Learjet 35 - Page 36

2B-12 Developed for Training Purposes Leerjet 35/36
February 2004
CAE SimuFlite
With FC 200 Autopilot:
During heavy wind conditions, it may be necessary to head
aircraft into the wind to prevent wind from blowing stall
warning vanes up.
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
STALLWARNING Switches. . . . . . . . . . . . . . . . . . . . . . . . ON
TEST Selector Switch. . . . . . . . . . . . . . . . . . . . . . . . L STALL
Test Button . . . . . . . . . . . . . . . . . . . . .DEPRESS AND HOLD
The pilot’s angle-of-attack indicator needle begins to sweep
from the green segment to the red segment. As the needle
passes the green-yellow margin, the shaker actuates and
the L STALL warning annunciator flashes. As the needle
advances to the red segment, the pusher activates briefly,
then stops. The L STALL warning annunciator illuminates
steadily just prior to or at pusher actuation. After pusher
stops, the needle sweeps back and remains in the yellow or
green segment. Pusher release must occur or the test has
failed.
Test Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .RELEASE
TEST Selector Switch. . . . . . . . . . . . . . . . . . . . . . . . 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
malfunction except during pusher actuation or system test.
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DN
Check that both angle-of-attack indicators shift position
three times as flaps are lowered to full down.
STALL WARNING Switches . . . . . . . . . . . . . . . . . . . . . . OFF