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2026-10-04: Electrical connectors

FAA order 2026-10-04 is an airworthiness directive in force since June 25, 2026. The FAA's subject line: Electrical connectors. It names Bell 407: about 984 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
Bell Textron Canada Limited
Models
407
On this site
Bell 407 984 registered

Dates and paperwork

In force since
June 25, 2026
Published
May 21, 2026 (signed May 7, 2026)
Docket
FAA-2026-0736
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 Bell Textron Canada Limited (BTCL) Model 407 helicopters. This AD was prompted by a determination that chafing can occur at various locations on the electrical harnesses located in the aircraft instrument panel area. This AD requires a one-time detailed visual inspection of the electrical harnesses for chafing and corrective actions if necessary. This AD also requires rotation of the backshell cast housing of connectors of the lower engine airframe unit and installation of a wire harness bracket and support, and for certain helicopters, installation of a wire bundle sleeve. 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 (4,499 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: 2026-10-04 Bell Textron Canada Limited: Amendment 39-23344; Docket No. FAA-2026-0736; Project Identifier MCAI-2025-00698-R. (a) Effective Date This airworthiness directive (AD) is effective June 25, 2026. (b) Affected ADs None. (c) Applicability This AD applies to Bell Textron Canada Limited Model 407 helicopters, serial numbers 54300 through 54752, 54805 through 54999, and 56300 through 56366 and 56368, certificated in any category. (d) Subject Joint Aircraft System Component (JASC) Code 1420, Electrical connectors. (e) Unsafe Condition This AD was prompted by a determination that chafing can occur at various locations on the electrical harnesses located in the aircraft instrument panel area. The FAA is issuing this AD to detect and address chafing. The unsafe condition, if not addressed, could result in smoke or fire in the cockpit and loss of control of the helicopter. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, Transport Canada AD CF-2025-22, dated April 23, 2025 (Transport Canada AD CF-2025-22). (h) Exceptions to Transport Canada AD CF-2025-22 (1) Where Transport Canada AD CF-2025-22 refers to its effective date, this AD requires using the effective date of this AD. (2) Where Transport Canada AD CF-2025-22 requires compliance in terms of air time, this AD requires using hours time-in-service. (3) Where the material referenced in Transport Canada AD CF-2025-22 specifies "grounding screw heads should face on the left-hand side" or "grounding screw heads should face left-hand side", this AD requires replacing that text with "grounding screw heads must face on the left-hand side". (i) Special Flight Permits Special flight permits are prohibited. (j) Alternative Methods of Compliance (AMOCs) (1) 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. (2) 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 Matthew Williams, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (316) 946-4134; email: matthew.t.williams@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) Transport Canada AD CF-2025-22, dated April 23, 2025. (ii) [Reserved] (3) For Transport Canada material identified in this AD, contact Transport Canada, Transport Canada National Aircraft Certification, 159 Cleopatra Drive, Nepean, Ontario, K1A 0N5, Canada; phone: (888) 663-3639; email: TC.AirworthinessDirectives-Consignesdenavigabilite.TC@tc.gc.ca. You may find this material on the Transport Canada website at tc.canada.ca/en/aviation. (4) You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 10101 Hillwood Parkway, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call (817) 222-5118. (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 May 7, 2026. Steven W. Thompson, Acting Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2026-10167 Filed 5-20-26; 8:45 am]BILLING CODE 4910-13-P

Related safety bulletins advice on the same designs, not orders

2015-08-13SW-15-20 · Air Conditioning System Wiring
2012-10-03SW-12-45 · Garmin Model 400W/500W Series GPS-WAAS Navigation System
2010-08-11SW-10-42R1 · Emergency Float Kits
2010-08-05SW-10-42 · Emergency Float Kits
2008-08-27SW-08-42 · Emergency Float with Liferaft Kits (kits)

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 7, 2026. Connections as data: /graph/directive/2026-10-04.json · aircraft systems.