Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 201

CESSNA
MODEL 208B 867 SHP
GARMIN G1000
ELECTRICAL
MALFUNCTIONS
AMBER GENERATOR OFF ANNUNCIATOR COMES ON
(Continued)
h. Electrical Load . . . . . . . . . . . . . . . . . REDUCE (Continued)
(5) VENT AIR FANS . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(6) AIR CONDITIONING (if installed) . . . . . . . . . . . . . OFF
(7) GEN CONT and
GEN FIELD Circuit Breakers . . . . . . . OPEN (pull out)
(8) RDNG LIGHT Circuit Breaker . . . . . . . OPEN (pull out)
(9) RADAR R/T Circuit Breaker . . . . . . . . OPEN (pull out)
(AVN BUS 1, second row, sixth breaker from left side)
(10) HF RCVR and
HF AMP Circuit Breakers
(AVN BUS 2, second row, fifth and sixth breakers from
left side)
(11) 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 annunciator shown. Monitor ALT AMPS
load using ENGINE SYSTEM page.
FAA APPROVED
208BPHCUS-00
POWER
(Continued)
(top row, last two breakers on forward end)
(third row, second breaker from aft end)
(continue shedding if not below 75 amps)
NOTE
SECTION 3
ABNORMAL PROCEDURES
SUPPLY SYSTEM
OPEN (pull out)
U.S. 3-85