Airworthiness directives › 2005-02-10
AD 2005-02-10 Airworthiness Directives; Boeing Model 757 Series Airplanes Equipped With Rolls Royce Model RB211 Engines
Models named: 757 series, RB211. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model 757 series airplanes; certificated in any category; line numbers 1 through 1018 inclusive; equipped with Rolls Royce Model RB211 engines.
Compliance
Required as indicated, unless accomplished previously. To prevent flammable fluids from leaking into the interior compartment of the nacelle struts where ignition sources exist, which could result in the ignition of flammable fluids and an uncontained fire, accomplish the following: Inspection (a) Within 3,000 flight hours after the effective date of this AD: Do a detailed inspection of the support brackets and associated fasteners for the hydraulic lines located in the nacelle struts for loose or damaged parts, by accomplishing all of the actions specified in Part 1 of the Accomplishment Instructions of Boeing Alert Service Bulletin 757-54A0045 (for Model 757-200 series airplanes), dated May 22, 2003; or Boeing Alert Service Bulletin 757-54A0046 (for Model 757-300 series airplanes), dated May 29, 2003; as applicable. Do the actions per the applicable service bulletin. Repeat the inspection thereafter at intervals not to exceed 3,000 flight hours. Note 1: For the purposes of this AD, a detailed inspection is defined as: “An intensive visual examination of a specific structural area, system, installation, or assembly to detect damage, failure, or irregularity. Available lighting is normally supplemented with a direct source of good lighting at intensity deemed appropriate by the inspector. Inspection aids such as mirror, magnifying lenses, etc., may be used. Surface cleaning and elaborate access procedures may be required.” Related Investigative and Corrective Actions (b) Except as required by paragraph (d) of this AD: If any loose or damaged parts are found during any inspection required by paragraph (a) of this AD, before further flight, for the affected nacelle strut only, do all of the related investigative and corrective actions specified in Part 2 of the Accomplishment Instructions of Boeing Alert Service Bulletin 757-54A0045 (for Model 757-200 series airplanes), dated May 22, 2003; or Boeing Alert Service Bulletin 757-54A0046 (for Model 757-300 series airplanes), dated May 29, 2003; as applicable. Do the actions in accordance with the applicable service bulletin. Accomplishment of these actions constitutes terminating action for the repetitive inspections required by paragraph (a) of this AD for that nacelle strut only. Optional Terminating Action (c) If performed on both nacelle struts concurrently: Accomplishment of all of the actions specified in Part 2 of the Accomplishment Instructions of Boeing Alert Service Bulletin 757-54A0045 (for Model 757-200 series airplanes), dated May 22, 2003; or Boeing Alert Service Bulletin 757-54A0046 (for Model 757-300 series airplanes), dated May 29, 2003; as applicable; constitutes terminating action for the repetitive inspections required by paragraph (a) of this AD. Repair Information (d) If any damage is found during any inspection required by this AD, and the service bulletin specifies contacting Boeing for appropriate action. Before further flight, repair per a method approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA. For a repair method to be approved by the Manager, Seattle ACO, as required by this paragraph, the Manager's approval letter must specifically refer to this AD. Alternative Methods of Compliance (e) In accordance with 14 CFR 39.19, the Manager, Seattle ACO, is authorized to approve alternative methods of compliance for this AD. Incorporation by Reference (f) Unless otherwise specified in this AD, the actions shall be done in accordance with Boeing Alert Service Bulletin 757-54A0045, dated May 22, 2003; or Boeing Alert Service Bulletin 757-54A0046, dated May 29, 2003; as applicable. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124-2207. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal _register/code_ of_federal_ regulations/ibr_locations.html. Effective Date (g) This amendment becomes effective on March 7, 2005. Issued in Renton, Washington, on January 18, 2005. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05-1517 Filed 1-28-05; 8:45 am] BILLING CODE 4910-13-P
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