83-10-03: Control Wheel Yoke Guide Modification

83-10-03 CESSNA: Amendment 39-4655. Applies to the following airplanes certificated in any category: \n\n\nModel\nSerial Numbers \n172M\n17266940 thru 17267584\n172N\n17267585 thru 17274009\n172P\n17274010 thru 17275762, 17275764, 17275765, 17275769, 17275770, 17275788, 17275792, 17275793, 17275796, 17275798, 17275800 thru 17275803, 17275806, and 17275818\nR172K\nR1722000 thru R1723454\nF172\nF17201445 thru F17202194\nFR172\nFR17200591 thru FR17200675\n\n\tCOMPLIANCE: Required as indicated unless already accomplished. \n\n\tTo prevent possible jamming of the elevator control, accomplish the following: \n\n\ta)\tWithin the next 100 hours time-in-service, modify the right-hand control wheel yoke guide in accordance with the instructions in Cessna Single-Engine Customer Care Service Information Letter SE82-38, dated August 13, 1982, and SE82-38 Revision # 1 dated October 29, 1982. \n\n\tb)\tAirplanes may be flown in accordance with FAR 21.197 to a base where this AD may be accomplished.c)\tAn equivalent method of compliance with this AD may be used if approved by the Manager, Wichita Aircraft Certification Office, Federal Aviation Administration, Room 238, Terminal Building 2299, Wichita, Kansas 67209, telephone (316) 269-7000. \n\n\tThis amendment becomes effective on June 30, 1983.