AD 83-22-06

83-22-06 CESSNA: Amendment 39-4763. Applies to the following airplanes certificated in any category:

Model Serial Number 152 15282032 thru 15284659, 15284661 thru 15284684, 15284686 thru 15284851, 15284853 thru 15285417, 15285419 thru 15285621, 15285623 thru 15285625, 15285627 thru 15285651, 15285653 thru 15285681, 15285683, 15285685 thru 15285693, 15285695 thru 15285700, 15285702 thru 15285713, 15285716 thru 15285719, 15285722 thru 15285724, 15285726 thru 15285728, 15285730 thru 15285731, 15285733 thru 15285744, 15285748, 15285750, 15285751, 15285753, 15285756, 15285757, 15285759, 15285760, 15285764, 15285765, 15285767, 15285769, 15285772, 15285773, 15285778, 15285779, 15285781, 15285783, A152 A1520809 thru A1520990, A1520992 thru A1520997, A1520999 thru A1521020, A1521022, 172N 17271035 thru 17274009, 172P 17274010 thru 17275806, 17275809, 17275817 thru 17275854, 17275857, 17275861 thru 17275881, 17275883 thru 17275910, 17275912 thru 17275947, 17275949 thru 17275953, 17275955 thru 17275958, 17275960 thru 17275971, 17275973, 17275974, 17275976, 17275978, 17275980 thru 17275982, 17275984, 17275986 thru 17275992, 17275994, 17275995, 17275997, 17275999 thru 17276002, 17276005, 17276010, 17276012, 17276014, 172Q 17275869 thru 17275881, 17275883 thru 17275910, 17275912 thru 17275947, 17275949 thru 17275953, 17275955 thru 17275958, 17275960 thru 17275971, 17275973, 17275974, 17275976, 17275978, 17275980 thru 17275982, 17275984, 17275986 thru 17275992, 17275994, 17275995, 17275997, 17275999 thru 17276002, 17276005, 17276010, 17276012, 17276014, 172RG 172RG0001 thru 172RG1134, 172RG1137, R172K R1722930 thru R1723454, 180K 18053001 thru 18053203, 182Q 18266591 thru 18267715, 182R and 18267716 thru 18268103, 18268105 thru 18268107, T182 18268109 thru 18268129, 18268131 thru 18268141, 18268143, 18268144, 18268146 thru 18268293, 18268295, 18268310, 18268312 thru 18268322, 18268324 thru 18268327, 18268330 thru 18268332, 18268335, 18268336, 18268339, 18268343, 18268345, 18268348, 18268350, R182 and R18200584 thru R18201912, R18201914 thru R18201933, TR182 R18201935 thru R18201938, R18201940, R18201942, R18201943, R18201945, R18201946, R18201949, R18201950, R18201953, R18201954, A185F 18503684 thru 18504334, 18504336, 18504337, 18504339 thru 18504395, 18504397, 18504398, 18504400, F152 F15201529 thru F15201883, F15201885 thru F15201896, F15201898 thru F15201931, F15201933, F15201935, F15201936, FA152 FA1520348 thru FA1520382, F172N F17201750 thru F17202039, F172P F17202040 thru F17202146, F17202148 thru F17202175, F17202177 thru F17202181, F17202183 thru F17202186, F17202189 thru F17202194, F17202197, F17202200, F17202202, FR172K FR17200631 thru FR17200675, Fl82Q F18200095 thru F18200169, FR182 FR18200021 thru FR18200070,

Compliance: Required as indicated, unless already accomplished.

To prevent possible loss of an aileron hinge pin, accomplish the following:

a) Within the next 100 hours time in service, after the effective date of this AD, visually inspect each aileron hinge (6 total) for correct location of the cotter pin in accordance with Figure 1. of this AD or Cessna Service Information Letter SE83-18 dated July 29, 1983.

1. If the cotter pin holes are correctly located the airplane may be returned to service without further action.

2. If the cotter pin holes are incorrectly located, prior to further flight modify or replace aileron hinges in accordance with instructions in Figure 1. of this AD or Cessna Service Information Letter SE83-l8 dated July 29, 1983.

b) Airplanes may be flown in accordance with FAR 21.197 to a base where this AD may be accomplished.

c) An 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.

This amendmentbecomes effective on November 8, 1983.

Figure 1. Aileron Hinge Inspection, Modification or Replacement.