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AD 93-24-15 ACTIVE

Instrument Panel Light Rheostat
Key Information
AD Number 93-24-15 Status Active
Effective Date February 11, 1994 Issue Date Not specified
Docket Number 93-CE-43-AD Amendment 39-8764
Product Type ["Aircraft"] Product Subtype ["Small Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) Cessna Aircraft Company Textron Aviation Inc.
Model(s) F150F F150G F150H F150J F172E F172F F172G F172H FR172E FR172F FR172G 150F 150G 150H 150J 172E 172F (USAF T-41A) 172G 172H (USAF T-41A) 172I 172K 180H 180J 185D 185E R172E R172F R172G R172H
Regulatory Text

93-24-15 CESSNA AIRCRAFT COMPANY: Amendment 39-8764. Docket No. 93-CE-43-AD. Applicability: The following model and serial number airplanes, certificated in any category: \n\n\nModels\nSerial Numbers \n150F, 150G, \n150H, and 150J. \n15061533 through 15071128.\nF150F, F150G,\t\nF150H, and F150J. \nF150-0001 through F150-0529. \n172E, 172F, 172G,\n172H, 172I, and\n172K (T-41A). \n17250573 through 17259223.\nF172E, F172F,\n F172G, and F172H. \nF172-0019 through F17200754.\nFR172E, FR172F,\nand FR172G. \nFR17200001 through FR17200225. \n180H and 180J.\n18051446 through 18052384. \n185D, 185E,\nand 185F. \n185-0777 through 18502310. \nR172E, R172F,\n R172G, and \nR172H (T-41B,\n T-41C, and T-41D). \nR172-0001 through R172-0452.\n\n\tCompliance: Required within the next 6 calendar months after the effective date of this AD, unless already accomplished. \n\n\tTo prevent an in-flight fire caused by a short in the electrical wiring controlled by the instrument panel light dimming rheostat,accomplish the following: \n\n\t(a)\tReplace the existing instrument panel light dimming rheostat with one of improved design that is current-limited and heat-protected, part number RD-0015H-1600, in accordance with Cessna ACCOMPLISHMENT INSTRUCTIONS SEB92-33R1, Revision 1, dated June 25, 1993. \n\n\t(b)\tSpecial flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished. \n\n\t(c)\tAn alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be approved by the Manager, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Wichita Aircraft Certification Office. \n\n\tNOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita Aircraft Certification Office. \n\n\t(d)\tThe replacement required by this AD shall be done in accordance with Cessna ACCOMPLISHMENT INSTRUCTIONS SEB92-33R1, Revision 1, dated June 25, 1993. 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 Cessna Aircraft Company, P.O. Box 7704, Wichita, Kansas 67277. Copies may be inspected at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. \n\n\t(e)\tThis amendment becomes effective on February 11, 1994.