Document ID: chunk:federal_register_of_legislation:F2006B10833:body:0
Version: federal_register_of_legislation:F2006B10833
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Instruments and Automatic Pilots

AD/INST/30 King KAP 100/KAP 150/KFC 150
                          Flight Control System

 Applicability: Flight Computers KC 190, KPN 065-0055-00/-01, all serial numbers.

2/86
                         KC 190, KPN 065-0055-02, serial number 1474 and below. KC 190, KPN 065-0055-03, serial number 10095 and below. KC 191, KPN 065-0054-00/-01, all serial numbers.
                         KC 191, KPN 065-0054-02 & -04, serial number 20754 and below.
                         KC 191, KPN 065-0054-03 & -05, serial number 30227 and below.
                         KC 192, KPN 065-0042-00/-01, all serial numbers.
                         KC 192, KPN 065-0042-02 & -04, serial number 40614 and below.
                         KC 192, KPN 065-0042-03 & -05, serial number 50464 and below.

            Units with serial numbers above those stated have Mod 9 incorporated during original manufacturing.

 Requirement: King SB KC 190/191/192-9.

            Note: FAA AD 85-23-07 also refers.

 Compliance: Within 100 hours time in service after 28 February 1986.

            Background:  To ensure the trim monitor in the flight computer will provide an audible warning signal upon detection of a trim failure.