Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 838

SECTION 9 - SUPPLEMENTS
SUPPLEMENT 15
ABNORMAL PROCEDURES
ELECTRICAL
MALFUNCTIONS
AMBER BATTERY HOT ANNUNCIATOR COMES ON
(Continued)
5. 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
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)
h. RDNG LIGHT Circuit Breaker. . . . . . . . . . . OPEN (pull out)
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
(AVN BUS 2, second row, fifth and sixth breakers from left
side)
6. STBY ALT PWR Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
7. AVIONICS STBY PWR Switch . . . . . . . . . . . . . . . . . . . . . . . ON
8. AVIONICS BUS TIE Switch. . . . . . . . . . . . . . . . . . . . . . . . . . ON
9. ALT AMPS. . . . . . . . . . . . . . . . . . . . VERIFY BELOW 75 AMPS
10. Flight . . . . . . . . . . . . . . . . . . LAND AS SOON AS PRACTICAL
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.
U.S.
S15-8
(Continued)
POWER
(Continued)
NOTE
(first row, last two breakers on forward end)
(third row, second breaker from aft end)
(continue shedding if not below 75 amps)
NOTE
MODEL 208B 867 SHP
GARMIN G1000
SUPPLY SYSTEM
OPEN (pull out)
FAA APPROVED
208BPHCUS-S15-00
CESSNA