CESSNA
SECTION 4
~,
MODEL
2088
(675 SHP)
NORMAL PROCEDURES
~,
I
SYSTEMS CHECKS
(Continued)
AUTOPILOT CHECK (KING KFC-150)
(Continued)
4. Manual Electric Trim
-
TEST as follows:
A. Actuate left side of split switch unit to the fore and aft positions.
The trim wheel should not move on its own. Rotate the trim
wheel manually against the engaged clutch to check the pilot's
trim overpower capability.
B.
Actuate right side of split switch unit to the fore and aft
positions. The trim wheel should not move on its own and
normal trim wheel force is required to move it manually.
C. Press the
NP DlSCRRlM INTER switch down and hold.
Manual electric trim should not operate either nose up or nose
down.
5.
Flight Director
-
ENGAGE by pressing FD or CWS button.
6. Autopilot
-
ENGAGE by pressing AP ENG button.
7. Yaw Damper (Optional)
-
ENGAGE by pressing YAW DAMP
switch button.
8.
Flight Controls
-
MOVE fore, aft, left, and right to verify that the
-
autopilotlyaw damper can be overpowered.
9.
NP DISC/TRIM INTER Switch
-
PRESS. Verify that the autopilot
and yaw damper (optional) disconnects and all flight director
modes are canceled.
10.TRIM -SET to takeoff position.
AUTOPILOT CHECK (KING KAP-150)
s
Refer to Section 9 of this Pilot's Operating Handbook, STC
I
Supplement K3G, for complete information.
=,
NOTE
When autopilot is turned on wh~le airplane is on the ground,
the control wheel should be held to prevent ailerons from
.
banging stops.
--
BEFORE TAKEOFF RELlABlLlN TESTS
=,
NOTE
1
Perform steps
1
thru
9
prior to each flight
-
1.
Gyros -Allow 3-4 minutes for gyros to come up to speed
=*
2. AVIONICS POWER
1
Switch -ON.
-
(Continued Next Page)
=,
--
1
Revision 23
-a
.
e
U.S. 4-29
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