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AD 90-10-51 ACTIVE

Control Wheels
Key Information
AD Number 90-10-51 Status Active
Effective Date August 27, 1990 Issue Date Not specified
Docket Number 90-NM- Amendment 39-6700
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) 737-300 Series 737-400 Series 737-500 Series
Regulatory Text

90-10-51 BOEING: Amendment 39-6700. Final copy of telegraphic AD. Docket No. 90-NM- 99-AD. \n\n\tApplicability: Model 737-300, -400, and -500 series airplanes, line number 1488 through line number 1866, certificated in any category. \n\n\tCompliance: Required as indicated, unless previously accomplished. \n\n\tTo prevent the separation of the control wheel from the control column, accomplish the following: \n\n\tA.\tWithin 72 hours (clock hours, not flight hours) after the effective date of this AD, perform a visual inspection of the control wheels (pilot and co-pilot) for missing cotter pins and damaged threads on the attach bolts. \n\n\t\t1.\tIf the cotter pin is in place, properly installed, and no exposed bolt thread damage is evident, no further action is required. \n\n\t\t2.\tIf the cotter pin is missing, prior to further flight, check for proper installation of the nut and install a new cotter pin in accordance with the Boeing Model 737 Maintenance Manual. \n\n\t\t3.\tIf any exposed bolt thread is found damaged, prior to further flight, replace the nut, bolt, and cotter pin with new parts in accordance with the Boeing Model 737 Maintenance Manual. \n\n\tB.\tWithin 48 hours after completion of the inspection required by paragraph A., above, for each airplane, submit a report of findings, positive or negative, to the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region, Transport Airplane Directorate (Fax Number (206) 431-1913). This report must include the model of airplane inspected and line number. \n\n\tC.\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 (ACO), FAA, Transport Airplane Directorate. \n\n\tNOTE: The request should be submitted directly to the Manager, Seattle ACO, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Seattle ACO. \n\n\tD.\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 documents from the manufacturer, may obtain copies upon request to Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue, S.W., Renton, Washington. \n\n\tPortions of this amendment were effective earlier to recipients of telegraphic AD T90- 10-51, issued May 15, 1990. \n\tThis amendment (39-6700, AD 90-10-51) becomes effective on August 27, 1990.