,=
SECTION 4 CESSNA
,=
NORMAL PROCEDURES
MODEL
2086 (675 SHP)
.
BEFORE TAKEOFF
(Continued)
5. Fuel Boost Switch
-
RECHECK NORM.
/=
6. Fuel Tank Selectors
-
RECHECK BOTH ON.
7. Fuel Quantity
-
RECHECK.
8.
Fuel Shutoff
-
RECHECK FULLY ON.
,
-
9. Elevator, Aileron, and Rudder Trim Controls
-
SET for takeoff.
,
.
10.Power Lever
-
400 FT-LBS.
A. Suction Gage -CHECK.
f=
B. Volt/Ammeter
-
CHECK and return selector to BATT position.
f.z
C.
Inertial Separator
-
CHECK. Turn control counterclockwise,
pull to BYPASS position and check torque drop; move control
,.
back to NORMAL position and check that original torque is
regained.
D. Engine Instruments
-
CHECK (See Section 2, Limitations for
minimum oil temperature required for flight).
1l.Overspeed Governor
-
CHECK (stabilized at 1750 t60 RPM)
(See Systems Checks).
12.Power Lever
-
IDLE.
13.Quadrant Friction Lock
-
ADJUST.
14.Standby Power (if installed)
-
CHECK (See Systems Checks).
(
15.Autopilot (if installed)
-
PREFLIGHT TEST (See Systems
Checks).
1
16.Known Icing System (if installed)
-
PREFLIGHT COMPLETE
(See Systems Checks) prior to any flight in icing conditions.
I
17.PitoffStatic Heat
-
ON when OAT is below 4°C (39°F).
18.lce Protection (if installed) -AS REQUIRED.
19.Avionics and Radar (if installed) -CHECK and SET.
20.GPSINAV Switch -SET.
21 .Strobe Lights
-
AS REQUIRED.
22.Annunciators
-
EXTINGUISHED or considered.
23.Wing Flaps -SET at 20".
24.Cabin Heat Mixing Air Control
-
FLT-PUSH.
25.Window
-
CLOSE.
26.Brakes
-
RELEASE.
27.Fuel Condition Lever
-
HIGH IDLE.
28.Standby Power Switch (if installed)
-
ON (Standby Power INOP
Annunciator
-
OFF).
(Continued Next Page)
Revision 23