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

2005-23-14: Low-stage check valve

FAA order 2005-23-14 is an airworthiness directive in force since November 29, 2005. The FAA's subject line: Low-stage check valve. It names Embraer ERJ 170 E170 and E175: about 768 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
Embraer S.A.
Models
ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD, ERJ 170-100 SU
On this site
Embraer ERJ 170 E170 and E175 768 registered

Dates and paperwork

In force since
November 29, 2005
Published
November 14, 2005 (signed November 2, 2005)
Docket
FAA-2005-22910
Replaced by
2007-16-09
Status
Historical
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 Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 airplanes. This AD requires repetitively replacing the low-stage check valve and associated seals of the right-hand engine bleed system. This AD results from a report that an engine shut down during flight due to the failure of the low-stage check valve to close. We are issuing this AD to prevent failure of the low-stage check valve, which could result in an engine shutting down during flight.

The order itself the regulatory text, as published

Show the full text (3,396 characters)
2005-23-14 Empresa Brasileira de Aeronautica S.A. (EMBRAER): Amendment 39-14372. Docket No. FAA-2005-22910; Directorate Identifier 2005-NM-208-AD. Effective Date (a) This AD becomes effective November 29, 2005. Affected ADs (b) None. Applicability (c) This AD applies to all EMBRAER Model ERJ 170-100LR, -100 STD, -100SE, and -100 SU airplanes, certificated in any category. Unsafe Condition (d) This AD results from a report that an engine shut down during flight due to the failure of the low-stage check valve to close. We are issuing this AD to prevent failure of the low-stage check valve, which could result in an engine shutting down during flight. Compliance (e) You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. Replacement (f) Within 100 flight hours after the effective date of this AD or prior to the accumulation of 3,000 total flight hours, whichever occurs later, replace the low-stage check valve and associated seals of the right-hand engine's engine bleed system with a new check valve and new seals in accordance with the Accomplishment Instructions of EMBRAER Alert Service Bulletin 170-36-A004, dated September 28, 2005. Repeat the replacement thereafter at intervals not to exceed 3,000 flight hours. Parts Installation (g) As of the effective date of this AD, no engine may be installed in the right-hand position unless the low-stage check valve has been replaced in accordance with the actions required by paragraph (f) of this AD. Removed Check Valves (h) Although EMBRAER Alert Service Bulletin 170-36-A004, dated September 28, 2005, specifies to send removed check valves to the manufacturer, this AD does not include that requirement. Alternative Methods of Compliance (AMOCs) (i)(1) The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authorityto approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. (2) Before using any AMOC approved in accordance with Sec. 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. Related Information (j) Brazilian emergency airworthiness directive 2005-09-03, dated September 29, 2005, also addresses the subject of this AD. Material Incorporated by Reference (k) You must use EMBRAER Alert Service Bulletin 170-36-A004, dated September 28, 2005, to perform the actions that are required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approved the incorporation by reference of this document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box 343-CEP 12.225, Sao Jose dos Campos-SP, Brazil, for a copy of this service information. Youmay review copies at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., room PL-401, Nassif Building, Washington, DC; on the Internet at http://dms.dot.gov; or at the National Archives and Records Administration (NARA). For information on the availability of this material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html .

Related safety bulletins advice on the same designs, not orders

2020-06-18NM-20-12 · Powerplant System - Operating in Icing Conditions

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 6, 2026. Connections as data: /graph/directive/2005-23-14.json · aircraft systems.