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AD 89-08-09 ACTIVE

Pulley Bracket
Key Information
AD Number 89-08-09 Status Active
Effective Date April 24, 1989 Issue Date Not specified
Docket Number Unknown Amendment 39-6188
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) 747-100 Series 747-100B Series 747-100B SUD Series 747-200B Series 747-200C Series 747-200F Series 747-300 Series 747-400 Series 747-400D Series 747-400F Series 747SP Series 747SR Series
Regulatory Text

89-08-09 BOEING: Amendment 39-6188. \n\tApplicability: Model 747 series airplanes, as listed in Boeing Alert Service Bulletin 747- 76A2074 dated January 19, 1989, certificated in any category. \n\n\tCompliance: Required as indicated, unless previously accomplished. \n\n\tTo eliminate the potential for uncommanded thrust operation due to engine control cable rupture, accomplish the following: \n\n\tA.\tWithin the next 30 days after the effective date of this AD, inspect control cable pulley bracket assemblies of the outboard engines located at Inboard Leading Edge Station (ILES) 1116 for proper installation and wear, and attach decals, in accordance with the accomplishment instructions of Boeing Alert Service Bulletin 747-76A2074, dated January 19, 1989. \n\n\tB.\tIf the installation is incorrect, prior to further flight, remove and install the pulley bracket in the correct position; and/or if parts are found to be worn, prior to further flight, replace worn parts; in accordance with theaccomplishment instructions of Boeing Service Bulletin 747-76A2074. \n\n\tC.\tReport any incorrect pulley bracket installations detected during the inspections required by paragraph A., above, to the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region, within seven days after the completion of the inspection. \n\n\tD.\tAn alternate means 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, FAA, Northwest Mountain Region. \n\n\tNote: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who may add any comments and then send it to the Manager, Seattle Aircraft Certification Office. \n\n\tE.\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\tAll persons affected by this directive who have not already received the appropriate service information from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. This information may be examined at FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, FAA, Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington. \n\n\tThis amendment (39-6188, AD 89-08-09) becomes effective on April 24, 1989.