Document ID: chunk:federal_register_of_legislation:F2006B05080:body:0
Version: federal_register_of_legislation:F2006B05080
Segment Type: other
Provision Reference: 
Character Range: 0–1674

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Cessna 180, 182 and Wren 460 Series Aeroplanes

AD/CESSNA 180/68 Aileron Hinge Pin 1/84

Applicability:  Model             Serial Number
                180K              18053001 thru 18053203,
                182Q              18266591 thru 18267715,
                182R and T182     18267716 thru 18268103, 18268105 thru 18268107, 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 TR182    R18200584 thru R18201912, R18201914 thru R1820193, R18201935 thru R18201938, R18201940, R18201942, R18201943, R18201945, R18201946, R18201949, R18201950, R18201953, R18201954,
                F182Q             F18200095 thru F18200169,
                FR182             FR18200021 thru FR18200070.

Requirement: Action in accordance with Cessna S.I.L. SE 83-18.

Note: FAA AD 83-22-06 refers.

            Compliance: Unless already accomplished within 100 hours time in service after 31 January 1984 or at the next scheduled inspection for Maintenance Release issue after 31 January 1984 whichever is the later.

            Background:  Possible migration and loss of the aileron hinge pin could result if the retaining split pin holes are incorrectly located.