Learjet 35 - Page 46

2B-22 Developed for Training Purposes Leerjet 35/36
February 2002
CAE SimuFlite
Autopilot Monitor. . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED
Autopilot Monitor (FC 200 Autopilot):
AUTOPILOT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Ensure the PWR annunciator on the Autopilot Controller
illuminates.
TEST Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DEPRESS
Check that all annunciators on the Autopilot Controller illu-
minate.
ADI/HSI Flags . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK
Ensure that all flags have disappeared to indicate that verti-
cal and directional gyros have been energized long enough
to time-out erection cycles (approximately 90 seconds).
ENG Button. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DEPRESS
ROLL, PITCH, and LVL annunciators illuminate. The autopi-
lot then opposes movement of the flight controls.
TEST Button . . . . . . . . . . . . . . . . . . . .DEPRESS AND HOLD
Control Wheel Trim Switch . . . . . . . . . . . . . . . . . . . . . . . LWD
Without depressing arming button, move to LWD. ROLL
annunciator extinguishes and autopilot disconnect horn
sounds within five seconds. Hold wheel at wings level posi-
tion.
Trim Switch/TEST Button . . . . . . . . . . . . . . . . . . . .RELEASE
ENG Button. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DEPRESS
TEST Button . . . . . . . . . . . . . . . . . . . .DEPRESS AND HOLD
Control Wheel Trim Switch . . . . . . . . . . . . . . . . . . . . . . .RWD
Without depressing arming button, move to RWD. ROLL
annunciator extinguishes and autopilot disconnect horn
sounds within five seconds. Hold wheel at wings level posi-
tion.
Trim Switch/TEST Button . . . . . . . . . . . . . . . . . . . .RELEASE
ENG Button. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DEPRESS
ROLL, PITCH, and LVL annunciators illuminate. The autopi-
lot then opposes movement of the flight controls.