Back to AD

AD 91-23-10 ACTIVE

Advanced Cabin Entertainment and Service System Wire Bundles
Key Information
AD Number 91-23-10 Status Active
Effective Date January 07, 1992 Issue Date Not specified
Docket Number 91-NM-109-AD Amendment 39-8079
Product Type ["Aircraft"] Product Subtype ["Large Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) The Boeing Company
Model(s) 747-400 Series 747-400D Series
Regulatory Text

91-23-10 BOEING: Amendment 39-8079. Docket No. 91-NM-109-AD. \n\n\tApplicability: Model 747-400 series airplanes, listed in Boeing Alert Service Bulletin 747-23A2241, Revision 3, dated September 5, 1991, certificated in any category. \n\n\tCompliance: Required as indicated, unless previously accomplished. \n\n\tTo prevent the occurrence of smoke and fire in the passenger cabin, accomplish the following: \n\n\t(a)\tWithin 12 months after the effective date of this AD, accomplish the following on the main and upper decks: \n\n\t\t(1)\tInspect the advanced cabin entertainment and service system (ACESS) wire bundle installation at the dado panel near each sidewall disconnect for chafing and wear in accordance with Boeing Alert Service Bulletin 747-23A2241, Revision 3, dated September 5, 1991. \n\n\t\t\t(i)\tIf chafing or wear is found, prior to further flight, repair or replace the ACESS cable and install teflon expandable sleeving in accordance with the service bulletin. \n\n\t\t\t(ii)\tIf no chafing or wear is found, install teflon expandable sleeving on the ACESS cable in accordance with the service bulletin. \n\n\t\t(2)\tInspect all advanced cabin entertainment and service system (ACESS) seat to seat cables for chafing and wear in accordance with Boeing Alert Service Bulletin 747- 23A2241, Revision 3, dated September 5, 1991. \n\n\t\t\t(i)\tIf chafing or wear is found, prior to further flight, repair or replace the ACESS cable, and ensure proper installation in accordance with the service bulletin. \n\n\t\t\t(ii)\tIf no chafing or wear is found, ensure proper cable installation in accordance with the service bulletin. \n\n\t\t(3)\tModify the ACESS wire bundle installation at the dado panel near each sidewall disconnect in accordance with Boeing Alert Service Bulletin 747-23A2241, Revision 3, dated September 5, 1991. \n\n\t(b)\tAn alternative method of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. \n\n\tNOTE: The request should be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO. \n\n\t(c)\tSpecial flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD. \n\n\t(d)\tThe inspections, repairs, and modifications shall be done in accordance with Boeing Alert Service Bulletin 747-23A2241, Revision 3, dated September 5, 1991, which contains the following list of effective pages: \n\t\n\n\nPage Number\nRevision Level\nDate\n1, 4-7, 10, 14-16, 24-26 \n\n3\nSeptember 5, 1991 \n2, 3, 8-9, 11-13, 17-23 \n2\nNovember 1, 1990 \n\n\n\tThis 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 Airplane Group, P.O. Box 3707, Seattle, Washington 98124. Copies may be inspected at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington, or at the Office of the Federal Register, 1100 L Street N.W., Room 8401, Washington, D.C. \n\n\tThis amendment (39-8079, AD 91-23-10) becomes effective on January 7, 1992.