Shutdown And Securing Airplane - Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

SECTION 4
NORMAL PROCEDURES

SHUTDOWN AND SECURING AIRPLANE

1. PARKING BRAKE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
2. BLEED AIR HEAT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
3. TEMP Control Knob . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED
4. VENT AIR FANS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
5. AIR CONDITIONING Switch (if installed) . . . . . . . . . . . . . . OFF
6. POWER Lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
7. ITT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STABILIZED
8. PROP RPM Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . FEATHER
9. FUEL CONDITION Lever . . . . . . . . . . . . . . . . . . . . . . CUTOFF
10. LIGHTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
11. FUEL BOOST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
12. N Indication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
g
Verify engine is spooling down properly and N
below 10% prior to setting the AVIONICS No. 1 switch to
OFF. Engine indications will not be shown after AVIONICS
No. 1 switch is positioned to OFF.
13. AVIONICS No. 1 and No. 2 Switches . . . . . . . . . . . . . . . . . OFF
14. BATTERY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
15. Control Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSTALL
16. OXYGEN Supply Control Lever (if installed) . . . . . . . . . . . . OFF
17. FUEL TANK SELECTORS . . . . . . . LEFT OFF or RIGHT OFF
Turn high wing tank off if parked on a sloping surface to prevent
crossfeeding.
18. Tiedowns and Chocks . . . . . . . . . . . . . . . . . . . . AS REQUIRED
19. External Covers. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSTALL
20. Oil Breather Drain Can . . . . . . . . . . . . . . . . . . . . . . . . . . DRAIN
Possible delays of subsequent flights, or even missed
flights, are often eliminated by routinely conducting a brief
postflight inspection. Usually, a visual check of the airplane
for condition, security, leakage, and tire inflation will alert
the operator to potential problems, and is therefore
recommended.
4-42
(depress brake pedals and pull handle out)
(at minimum temperature for one minute)
NOTE
NOTE
U.S.
MODEL 208B 867 SHP
GARMIN G1000
(rotate FULL counterclockwise)
indication is
g
FAA APPROVED
208BPHCUS-00
CESSNA
(until empty)