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