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2008-26-03: Electronic strike system of the cockpit doo

FAA order 2008-26-03 is an airworthiness directive in force since April 13, 2009. The FAA's subject line: Electronic strike system of the cockpit doo. It names Boeing Of Canada/Dehav Div DHC-8, Bombardier DHC-8 Dash 8 and Q400, Dehavilland DHC-8: about 92 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: airframe structure.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Bombardier Inc.
Models
DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, DHC-8-315
On this site
Boeing Of Canada/Dehav Div DHC-8 6 registered
Bombardier DHC-8 Dash 8 and Q400 58 registered
Dehavilland DHC-8 28 registered

Dates and paperwork

In force since
April 13, 2009
Published
July 20, 2009 (signed March 30, 2009)
Docket
FAA-2009-0313
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

This document publishes in the Federal Register an amendment adopting airworthiness directive (AD) 2008-26-03. This AD requires modifying the electronic strike system of the cockpit door. This AD results from a report indicating that the equipment is defective. We are issuing this AD to prevent failure of this equipment, which could compromise flight safety.

The order itself the regulatory text, as published

Show the full text (2,290 characters)
2008-26-03 Bombardier Inc.: Amendment 39-15769. Docket No. FAA- 2009-0313; Directorate Identifier 2008-NM-144-AD. Effective Date (a) This sensitive security airworthiness directive (AD) is effective April 13, 2009. Affected ADs (b) None. Applicability (c) This AD applies to Bombardier Model DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, and DHC-8-315 airplanes, certificated in any category, equipped with a cockpit door electronic strike system installed in accordance with supplemental type certificate (STC) ST02014NY (which is equivalent to STC SA03-70). Unsafe Condition (d) This AD results from a report indicating that the equipment is defective. We are issuing this AD to prevent failure of this equipment, which could compromise flight safety. Compliance (e) Comply with this AD within the compliance times specified, unless already done. Modification (f) Within 90 days after the effective date of thisAD, modify the electronic strike system of the cockpit door in accordance with a method approved by the Manager, New York Aircraft Certification Office (ACO), FAA, or Transport Canada Civil Aviation (TCCA) (or its delegated agent). Alternative Methods of Compliance (AMOCs) (g)(1) The Manager, New York ACO, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Fabio Buttitta, Aerospace Engineer, Systems and Flight Test Branch, ANE-171, FAA, New York Aircraft Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, New York 11590; telephone (516) 228-7303; fax (516) 794- 5531. (2) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. Before using any approved AMOC on any airplane to which the AMOC applies, notify your principal maintenance inspector (PMI) or principal avionics inspector (PAI), as appropriate, or lacking a principal inspector, your local Flight Standards District Office. The AMOC approval letter must specifically reference this AD. Related Information (h) Canadian airworthiness directive CF-2008-26R1, dated August 15, 2008, also addresses the subject of this AD. Material Incorporated by Reference (i) None.

Related safety bulletins advice on the same designs, not orders

2011-08-31NM-11-52 · Flight Controls: Stabilizer Control System
2003-02-28NE-03-25 ·

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 3, 2026. Connections as data: /graph/directive/2008-26-03.json · aircraft systems.