Leerjet 35/36 Developed for Training Purposes 2B-13
February 2004
Expanded Normal Procedures
With FC 530 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
STALL WARNING Switches . . . . . . . . . . . . . . . . . . LEFT ON
Ensure L STALL annunciator extinguishes.
STALL WARNING Switches . . . . . . . . . . . . . . . . . LEFT OFF
STALL WARNING Switches . . . . . . . . . . . . . . . . . RIGHT ON
Ensure R STALL annunciator extinguishes
STALL WARNING Switches . . . . . . . . . . . . . . . . . . LEFT ON
TEST Selector Switch. . . . . . . . . . . . . .ROTATE TO L STALL
TEST Button . . . . . . . . . . . . . . . . . . . .DEPRESS AND HOLD
The nudger monitor horn sounds for approximately one sec-
ond and then the pilot’s angle-of-attack indicator needle
begins to sweep from the green segment to the red seg-
ment. As the needle passes the green-yellow margin, the
shaker activates, the nudger actuates, and the L STALL
warning annunciator flashes. High-frequency vibration of the
control column signals shaker actuation. Low frequency for-
ward movement (if not opposed) of the control column sig-
nals nudger actuation. 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.
WARNING: The action of the nudger verifies operation of
the pitch torquer prior to pusher actuation. If, during ground
test, the shaker is not accompanied by the nudger (the
nudger monitor horn will sound) – do not dispatch. If, dur-
ing flight, the shaker is not accompanied by the nudger (the
nudger monitor horn will sound) – do not decelerate fur-
ther.
To Next Page
Loading...
