2B-14 Developed for Training Purposes Leerjet 35/36
February 2004
CAE SimuFlite
Test Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .RELEASE
TEST Selector Switch. . . . . . . . . . . . . ROTATE TO R STALL
Test Button . . . . . . . . . . . . . . . . . . . . .DEPRESS AND HOLD
The operation is identical to that of L STALL above except
needle sweeps copilot’s angle-of-attack indicator, and the
R STALL warning annunciator flashes.
Test Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .RELEASE
With STALL WARNING switches in ON, steady illumination
of the L or R STALL warning annunciator indicates a mal-
function except during pusher actuation or system test.
With either control wheel master switch (MSW) depressed:
TEST Selector Switch. . . . . . . . . . . . . . . . . . . . . . . . R STALL
Test Button . . . . . . . . . . . . . . . . . . . . .DEPRESS AND HOLD
Verify that the nudger and pusher do not actuate as the
angle-of-attack indicator moves through the band. The
nudger monitor horn sounds if the needle stays in the yel-
lowsegment.
Test ButtonRELEASE
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DN
Ensure that both angle-of-attack indicator needles make at
least one significant shift in position as flaps are lowered.
STALLWARNING Switches. . . . . . . . . . . . . . . . . . . . . . . OFF
Current Limiter (if installed):
Rotary Test Switch . . . . . . . . . . . . . . . CURRENT LIMITER L
Test Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DEPRESS
The green indicator light illuminates if the left current limiter
is functional.
Rotary Test Switch . . . . . . . . . . . . . . . CURRENT LIMITER R
The green indicator light illuminates if the right current limiter
is functional. Repeat the Current Limiter test after both
engines have been started.
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