Learjet 35 - Page 58

2B-34 Developed for Training Purposes Leerjet 35/36
February 2007
CAE SimuFlite
Windshield Heat. . . . . . . . . . . . . . . . . . . . . . . . . . . . PURGED
Aircraft with 450 pressurization:
In-NORMAL/Out-DEFOG Knob . . . . . . . . . . . . . . PULL OUT
WSHLD HEAT-MAN-AUTO Switch. . . . . . . . . . . . . . . . AUTO
Until water has cleared.
WSHLD OV HT Light . . . . . . . . . . . . . . . . . . . . . . .MONITOR
When moisture has cleared:
WSHLD HEAT AUTO-MAN Switch. . . . . . . . . . . . . . . . . MAN
WSHLD HEAT ON-OFF Switch . . . . . . . . . . . . . . . . . . . OFF
Hold until airflow stops.
In-NORMAL/Out-DEFOG Knob . . . . . . . . . . . . . . . .PUSH IN
Aircraft with 510 pressurization:
WSHLD HEAT ON-OFF Switch . . . . . . . . . . . . . . . . . . . . ON
Until water has cleared.
WSHLD OV HT Light . . . . . . . . . . . . . . . . . . . . . . .MONITOR
When moisture has cleared:
WSHLD HEAT ON-OFF Switch . . . . . . . . . . . . . . . . . . . OFF
Fuel Control Governors . . . . . . . . . . . . . . . . . . . . CHECKED
Left Thrust Lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
If the engine accelerates uncontrolled during the following
steps, turn fuel computer on until engine stabilizes at idle,
then shut down and correct the problem.
L Fuel Computer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
L FUEL CMPTR annunciator illuminates. Engine RPM may
increase or decrease slightly and then stabilize.
When RPM stabilizes:
Left Thrust Lever. . . . . . . . . . . . . . ADVANCE AND RETARD
Advance thrust lever and watch for an increase in turbine
RPM and that turbine speed follows the thrust lever. If tur-
bine speed fails to respond to thrust lever, shut down engine
and correct the problem