NOTICE

SECTION 4 CESSNA
NORMAL PROCEDURES MODEL 208B G1000
BEFORE STARTING ENGINE (Continued)
Before starting the engine, the POWER Lever is placed at the IDLE
position (against the BETA gate), the propeller control lever is moved to
the MAX RPM position (full forward), and the FUEL CONDITION Lever
is stowed in the CUTOFF position.
CAUTION
The propeller reversing linkage can be damaged if the
POWER Lever is moved aft of the IDLE position when
the engine is not running and the propeller is feathered.
STARTING ENGINE
The Starting Engine checklist procedures should be followed closely to
assure a satisfactory engine start. With the FUEL CONDITION Lever in
the CUTOFF position, move the starter switch to the START position;
verify that the STARTER ON and IGNITION ON CAS MSG(s) are
displayed. Next, check for a positive indication of engine oil pressure.
After N g stabilizes (minimum of 12%), move the FUEL CONDITION
Lever to the LOW IDLE position and verify fuel flow in the general
range of 90 to 140 pph. After the engine "lights off" and during
acceleration to idle (approximately 52% N g), monitor ITT and N g.
Maximum ITT during engine start is 1090°C, limited to 2 seconds.
Typically, the ITT during start is well below this maximum value. After
the engine has stabilized at idle, the STARTER ON CAS MSG should
be OFF. If this CAS MSG remains ON, it indicates the starter has not
been automatically disengaged during the engine starting sequence
due to a failed speed sensor.
4-36
CAUTION
If no ITT rise is observed within 10 seconds after
moving the FUEL CONDITION Lever to the LOW IDLE
position, or ITT rapidly approaches 1090°C, move the
FUEL CONDITION Lever to CUTOFF and perform the
Engine Clearing Procedure in this section.
U.S.
(Continued Next Page)
FAA APPROVED
208BPHBUS-00