Learjet 35 - Page 48

2B-24 Developed for Training Purposes Leerjet 35/36
December 1998
CAE SimuFlite
If test fails: the failed axis (PITCH and/or ROLL) annuncia-
tors flash. The MON annunciator remains illuminated. Cycle
the AUTOPILOT switch to extinguish the annunciators.
Autopilot must not be used in any axis that fails the autopilot
monitor check. If it is intended to use autopilot with a failed
axis, the failed axis DC CB (AFCS PITCH or AFCS ROLL)
must be pulled.
Yaw Dampers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED
Yaw Dampers (FC 200 autopilot):
Primary PWR/TEST Button. . . . . . . . .DEPRESS AND HOLD
Check that the PWR/TEST and PRI ENG lights illuminate.
Primary PWR/TEST Button. . . . . . . . . . . . . . . . . . .RELEASE
Ensure the PWR/TEST remains illuminated and that the
PRI ENG light extinguishes.
Secondary PWR/TEST Button . . . . . .DEPRESS AND HOLD
Check that the PWR/TEST and SEC ENG lights illuminate.
Secondary PWR/TEST Button . . . . . . . . . . . . . . . .RELEASE
Ensure the PWR/TEST remains illuminated and that the
SEC ENG light extinguishes.
Yaw Force Indicator . . . . . . . . . . . . . . . . . . . . . . . . .CENTER
Rotate control wheel to center.
SEC ENG Button . . . . . . . . . . . . . . . . . . . . . . . . . DEPRESS
Ensure SEC ENG light illuminates.
Rudder Pedals . . . . . . . . . . . DEPRESS ONE/THEN OTHER
NOTE: Significantly lower rudder pedal force required to
overpower yaw damper.