Leerjet 35/36 Developed for Training Purposes 2B-11
February 2007
Expanded Normal Procedures
Check pitch trim within takeoff segment on pitch trim indica-
tor.
Left Stall Warning Switch . . . . . . . . . . . . . . . . . . . . . . . . . ON
An inverter must be on.
Test Button . . . . . . . . . . . . . . . . . . . . .DEPRESS AND HOLD
FC 200 Autopilot:
Hold the control column at mid-travel. The overspeed
warning sounds and the stick puller moves the control
column aft with an approximate 18 lbs force.
FC 530 Autopilot:
Control column moves aft with approximately 18 pounds
force and the aural overspeed warning sounds. After
approximately
1/2 second, the puller and overspeed warning-
ceases. After approximately
1/2 additional second, the puller
and overspeed warning activate again and then cease. On
all S/Ns through 35-670 and 36-063, after approximately
another 1/2 second, the overspeed warning sounds again to
check the 300 KIAS speed switch in the ADU.
Test Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .RELEASE
Mach Trim:
Rotary Test Switch . . . . . . . . . . . . . . . . . . . . . . .MACH TRIM
Test Button . . . . . . . . . . . . . . . . . . . . .DEPRESS AND HOLD
Visually check the pitch trim indicator. Depress and hold the
test button. The pitch trim system runs nose-up for one to
three seconds and then stops. The Mach trim annunciator
illuminates and the overspeed warning horn sounds.
Release the test button. Mach trim annunciator extinguishes
and horn ceases.
Test Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .RELEASE
Stall Warning:
Aircraft with Standard Wing, refer to AFM for check.
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