Document ID: chunk:federal_register_of_legislation:F2006B08589:body:0:p1
Version: federal_register_of_legislation:F2006B08589
Segment Type: other
Provision Reference: 
Character Range: 4–3242

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

    Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes

    AD/CL-600/29 Horizontal Stabiliser Trim Actuator 6/95

DM

    Applicability: All Canadair CL-600 aircraft as follows:

               Model Serial Numbers

               CL-600-1A11 1004 to 1085

               CL-600-2A12 3001 to 3066
    CL-600-2B16 5001 to 5299 excluding 5138 Requirement:              1. Perform the following operational check of the Horizontal Stabilizer Trim
                 Actuator (HSTA) brake:

                   1. Press the CHAN 1 INOP/CHAN 2 INOP switch/light and then the OVSP/CHNG CHAN switch/light on the centre pedestal control panel.

b.   Set and hold the pitch trim switch on the pilot's control wheel until the stabilizer is in full NOSE UP position.

c.    Set and hold the pitch trim switch on the pilot's control wheel to NOSE DOWN position and while the stabilizer is moving, press the PITCH TRIM DISC switch on the pilot's control wheel when the needle on the stabilizer trim position indicator reaches the first marking of the take-off configuration green band. Verify that both CHAN INOP lights are on.

d.   Verify that the stabilizer over-travel is less than one degree, as read on the stabilizer trim position on the centre instrument panel.

               Note: One increment on the stabilizer trim position indicator is equal to one degree of stabilizer travel.

               If the stabilizer over-travel is less than or equal to one degree, the pitch trim brake performance meets the ground performance requirements and is serviceable.

               If the stabilizer over-travel is more than one degree, refer to Requirement 2.

                 2.    Action in accordance with the Accomplishment Instructions Part A of Bombardier Inc, Canadair Business Aircraft Division Alert Service Bulletin A600-0645 or A601-0443, both dated 11 January 1995, as applicable.

                 3.    Action in accordance with the Accomplishment Instructions Part B of Bombardier Inc, Canadair Business Aircraft Division Alert Service Bulletin A600-0645 or A601-0443, both dated 11 January 1995, as applicable.

               Note: Transport Canada Aviation AD CF-95-02 dated 28 February 1995 refers.
 COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

               Compliance: 1. a. Initially, if there has not been a report of a previous HSTA overspeed annunciation, within 20 hours time in service from 31 March 1995 and thereafter every 100 hours time in service, or

                1.  b. If there has been a report of a previous HSTA overspeed annunciation then, before each flight after 31 March 1995.

               2.             Before further flight, if the aircraft fails the Requirement 1 checks.

               3.    a. If there have been previous reports of HSTA overspeed annunciation, then within 50 flight cycles after 31 March 1995, or

               3. b. Within 50 flight cycles following a reported incident of HSTA overspeed annunciation after