Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 245

CESSNA
MODEL 208B 867 SHP
GARMIN G1000
STARTING ENGINE (With External Power)
18. FUEL BOOST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
a. Amber FUEL BOOST ON Annunciator . . . . . . . . . CHECK
b. Amber FUEL PRESS LOW Annunciator . . . . . . . . CHECK
c. FFLOW PPH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
If the external power unit drops off the line, initiate
engine shutdown.
19. STARTER Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START
a. White IGNITION ON Annunciator . . . . . . . . . . . . . CHECK
b. OIL PSI. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
c. N . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STABLE
g
20. FUEL CONDITION Lever . . . . . . . . . . . . . . . . . . . . . LOW IDLE
a. FFLOW PPH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
b. ITT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
•
If ITT climbs rapidly towards 1090°C, be prepared to
return the FUEL CONDITION lever to CUTOFF
position.
•
Under hot OAT and/or high ground elevation
conditions, idle ITT can exceed maximum idle ITT
limitation of 700°C. Increase N
accessory load to maintain ITT within limits.
c. N . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 55% MINIMUM
g
FAA APPROVED
208BPHCUS-00
(verify annunciator is not shown)
(verify 0 fuel flow PPH indicated)
CAUTION
(1090°C maximum, limited to 2 seconds)
CAUTION
(Continued Next Page)
SECTION 4
NORMAL PROCEDURES
(Continued)
(verify annunciator is shown)
(verify annunciator is shown)
(verify oil pressure indicated)
(12% minimum)
(90 to 140 PPH)
and/or reduce
g
U.S. 4-27