Cessna 208B - Engine Malfunctions; Gear Box Contamination; Loss of Oil Pressure

CESSNA
MODEL
2088 (675 SHP)
SECTION 3
EMERGENCY PROCEDURES
ENGINE MALFUNCTIONS
LOSS OF OIL PRESSURE (Red OIL PRESS LOW
Annunciator ON)
1. Oil Pressure Gage - CHECK oil pressure indication. If oil
pressure gage confirms annunciator warning, proceed in
accordance with Engine Failures 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.
FUEL CONTROL UNIT MALFUNCTION IN THE
PNEUMATIC OR GOVERNOR SECTIONS (Engine Power
Falls Back To Idle)
I. Power Lever - IDLE.
2. Emergency Power Lever - AS REQUIRED (maintain 65% Ng
minimum during flight).
CAUTION
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
.7
LIMITS.
GEAR BOX CONTAMINATION (Amber CHIP DETECTOR
Annunciator ON)
1. Engine Gages - CAREFULLY MONITOR engine gages for
-,
abnormal oil pressure, oil temperature, or power indications.
2. If engine gages are normal, proceed to destination and determine
cause of
chi^ detector annunciator warning ~rior to next flight.
-.
-,
3. If engine gages confirm chip detector annunciator warning,
proceed in accordance with Engine Failures 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.
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