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FAA orders · airworthiness directive · historical

2006-06-09: Horizontal stabilizer actuator

FAA order 2006-06-09 is an airworthiness directive in force since April 26, 2006. The FAA's subject line: Horizontal stabilizer actuator. It names Embraer ERJ 170 E170 and E175: about 759 aircraft on the U.S. register today, 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
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 759 registered

Dates and paperwork

In force since
April 26, 2006
Published
March 22, 2006 (signed March 10, 2006)
Docket
FAA-2005-23475
Replaced by
2017-06-08
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 EMBRAER Model ERJ 170 airplanes. This AD requires revising the Airworthiness Limitations section (ALS) of the airplane maintenance manual (AMM) to include new, specific maintenance tasks related to the incorporation of a new horizontal stabilizer actuator. This AD also requires revising the ALS of the AMM to include revised repetitive inspection intervals for certain tasks in the maintenance plan related to the aileron and flap/slat flight controls system. This AD results from safety assessments of the aileron and flap/slat flight controls system, conducted after the type certification of the airplane, which showed that some dormant faults did not comply with the safety assessment criteria. We are issuing this AD to prevent failure of the aileron and flap/slat controls system, which could result in reduced controllability of the airplane.

The order itself the regulatory text, as published

Show the full text (4,631 characters)
2006-06-09 Empresa Brasileira de Aeronautica S.A. (EMBRAER): Amendment 39-14518. Docket No. FAA-2005-23475; Directorate Identifier 2005-NM-117-AD. Effective Date (a) This AD becomes effective April 26, 2006. Affected ADs (b) None. Applicability (c) This AD applies to all EMBRAER Model ERJ 170-100 LR, -100 STD, -100 SE, and -100 SU airplanes, certificated in any category. Unsafe Condition (d) This AD results from safety assessments of the aileron and flap/slat flight controls system, conducted after the type certification of the airplane, which showed that some dormant faults did not comply with the safety assessment criteria. We are issuing this AD to prevent failure of the aileron and flap/slat controls system, which could result in reduced controllability of the airplane. 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. Airplane Maintenance Manual (AMM) Revisions (f) Within 30 days after the effective date of this AD: Revise the Airworthiness Limitations section of the Instructions for Continued Airworthiness in the EMBRAER 170 AMM to include revisions to the maintenance tasks and repetitive inspections intervals, and applicable corrective actions that are approved by either the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the Departmento de Aviacao Civil (DAC), (or its delegated agent). The revisions in paragraphs (f)(1) and (f)(2) of this AD are approved methods. (1) EMBRAER Temporary Revision (TR) 1-3 of the EMBRAER 170 Maintenance Review Board (MRB) Report MRB-1621, dated December 27, 2004, to the EMBRAER 170 AMM includes revised repetitive inspection intervals for MRB tasks 27-11-00-002 (Operational Check of Control- Yoke Disconnect System) and 27-11-11-001 (Operational Check of Aileron Override Unit). Where the revision requires a compliance time that is less than 700 flight hours after the effective date of this AD, do the action within 700 flight hours after the effective date of this AD. Thereafter, except as provided by paragraph (h) of this AD, no alternative inspection intervals may be approved. (2) The revised EMBRAER 170 AMM maintenance tasks identified in Table 1 of this AD include new maintenance tasks and inspections related to the incorporation of a new horizontal stabilizer actuator. Thereafter, except as provided by paragraph (h) of this AD, no alternative tasks or inspections may be approved. Table 1.--EMBRAER 170 AMM Maintenance Tasks AMM chapter Task Nos. Date Title 27 11 03 27 11 03 710 801 A, 27 11 03 720 801 A January 25, 2005 Aileron Control Cable Ajustment/Test. 27 41 01 27 41 01 210 801 A, 27 41 01 220 801 A, 27 41 01 220 802 A. January 25, 2005 Horizontal Stabilizer Trim Actuator Inspection/Check. 27 81 01 27 81 01 710 801 A January 25, 2005 Slat Actuator Adjustment/Test. Alternative Methods of Compliance (AMOCs) (g)(1) The Manager, ANM-116, Transport Airplane Directorate, FAA, has the authority to 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 (h) Brazilian airworthiness directive 2005-03-02, effective April 20, 2005, also addresses the subject of this AD. Material Incorporated by Reference (i) You must use EMBRAER Temporary Revision 1-3 of the EMBRAER 170 Maintenance Review Board Report MRB-1621, dated December 27, 2004, to the EMBRAER 170 Airplane Maintenance Manual, 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. You may 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.

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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/2006-06-09.json · aircraft systems.