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FAA orders · airworthiness directive · current

2026-09-13: Flight controls

FAA order 2026-09-13 is an airworthiness directive in force since June 18, 2026. The FAA's subject line: Flight controls. It names Aerospatiale/Aeritalia ATR 42, Atr-Gie Avions De Trnsp Region ATR42: about 22 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
ATR – GIE Avions de Transport Régional
Models
ATR42-200, ATR42-300, ATR42-320
On this site
Aerospatiale/Aeritalia ATR 42 16 registered
Atr-Gie Avions De Trnsp Region ATR42 6 registered

Dates and paperwork

In force since
June 18, 2026
Published
May 14, 2026 (signed April 28, 2026)
Docket
FAA-2026-2278
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is adopting a new airworthiness directive (AD) for all ATR--GIE Avions de Transport R[eacute]gional Model ATR42-200, -300, and -320 airplanes. This AD was prompted by a report of an occurrence of a flap asymmetry detector and flap interconnection shaft having worn splines and not engaging mechanically. This AD requires a special detailed inspection (SDI) of the affected flap asymmetry detection mechanism, and applicable corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (4,529 characters)
1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. 2. The FAA amends § 39.13 by adding the following new airworthiness directive: 2026-09-13 ATR-GIE Avions de Transport Régional: Amendment 39-23335; Docket No. FAA-2026-2278; Project Identifier MCAI-2025-00628-T. (a) Effective Date This airworthiness directive (AD) is effective June 18, 2026. (b) Affected ADs None. (c) Applicability This AD applies to all ATR-GIE Avions de Transport Régional Model ATR42-200, -300, and -320 airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 27, Flight controls. (e) Unsafe Condition This AD was prompted by a report of a flap asymmetry detector and flap interconnection shaft having worn splines and not engaging mechanically. The FAA is issuing this AD to address this condition, which, if not addressed, could result in the loss of flap asymmetry monitoring and reduced control of the airplane in case of asymmetrical flaps extension or retraction. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Requirements Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2025-0087, dated April 16, 2025 (EASA AD 2025-0087). (h) Exceptions to EASA AD 2025-0087 (1) Where EASA AD 2025-0087 refers to its effective date, this AD requires using the effective date of this AD. (2) This AD does not adopt the "Remarks" section of EASA AD 2025-0087. (i) No Reporting Requirement Although the material referenced in EASA AD 2025-0087 specifies to submit certain information to the manufacturer, this AD does not include that requirement. (j) Additional AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Validation Branch, 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 responsible Flight Standards Office, as appropriate. If sending information directly to the manager of the International Validation Branch, send it to the attention of the person identified in paragraph (k) of this AD and email to: AMOC@faa.gov . Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. (2) Contacting the Manufacturer: For any requirement in this AD to obtain instructions from a manufacturer, the instructions must be accomplished using a method approved by the Manager, International Validation Branch, FAA; or EASA; or ATR-GIE Avions de Transport Régional's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (k) Additional Information For more information about this AD, contact Fatin Saumik, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 516-228-7350; email: 9-AVS-AIR-BACO-COS@faa.gov. (l) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference of the material listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this material as applicable to do the actions required by this AD, unless this AD specifies otherwise. (i) European Union Aviation Safety Agency (EASA) AD 2025-0087, dated April 16, 2025. (ii) [Reserved] (3) For EASA material identified in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu. You may find this material on the EASA website at ad.easa.europa.eu. (4) You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. (5) You may view this material at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations or email fr.inspection@nara.gov. Issued on April 28, 2026. Steven W. Thompson, Acting Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2026-09658 Filed 5-13-26; 8:45 am]BILLING CODE 4910-13-P

Related safety bulletins advice on the same designs, not orders

2015-04-20NM-15-14 · Propellers/Propulsors
2011-08-01NM-11-45 · Doors: Cargo/Baggage Doors
2011-02-03NM-11-19 · Indicating/Recording System Angle of Attack Sensors
2010-03-04NM-10-18 · Instruments: Redesigned Aileron Sensors for Flight Data Recorder
2010-01-07NM-10-13 · Navigation: Flight Management System

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/2026-09-13.json · aircraft systems.