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7) Using the test stand switch marked "CAPSTAN ROTATION", rotate the test stand motor clockwise (CW) and read of the torque indicated on the torque wrench.
8) Repeat this step rotating the motor counterclockwise (CCW).
NOTE : The reading of the required torque corresponds to the continuous rotation torque.
9) Repeat steps 7) and 8) twice.
NOTE : The mean value of the 6 readings determines the actual friction torque reading value.
10) Compare the actual friction torque to the required friction torque - refer to Table 501.
11) If clutch friction torque is out-of-tolerance, perform the following operations
a) Remove torque wrench (7), adapter (6) and locating pin (3).
b) Hand-hold drive capstan (9).
c) Rotate nut (8) clockwise if friction torque is less than the required torque and counterclockwise if the friction torque is greater than the required torque.
d) Repeat steps 4) thru 11).
12) Disconnect the power supply source.
13) Remove torque wrench (7), locating pin (3) and adapter (6).
14) Remove mounting plate (2) from test stand (1).
15) Install mounting plate (2)
- refer to 22-12-03 for B36 roll servo actuator,
- refer to 22-12-04 for B35 pitch servo actuator,
- refer to 22-12-06 for B38 pitch trim servo actuator.
SERVO ACTUATOR B36 ROLL B35 PITCH B38 PITCH TRIM
Clutch friction torque 20 ± 2 lbf. in
2.26 ± 0.226 N.m 20 ± 2 lbf. in
2.26 ± 0.226 N.m 18 ± 2 lbf. in
2.03 ± 0.226 N.m

Clutch friction torques
Table 501
 
3. CONFIGURATION OF FLIGHT COMPUTER (Table 502)
NOTE : Flight computer configuration is only required when it is replaced.
A. Tools and consumable materials
None
B. Procedure
For configuration of A82 flight computer, refer to HONEYWELL Installation and Maintenance Manual I "KFC 225 automatic flight control system" P/N 006-00776-0000 at the latest amendment.
During the configuration procedure of the flight computer, make sure that values in installation menu display page correspond to the values given in Table 502.

Audio Volume 2
Select 350/256 0
Flaps Analog/Discrete 0 ou/or 1
Voice Msg. Enabled/Disabled 1
ARINC 429 (HSI) Heading 0
ARINC 429 (GPS) Steering 0 : KLN94
1 : GNS430/GNS 530
Dim Bus Voltage 5V/28V 0
AP DISC Disengages FD/Not 1*
Tone Alert at Sel Alt/Not 0
Gyro/Power Valid 0 ou/or 1

Configuration of A82 flight computer
Table 502
I* Aircraft S / N 1900,2056 : 0
AAAA
Validity : KFC 225 22-12 00 Page 505
(BA) JUN 04
 
1 - Test stand
2 - Mounting plate
3 - Locating pin
4 - Washer
5 - Wing nut
6 - Adapter
　
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