Engine Failure During Flight - Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

SECTION 3
EMERGENCY PROCEDURES
ENGINE FAILURES

ENGINE FAILURE DURING FLIGHT

1. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 95 KIAS
2. POWER Lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
3. PROP RPM Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . FEATHER
4. FUEL CONDITION Lever . . . . . . . . . . . . . . . . . . . . . . CUTOFF
5. WING FLAPS Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
6. FUEL BOOST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
7. FUEL/OIL SHUTOFF Knob . . . . . . . . . . . . . . . . . . . . PULL OFF
8. IGNITION Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
9. STBY ALT PWR Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
10. Electrical Load. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE
a. AVIONICS STBY PWR Switch . . . . . . . . . . . . . . . . . . . OFF
b. AVIONICS BUS TIE Switch . . . . . . . . . . . . . . . . . . . . . OFF
c. CABIN Lights Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
d. STROBE Lights Switch . . . . . . . . . . . . . . . . . . . . . . . . . OFF
e. LDG and TAXI/RECOG Lights Switches. . . . . . . . . . . . OFF
Keep LDG and TAXI/RECOG lights OFF until required for
approach and landing. Prior to landing, turn both LEFT and
RIGHT LDG light switches to ON.
f. VENT AIR FANS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
g. AIR CONDITIONING (if installed) . . . . . . . . . . . . . . . . . OFF
h. GEN CONT and
GEN FIELD Circuit Breakers . . . . . . . . . . . OPEN (pull out)
i. RIGHT PITOT HEAT Circuit Breaker . . . . . OPEN (pull out)
j. RDNG LIGHT Circuit Breaker. . . . . . . . . . . OPEN (pull out)
k. RADAR R/T Circuit Breaker . . . . . . . . . . . . OPEN (pull out)
(AVN BUS 1, second row, sixth breaker from left side)
l. AVIONICS No. 2 Switch . . . . . . . . . . . . . . . . . . . . . . . . OFF
11. BAT AMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
12. Land as soon as possible. (refer to EMERGENCY LANDING
WITHOUT ENGINE POWER)
3-10
NOTE
(top row, last two breakers on forward end)
(second row, third breaker from aft end)
(third row, second breaker from aft end)
U.S.
CESSNA
MODEL 208B 867 SHP
GARMIN G1000
(verify below 45 amps)
FAA APPROVED
208BPHCUS-00