Cessna Grand Caravan 208B G1000 Manual page 108

SECTION 3
EMERGENCY PROCEDURES
GENERATOR FAILURE (Amber GENERATOR OFF CAS
MSG)
(Continued)
IF GEN AMPS IS STILL ZERO:
d. GENERATOR Switch . . . . . . . . . . . . . . . . . . . . . . . . . TRIP
e. AVIONICS BUS TIE Switch . . . . . . . . . . . . . . . . . . . . . . ON
f. AVIONICS STBY PWR Switch . . . . . . . . . . . . . . . . . . . . ON
AVIONICS No. 1 and No. 2 Switches must remain ON in
order for the battery to power the avionics buses.
g. Electrical Load . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE
(1) CABIN Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(2) POWER OUTLETS Switch . . . . . . . . . . . . . . . . . . OFF
(3) STROBE Switch . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(4) LDG and TAXI/ RECOG Switches. . . . . . . . . . . . . OFF
Keep LDG and TAXI/ RECOG OFF until required for
approach and landing. Prior to landing, only turn LEFT LDG
light ON to keep electrical load below limit.
(5) VENT AIR FANS . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(6) AIR CONDITIONING (if installed) . . . . . . . . . . . . . OFF
(7) GEN CONT and GEN FIELD Circuit Breakers . . PULL
(8) RIGHT PITOT HEAT Circuit Breaker. . . . . . . . . . PULL
(9) RDNG LIGHT Circuit Breaker . . . . . . . . . . . . . . . PULL
(10) RADAR R/T Circuit Breaker . . . . . . . . . . . . . . . . PULL
(AVN BUS 1, second row, sixth breaker from left side)
(11) HF RCVR and HF AMP Circuit Breakers . . . . . . PULL
h. ALT AMPS . . . . . . . . . . . . . . . . VERIFY BELOW 75 AMPS
i. Flight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONTINUE
With Standby Alternator powering the electrical system, the
flight can continue to destination airport with the Amber
GENERATOR OFF CAS message displayed. Monitor
alternator load using ENGINE SYSTEM page.
3-24
NOTE
NOTE
(top row, last two breakers on forward end)
(second row, third breaker from aft end)
(third row, second breaker from aft end)
(AVN BUS 2, second row, fifth and
(continue shedding if not below 75 amps)
NOTE
U.S.
MODEL 208B G1000
sixth breakers from left side)
FAA APPROVED
208BPHBUS-01
CESSNA