CESSNA SECTION 3
MODEL 208B 867 SHP ABNORMAL PROCEDURES
GARMIN G1000
U.S.
FAA APPROVED
ELECTRICAL POWER SUPPLY SYSTEM
MALFUNCTIONS (Continued)
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)
(top row, last two breakers on forward end)
(8) RDNG LIGHT Circuit Breaker. . . . . . . OPEN (pull out)
(third row, second breaker from aft end)
(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 OPEN (pull out)
(AVN BUS 2, second row, fifth and sixth breakers from
left side)
(11) ALT AMPS . . . . . . . . . . . . VERIFY BELOW 75 AMPS
(continue shedding if not 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.
208BPHCUS-00 3-85
To Next Page
Loading...
