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Airworthiness directives › 2004-11-11

AD 2004-11-11 Airworthiness Directives; Boeing Model 737-600, 737-700, 737-700C, 737-800, and 737-900 Series Airplanes

2004-07-13
2004-06-08
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Airframe
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Models named: 737-600, 737-700, 737-700C, 737-800, 737-900 series. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

Model 737-600, 737-700, 737-700C, 737-800, and 737-900 series airplanes, as listed in Boeing Alert Service Bulletin 737-28A1148, Revision 2, dated December 18, 2003; certificated in any category.

Compliance

Required as indicated, unless accomplished previously. To prevent electrical arcing in a fuel leakage zone, which could result in an uncontrolled fire, accomplish the following: Service Bulletin References (a) The term “service bulletin,” as used in this AD, means the Accomplishment Instructions of Boeing Alert Service Bulletin 737-28A1148, Revision 2, dated December 18, 2003. Inspection, Installation, and Corrective Actions (b) For airplanes listed in the service bulletin as Groups 1, 2, 3, and 4 on which Boeing Alert Service Bulletin 737-28A1148, dated September 14, 2000, has been accomplished; and for airplanes listed in the service bulletin as Groups 5, 6 and 7: Within six months after the effective date of this AD, install screws and spacers to secure the applicable wire bundles for the aft fuel boost pumps of the main fuel tanks. Perform all actions per the service bulletin. (c) For airplanes listed in the service bulletin as Groups 1 and 2 on which Boeing Alert Service Bulletin 737-28A1148, dated September 14, 2000, has not been accomplished: Within six months after the effective date of this AD, perform a general visual inspection of the applicable wire bundles for the aft fuel boost pumps of the main fuel tanks for chafing or other damage. Perform any applicable corrective action; and install a new bracket, clamp, and spacers to secure the wire bundles; prior to further flight. Perform all actions per the service bulletin. (d) For airplanes listed in the service bulletin as Groups 3 and 4 on which Boeing Alert Service Bulletin 737-28A1148, dated September 14, 2000, has not been accomplished: Within six months after the effective date of this AD, perform a general visual inspection of the applicable wire bundles for the aft fuel boost pumps of the main fuel tanks to determine if the wire bundle is secured with a clamp; and perform any related investigative action, and any applicable corrective actions, prior to further flight. Perform all actions per the service bulletin. Note 1: For the purposes of this AD, a general visual inspection is defined as: “A visual examination of an interior or exterior area, installation, or assembly to detect obvious damage, failure, or irregularity. This level of inspection is made from within touching distance unless otherwise specified. A mirror may be necessary to enhance visual access to all exposed surfaces in the inspection area. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight, or droplight and may require removal or opening of access panels or doors. Stands, ladders, or platforms may be required to gain proximity to the area being checked.” Actions Accomplished Per Previous Issue of the Service Bulletin (e) Actions accomplished before the effective date of this AD per Boeing Alert Service Bulletin 737-28A1148, Revision 1, dated August 22, 2002, are considered acceptable for compliance with the corresponding action specified in this AD. Alternative Methods of Compliance (f) In accordance with 14 CFR 39.19, the Manager, Seattle Aircraft Certification Office, FAA, is authorized to approve alternative methods of compliance (AMOCs) for this AD. Incorporation by Reference (g) Unless otherwise specified in this AD, the actions shall be done in accordance with Boeing Alert Service Bulletin 737-28A1148, Revision 2, dated December 18, 2003. 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 (h) This amendment becomes effective on July 13, 2004. Issued in Renton, Washington, on May 26, 2004. Kevin M. Mullin, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 04-12571 Filed 6-7-04; 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