Textron Cessna Grand Caravan Ex 208B - Page 149

CESSNA SECTION 3
MODEL 208B 867 SHP EMERGENCY PROCEDURES
GARMIN G1000
U.S.
FAA APPROVED
ELECTRICAL POWER SUPPLY SYSTEM
MALFUNCTIONS (Continued)
RED VOLTAGE HIGH ANNUNCIATOR COMES ON
(Continued)
IF GENERATOR DOES NOT AUTOMATICALLY TRIP OFFLINE
WITH BUS VOLTS ABOVE 32.5
2. GENERATOR Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TRIP
3. AVIONICS BUS TIE Switch . . . . . . . . . . . . . . . . . . . . . . . . . ON
4. AVIONICS STBY PWR Switch . . . . . . . . . . . . . . . . . . . . . . . ON
5. AVIONICS NO. 1 and NO. 2 Switches . . . . . . . . . . . . . . . . OFF
6. Electrical Load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE
a. CABIN Lights Switch . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
b. POWER OUTLET Switch(es). . . . . . . . . . . . . . . . . . . . OFF
c. BCN Lights Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
d. LDG and TAXI/ RECOG Light Switches. . . . . . . . . . . . OFF
NOTE
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.
e. VENT AIR FANS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
f. AIR CONDITIONING (if installed) . . . . . . . . . . . . . . . . OFF
g. GEN CONT and
GEN FIELD Circuit Breakers . . . . . . . . . . . OPEN (pull out)
(top row, last two breakers on forward end)
h. RDNG LIGHT Circuit Breaker . . . . . . . . . . OPEN (pull out)
(third row, second breaker from aft end)
i. RADAR R/T Circuit Breaker. . . . . . . . . . . . OPEN (pull out)
(AVN BUS 1, second row, sixth breaker from left side)
j. HF RCVR and
HF AMP Circuit Breakers OPEN (pull out)
(AVN BUS 2, second row, fifth and sixth breakers from left
side)
k. ALT AMPS . . . . . . . . . . . . . . . . VERIFY BELOW 75 AMPS
(continue shedding if not below 75 amps)
7. Flight. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONTINUE
NOTE
With Standby Alternator powering the electrical system, the
flight can continue to destination airport with the
GENERATOR OFF annunciator shown. Monitor ALT AMPS
load using ENGINE SYSTEM page.
208BPHCUS-01 3-33