The U.S. aircraft register, updated daily
FAA orders · airworthiness directive · current

2026-08-11: Landing Gear Brake System

FAA order 2026-08-11 is an airworthiness directive in force since May 11, 2026. The FAA's subject line: Landing Gear Brake System. It names Pilatus PC-12: about 1,441 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Pilatus Aircraft Ltd.
Models
PC-12/47G
On this site
Pilatus PC-12 1,441 registered

Dates and paperwork

In force since
May 11, 2026
Published
April 24, 2026 (signed April 16, 2026)
Docket
FAA-2026-3862
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 certain Pilatus Aircraft Ltd. (Pilatus) Model PC-12/47G airplanes. This AD was prompted by a report that a brake shuttle valve (BSV) on a production airplane shuttled and isolated the brake line to the left- hand (LH) brake, which resulted in brake lockup. This AD requires replacement of the LH and right-hand (RH) brake pipe assemblies and also prohibits the installation of affected parts. 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 (4,206 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: 2026-08-11 Pilatus Aircraft Ltd.: Amendment 39-23319; Docket No. FAA-2026-3862; Project Identifier MCAI-2026-00317-A. (a) Effective Date This airworthiness directive (AD) is effective May 11, 2026. (b) Affected ADs None. (c) Applicability This AD applies to Pilatus Aircraft Ltd., Model PC-12/47G airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) Emergency AD 2026-0065-E, dated March 25, 2026 (EASA Emergency AD 2026-0065-E). (d) Subject Joint Aircraft System Component (JASC) Code 3240, Landing Gear Brake System. (e) Unsafe Condition This AD was prompted by a report that a brake shuttle valve (BSV) on a production airplane shuttled and isolated the brake line to the left-hand (LH) brake, resulting in brake lockup. The FAA is issuing this AD to prevent unintended asymmetric wheel braking. The unsafe condition, if not addressed, could result in reduced directional control of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions Except as specified in paragraphs (h) and (i) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA Emergency AD 2026-0065-E. (h) Exceptions to EASA Emergency AD 2026-0065-E (1) Where EASA Emergency AD 2026-0065-E 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 Emergency AD 2026-0065-E. (i) No Reporting Requirement Although the material referenced in EASA Emergency AD 2026-0065-E specifies to submit certain information to the manufacturer, this AD does not include that requirement. (j) 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 local Flight Standards District 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 local flight standards district office/certificate holding district office. (k) Additional Information For more information about this AD, contact Doug Rudolph, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (816) 329-4059; email: doug.rudolph@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 the AD specifies otherwise. (i) European Union Aviation Safety Agency (EASA) Emergency AD 2026-0065-E, dated March 25, 2026. (ii) [Reserved] (3) For EASA material identified in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999 000; email: ADs@easa.europa.eu; website: easa.europa.eu. You may find this EASA AD on the EASA website at ad.easa.europa.eu. (4) You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (817) 222-5110. (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 16, 2026. Steven W. Thompson, Acting Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2026-08022 Filed 4-23-26; 8:45 am]BILLING CODE 4910-13-P

Related safety bulletins advice on the same designs, not orders

2017-05-19CE-17-13 · Engine Oil Pressure; Torque Transducer Oil Pressure Pipe P-Clamp Installation
2016-01-25CE-16-12 · AUTO FLIGHT - Autopilot
2004-10-25CE-05-08 ·
2004-07-08CE-04-70 ·
2004-04-12CE-04-62 ·

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/2026-08-11.json · aircraft systems.