Airworthiness directives › 2001-14-11
AD 2001-14-11 Airworthiness Directives; Boeing Model 747-100 and -200 Series Airplanes Modified by Supplemental Type Certificate SA8622SW
Models named: 747-100, -200 series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model 747-100 and -200 series airplanes modified by Supplemental Type Certificate (STC) SA8622SW, 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 is able to remove power from the in-flight entertainment (IFE) system when necessary; which, if not done during a non-normal or emergency situation, could result in inability to control smoke or fumes in the airplane flight deck or cabin; accomplish the following: Deactivation (a) Within 18 months after the effective date of this AD, deactivate the IFE system, in accordance with Continental Airlines Engineering Change/Repair Authorization 2330-02321, 2330-02322, 2330-02323, 2330-02324, 2330-02325, 2330-02326, 2330-02327, or 2330-02328; all dated August 29, 2000; as applicable. Spares (b) As of the effective date of this AD, no person shall install an IFE system in accordance with STC SA8622SW on any airplane. 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, Fort Worth Airplane 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, Fort Worth ACO. Note 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Fort Worth ACO. Special Flight Permits (d) Special flight permits may be issued in accordance with §§ 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 Continental Airlines Engineering Change/Repair Authorization 2330-02321, dated August 29, 2000; Continental Airlines Engineering Change/Repair Authorization 2330-02322, dated August 29, 2000; Continental Airlines Engineering Change/Repair Authorization 2330-02323, dated August 29, 2000; Continental Airlines Engineering Change/Repair Authorization 2330-02324, dated August 29, 2000; Continental Airlines Engineering Change/Repair Authorization 2330-02325, dated August 29, 2000; Continental Airlines Engineering Change/Repair Authorization 2330-02326, dated August 29, 2000; Continental Airlines Engineering Change/Repair Authorization 2330-02327, dated August 29, 2000; or Continental Airlines Engineering Change/Repair Authorization 2330-02328, dated August 29, 2000; as applicable. (Only the first page of these documents contains the document date; no other page contains this information.) 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 Continental Airlines, Inc., 600 Jefferson Street HQJAV, Houston, Texas 77002. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; at the FAA, Fort Worth Airplane Certification Office, 2601 Meacham Blvd., Fort Worth, Texas; 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 August 16, 2001. Issued in Renton, Washington, on July 3, 2001. Vi L. Lipski, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 01-17159 Filed 7-11-01; 8:45 am] BILLING CODE 4910-13-P
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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