Airworthiness directives › 2001-13-26
AD 2001-13-26 Airworthiness Directives; McDonnell Douglas Model DC-10-10, -15, -30, and -40 Series Airplanes, and Model MD-10-10F and -30F Series Airplanes
Models named: DC-10-10, -15, -30, -40 series, MD-10-10F, -30F series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
Model DC-10-10, -15, -30, and -40 series airplanes, and Model MD-10-10F and -30F series airplanes; as listed in McDonnell Douglas Alert Service Bulletin DC10-24A147, Revision 03, dated April 30, 2001; certificated in any category. Note 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been 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 (b) 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 prevent chafing of the feeder cables during removal of the sump panels of the cargo floor, which could result in electrical arcing and damage to adjacent structure, and consequent smoke and/or fire in the forward cargo compartment, accomplish the following: Inspection, Installation of Spiral Wrap, and Repair, if Necessary (a) Within 1 year after the effective date of this AD, do the actions specified in paragraphs (a)(1) and (a)(2) of this AD per McDonnell Douglas Alert Service Bulletin DC10-24A147, Revision 03, dated April 30, 2001. (1) Do a general visual inspection to detect chafing or damage of the feeder cables of the external ground power in the forward cargo compartment between fuselage stations Y=879.000 and Y=1019.000 left of centerline. If any chafing or damage is detected, before further flight, repair the feeder cables of the external ground power and adjacent structure. Note 2: 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 under normally available lighting conditions such as daylight, hangar lighting, flashlight, or drop-light, 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.” (2) Install spiral wrap on the feeder cables of the external ground power. Note 3: Accomplishment of the inspection, repair, and installation per McDonnell Douglas Alert Service Bulletin DC10-24A147, Revision 02, dated March 6, 2000, before the effective date of this AD, is considered acceptable for compliance with the requirements of this AD. Alternative Methods of Compliance (b) 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, Los Angeles 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, Los Angeles ACO. Note 4: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Los Angeles ACO. Special Flight Permits (c) 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 (d) The actions shall be done in accordance with McDonnell Douglas Alert Service Bulletin DC10-24A147, Revision 03, dated April 30, 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 Boeing Commercial Aircraft Group, 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 Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. Effective Date (e) This amendment becomes effective on August 27, 2001. Issued in Renton, Washington, on July 9, 2001. Vi L. Lipski, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 01-17591 Filed 7-20-01; 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