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Airworthiness directives › 2004-14-10

AD 2004-14-10 Airworthiness Directives; McDonnell Douglas Model MD-11 and -11F Airplanes

2004-08-13
2004-07-09
39-13719
2003-NM-74-AD
Airframe
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Models named: MD-11, -11F. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

Model MD-11 and -11F airplanes, as listed in Boeing Alert Service Bulletin MD11-24A138, Revision 2, dated July 11, 2003; certificated in any category.

Compliance

Required as indicated, unless accomplished previously. To prevent arcing and heat damage to the attachment points of the main external and galley power receptacle ground wire, insulation blankets outboard and aft of the receptacle area, and adjacent power cables, which could result in smoke and fire in the forward cargo compartment, accomplish the following: Replacement, Inspection, and Corrective Actions if Necessary (a) Within 12 months after the effective date of this AD, accomplish the actions specified in paragraphs (a)(1) through (a)(4) of Table 1 of this AD, as applicable, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin MD11-24A138, Revision 2, dated July 11, 2003. Any applicable corrective action must be accomplished before further flight. Table 1.—Required Actions For Group 1 airplanes listed in Revision 2 of the service bulletin on which previous issues of the service bulletin— Actions— (1) Have not been done Replace the ground support brackets with new brackets, and replace the ground cables of the galley external power and main external power with new cables. (2) Have been done Do a general visual inspection to detect the presence of a fillet seal at the ground brackets and to detect excessive length and correct terminations of the ground cables of the galley and main external power. If any discrepancy is detected, do applicable corrective actions per Figure 3 of the service bulletin.   For Group 2 airplanes listed in Revision 2 of the service bulletin on which previous issues of the service bulletin— Actions— (3) Have not been done Replace the ground support bracket with a new bracket, and replace the ground cables of the main external power with new cables. (4) Have been done Do a general visual inspection to detect the presence of a fillet seal at the ground brackets and to detect excessive length and correct terminations of the ground cables of the main external power. If any discrepancy is detected, do applicable corrective actions per Figure 4 of 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.” Alternative Methods of Compliance (b) In accordance with 14 CFR 39.19, the Manager, Los Angeles Aircraft Certification Office (ACO), FAA, is authorized to approve alternative methods of compliance (AMOCs) for this AD. (c) Alternative methods of compliance, approved previously per AD 2002-14-11, amendment 39-12811, are approved as alternative methods of compliance with this AD. Incorporation by Reference (d) The actions shall be done in accordance with Boeing Alert Service Bulletin MD11-24A138, Revision 2, dated July 11, 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, Long Beach Division, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Data and Service Management, Dept. C1-L5A (D800-0024). Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, California; 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 (e) This amendment becomes effective on August 13, 2004. Issued in Renton, Washington, on June 29, 2004. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 04-15371 Filed 7-8-04; 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