CESSNA
MODEL 208B 867 SHP
GARMIN G1000
ENGINE MALFUNCTIONS
RED OIL PRESS LOW ANNUNCIATOR COMES ON
1. OIL PSI Indication. . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
If oil pressure indications confirm warning annunciator,
proceed in accordance with ENGINE FAILURE
checklists, or at the discretion of the pilot and consistent
with safety, continue engine operation in preparation for
an emergency landing as soon as possible.
UNCOMMANDED ENGINE POWER REDUCTION TO IDLE
1. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
2. EMERGENCY POWER Lever . . SET POWER AS REQUIRED
Amber EMERG PWR LVR annunciator will come on once
EMERGENCY POWER lever is moved out of NORMAL.
•
The EMERGENCY POWER lever overrides normal
fuel control functions and results in the direct
operation of the fuel metering valve. Utilize slow and
smooth movement of the EMERGENCY POWER
lever to avoid engine surges, and/or exceeding ITT,
N
and torque limits.
g
•
MAXIMUM RATED power may not be achievable at
all temperatures and altitudes when using the
EMERGENCY POWER lever.
RED EMERG PWR LVR ANNUNCIATOR COMES ON
PRIOR TO OR DURING ENGINE START
1. EMERGENCY POWER Lever . . . . . . . . . . . . . . . . . . . CHECK
FAA APPROVED
208BPHCUS-00
EMERGENCY PROCEDURES
CAUTION
(maintain 65% N
g
CAUTION
(verify lever in NORMAL position)
SECTION 3
minimum during flight)
U.S.
3-27