Airworthiness directives › 2006-11-15
AD 2006-11-15 Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170-100 LR, -100 STD, -100 SE, and -100 SU Airplanes; and Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 190-100 LR, -100 STD, and -100 IGW Airplanes
Models named: ERJ 170-100 LR, -100 STD, -100 SE, -100 SU, ERJ 190-100 STD, -100 LR, -100 IGW. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all EMBRAER Model ERJ 170-100 LR, -100 STD, -100 SE, and -100 SU airplanes; and all Model ERJ 190-100 STD, -100 LR, and -100 IGW airplanes; certificated in any category.
Compliance
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 Flight Manual Revision (f) Within 7 days after the effective date of this AD, revise the Limitations section of the EMBRAER 170/190 Airplane Flight Manual (AFM) to include the following statement. This may be done by inserting a copy of this AD in the AFM. “After applying thrust reverser, do not move the throttle back to the forward thrust range, unless the REV icon on the EICAS is shown in amber or green.” Note 1: When a statement identical to that in paragraph (f) of this AD has been included in the general revisions of the AFM, the general revisions may be inserted into the AFM, and the copy of this AD may be removed from the AFM. Alternative Methods of Compliance (AMOCs) (g)(1) The Manager, International Branch, 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 § 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 directives 2006-03-02, effective April 21, 2006; and 2006-03-03, effective April 21, 2006, also address the subject of this AD. Material Incorporated by Reference (i) None. Issued in Renton, Washington, on May 22, 2006. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 06-4909 Filed 5-26-06; 8:45 am] BILLING CODE 4910-13-P
Unsafe condition
This AD results from a report that, during landing, the thrust reverser may not re-stow completely if the throttle lever is moved into the forward thrust range immediately after the thrust reverser is applied. We are issuing this AD to prevent the flightcrew from performing a takeoff with a partially deployed thrust reverser, which could result in reduced controllability of the airplane.
Read the original on the Federal Register →
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1