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Airworthiness directives › 2006-20-14

AD 2006-20-14 Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 and ERJ 190 Airplanes

2007-01-16
2007-01-10
39-14878
FAA-2007-26797
Airframe
—

Models named: ERJ 170-100 LR, -100 STD, -100 SE, -100 SU, -200 STD, -200 LR, -200 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 EMBRAER Model ERJ 170-100 LR, -100 STD, -100 SE, -100 SU, -200 STD, -200 LR, and -200 SU airplanes, and Model ERJ 190-100 STD, -100 LR, and -100 IGW airplanes; certificated in any category; as identified in EMBRAER Service Bulletins SB No. 170-52-0029 and SB No. 190-52-0011, both dated August 21, 2006.

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. Transfer of Airplane and Requirement To Inform New Operator of This AD (f) When an operator of an affected airplane sells or otherwise transfers the airplane to another operator, the new operator must be informed of this AD in a manner consistent with the procedures found in 49 CFR part 15. Replacement (g) Within 60 days after the effective date of this AD, modify the flight deck door electronic equipment in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA. Doing all actions in the Accomplishment Instructions of the applicable EMBRAER service bulletin identified in Table 1 of this AD is one approved method; except where the applicable service bulletin specifies to send the removed flight deck door electronic equipment to the manufacturer in paragraph 3.C., that action is not necessary. Table 1.—Service Bulletins For model— EMBRAER service bulletin— (1) ERJ 170 airplanes 170-52-0029, dated August 21, 2006. (2) ERJ 190 airplanes 190-52-0011, dated August 21, 2006. Parts Installation (h) As of the effective date of this AD, no person may install on any airplane any cockpit door control panel identified in paragraph 1.A. of the applicable service bulletin in Table 1 of this AD. Alternative Methods of Compliance (AMOCs) (i)(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. Issued in Renton, Washington, on December 21, 2006. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-147 Filed 1-9-07; 8:45 am] BILLING CODE 4910-13-P

Unsafe condition

This AD results from a report indicating that this equipment is defective. We are issuing this AD to prevent failure of this equipment, which could jeopardize flight safety.

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