2-14 FAA APPROVED 4-30-76
REISSUED 2-25-81, CHANGE 13
BEFORE STARTING ENGINES (CONT)
e. Actuate pilot’s and copilot’s control wheel trim and trim arm-
ing switches and pedestal NOSE DN-OFF-NOSE UP switch.
Trim motion shall not occur.
f. PITCH TRIM Switch —þPRI.
g. Pedestal NOSE DN-OFF-NOSE UP Switch — Operate NOSE
UP, then NOSE DN. Trim motion shall not occur.
h. Pilot’s Control Wheel Trim Switch — Without depressing arm-
ing button, move switch to LWD, RWD, NOSE UP and NOSE
DN; trim motion shall not occur. Depress arming button; trim
motion shall not occur. Then depress arming button and move
switch to LWD, RWD, NOSE UP and NOSE DN; trim motion
shall occur.
i. Repeat step h. for copilot’s control wheel trim switch.
j. Trim by positioning copilot’s control wheel trim switch, then
trim in the opposite direction using the pilot’s control wheel
trim switch. Pilot’s trim shall override copilot’s trim. Repeat for
each trim position.
k. Pilot’s Control Wheel Trim Switch —þNOSE UP. Then
depress control wheel master switch (MSW); trim motion shall
stop while control wheel master switch (MSW) is held. Repeat
procedure for NOSE DN condition; trim motion shall stop.
l. Repeat step k. using copilot’s control wheel trim switch and
control wheel master switch (MSW).
m. Yaw Trim Switch —þMove each half separately to NOSE
LEFT and NOSE RIGHT. Trim motion shall not occur.
n. Yaw Trim Switch — Move both halves simultaneously to each
position. Trim motion shall occur.
o. Trim — Set all axes for takeoff, and check amber T.O. TRIM
light not illuminated. On aircraft 35-146 & subsequent, and
aircraft 36-046 & subsequent, and prior aircraft incorporat-
ing AAK 83-8, determine Stabilizer Trim Setting by referring
to Figure 2-2.
22. Autopilot Monitor Check:
The following procedure accomplishes the autopilot
monitor preflight check. For a complete autopilot oper-
ational check, refer to the Flight Manual Supplement for
J.E.T. FC-200 Automatic Flight Control System.
a. AUTOPILOT Switch — ON. The PWR light on the Autopilot
Controller (glareshield) will illuminate.
b. TEST Button — Depress. All lights on the Autopilot Controller
will illuminate.
NOTE
◆
2-14 FAA APPROVED 4-30-76
REISSUED 2-25-81, CHANGE 13
BEFORE STARTING ENGINES (CONT)
e. Actuate pilot’s and copilot’s control wheel trim and trim arm-
ing switches and pedestal NOSE DN-OFF-NOSE UP switch.
Trim motion shall not occur.
f. PITCH TRIM Switch —þPRI.
g. Pedestal NOSE DN-OFF-NOSE UP Switch — Operate NOSE
UP, then NOSE DN. Trim motion shall not occur.
h. Pilot’s Control Wheel Trim Switch — Without depressing arm-
ing button, move switch to LWD, RWD, NOSE UP and NOSE
DN; trim motion shall not occur. Depress arming button; trim
motion shall not occur. Then depress arming button and move
switch to LWD, RWD, NOSE UP and NOSE DN; trim motion
shall occur.
i. Repeat step h. for copilot’s control wheel trim switch.
j. Trim by positioning copilot’s control wheel trim switch, then
trim in the opposite direction using the pilot’s control wheel
trim switch. Pilot’s trim shall override copilot’s trim. Repeat for
each trim position.
k. Pilot’s Control Wheel Trim Switch —þNOSE UP. Then
depress control wheel master switch (MSW); trim motion shall
stop while control wheel master switch (MSW) is held. Repeat
procedure for NOSE DN condition; trim motion shall stop.
l. Repeat step k. using copilot’s control wheel trim switch and
control wheel master switch (MSW).
m. Yaw Trim Switch —þMove each half separately to NOSE
LEFT and NOSE RIGHT. Trim motion shall not occur.
n. Yaw Trim Switch — Move both halves simultaneously to each
position. Trim motion shall occur.
o. Trim — Set all axes for takeoff, and check amber T.O. TRIM
light not illuminated. On aircraft 35-146 & subsequent, and
aircraft 36-046 & subsequent, and prior aircraft incorporat-
ing AAK 83-8, determine Stabilizer Trim Setting by referring
to Figure 2-2.
22. Autopilot Monitor Check:
The following procedure accomplishes the autopilot
monitor preflight check. For a complete autopilot oper-
ational check, refer to the Flight Manual Supplement for
J.E.T. FC-200 Automatic Flight Control System.
a. AUTOPILOT Switch — ON. The PWR light on the Autopilot
Controller (glareshield) will illuminate.
b. TEST Button — Depress. All lights on the Autopilot Controller
will illuminate.
NOTE
◆
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