Airworthiness directives › 2001-18-08
AD 2001-18-08 Airworthiness Directives; Boeing Model 767-300 Series Airplanes Modified by Supplemental Type Certificate SA7019NM-D
Models named: 767-300 series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model 767-300 series airplanes modified by supplemental type certificate (STC) SA7019NM-D, dated July 14, 1995; certificated in any category. Note 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been otherwise modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (c) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.
Compliance
Required as indicated, unless accomplished previously. To ensure that the flight crew and cabin crew are able to remove electrical power from the in-flight entertainment (IFE) system when necessary and are advised of appropriate procedures for such action, accomplish the following: Modification and Manual Revisions (a) Within 18 months after the effective date of this AD, accomplish paragraphs (a)(1) and (a)(2) of this AD. (1) Install a master power control switch for the video system and associated wiring, in accordance with BFGoodrich Engineering Order 23-32-767-031, dated August 16, 2000. (2) Following installation of the master power control switch in accordance with paragraph (a)(1) of this AD, prior to further flight, insert BFGoodrich 767 Flight Attendant Manual Supplement D2000-160, dated August 16, 2000, into the Flight Attendant Manual, and insert BFGoodrich B767 Airplane Flight Manual (AFM) Supplement D2001-025, dated February 26, 2001, into the Emergency Procedures section of the AFM. Spares (b) As of the effective date of this AD, no person shall install an IFE system in accordance with STC SA7019NM-D, dated July 14, 1995, on any airplane, unless it is modified, and the Flight Attendant Manual and AFM are revised, in accordance with this AD. Alternative Methods of Compliance (c) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Seattle ACO. Note 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Seattle ACO. Special Flight Permits (d) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. Incorporation by Reference (e) The actions shall be done in accordance with BFGoodrich Engineering Order 23-32-767-031, including Parts List Attachment and Wire List Attachment, dated August 16, 2000; BFGoodrich 767 Flight Attendant Manual Supplement D2000-160, dated August 16, 2000; and BFGoodrich B767 Airplane Flight Manual Supplement D2001-025, dated February 26, 2001. 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 BFGoodrich Aerospace, 3100 112th Street SW., Everett, Washington 98204-3500. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. Effective Date (f) This amendment becomes effective on October 11, 2001. Issued in Renton, Washington, on August 28, 2001. Vi L. Lipski, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 01-22110 Filed 9-5-01; 8:45 am] BILLING CODE 4910-13-U
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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