S.A. (Formerly known as Construcciones Aeronauticas, S.A.) Model CN-235, CN-235-100, CN- 235-200, CN-235-300, and C-295 airplanes, certificated in any category, all manufacturer serial numbers. (d) Subject Air Transport Association (ATA) of America Code 27, Flight Controls. (e) Reason This AD was prompted by a report of disconnection of the kinematic chain from the co-pilot rudder pedals to the rudder control bars located under the cockpit floor; subsequent investigation revealed that the failure was caused by disconnection of the pedal adjustment device from the adjustment actuator. We are issuing this AD to detect and correct incorrect alignment and incorrect installation of the adjustment device, which could lead to loss of the rudder control from the affected side and possibly result in reduced control of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) General Visual Inspection Within 30 days after the effective date of this AD: Do a general visual inspection of the rudder control system to confirm correct alignment and installation of the adjustment device, in accordance with the instructions of Airbus Defence and Space Alert Operators Transmission (AOT) AOT-C295-27-0001, Revision 1, dated September 29, 2015; or Airbus Defence and Space AOT AOT-CN235-27-0002, Revision 1, dated September 22, 2015; as applicable. (h) Corrective Action If, during the general visual inspection required by paragraph (g) of this AD, any discrepancy is found, as specified in Airbus Defence and Space AOT AOT-C295-27-0001, Revision 1, dated September 29, 2015; or Airbus Defence and Space AOT AOT-CN235-27-0002, Revision 1, dated September 22, 2015; as applicable: Before further flight, repair using a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency (EASA); or Airbus Defense and Space S.A.'s EASA Design Organization Approval (DOA). (i) Credit for Previous Actions This paragraph provides credit for actions required by paragraph (g) of this AD, if those actions were performed before the effective date of this AD using Airbus Defence and Space AOT AOT-C295-27-0001, dated October 23, 2014; or Airbus Defence and Space AOT AOT-CN235- 27-0002, dated October 23, 2014; as applicable. [[Page 9756]] (j) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, 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: Shahram Daneshmandi, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1112; 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) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency (EASA); or Airbus Defense and Space S.A.'s EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (k) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2016-0012, dated January 14, 2016, for related information. You may examine the MCAI on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-3704. (2) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (l)(3) and (l)(4) of this AD. (l) 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) Airbus Defence and Space Alert Operators Transmission AOT- C295-27-0001, Revision 1, dated September 29, 2015. (ii) Airbus Defence and Space Alert Operators Transmission AOT- CN235-27-0002, Revision 1, dated September 22, 2015. (3) For service information identified in this AD, contact Airbus Defense and Space S.A., Services/Engineering Support, Avenida de Arag[oacute]n 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; fax +34 91 585 3127; email [email protected]. For U.S. operators, email alternatively [email protected]. (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.

Related safety bulletins advice on the same designs, not orders

2008-12-11NM-09-03 · Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations

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 23, 2026. Connections as data: /graph/directive/2016-04-19.json · aircraft systems.