SECTION 3 CESSNA
EMERGENCY PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
ELECTRICAL POWER SUPPLY SYSTEM
MALFUNCTIONS (Continued)
RED VOLTAGE HIGH ANNUNCIATOR COMES ON
(Continued)
9. Electrical Load. . . . . . . . . . . . . . . . . . . . . REDUCE (Continued)
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)
10. Flight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONTINUE
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.
(Continued Next Page)
208BPHCUS-00
3-32
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