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Cessna 208B - Emergencydescentprocedures; Inverter Failure (Amber Inverter Lnop Annunciator On); Roughair; Starter Contactor Does Not Disengage after Engine Start (Amber Starter Energized Annunciator On)

Cessna 208B
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SECTION 3
CESSNA
-
EMERGENCYPROCEDURES MODEL 2088 (675 SHP)
I
ELECTRICAL POWER SUPPLY SYSTEM
MALFUNCTIONS
(Continued)
INVERTER FAILURE (Amber INVERTER INOP
Annunciator On) (Airplanes Equipped with KFC-250
Autopilot Only)
1. Inverter Swrtch
-
SELECT other inverter.
2.
Fa~led lnverter
-
REPAIR before next flight.
If INVERTER
INOP annunciator remains on:
3. lnverter 1 and 2 Circuit Breakers
-
CHECK IN.
4.
If the left-hand gyros are flagged, the INVERTER INOP
annunciator is correct.
5.
Disregard left-hand gyros, land as soon as practical, and repair
inverters.
STARTER CONTACTOR DOES NOT DISENGAGE AFTER
ENGINE START (Amber STARTER ENERGIZED
Annunciator On)
1.
Battery
Switch
-
OFF.
2.
Auxiliary
Power Unit
-
OFF,
then
DISENGAGE.
3. Fuel
Condition
Lever
-
CUTOFF.
4.
Engine Shutdown -COMPLETE.
EMERGENCYDESCENTPROCEDURES
ROUGH AIR
1.
Seats, Seat Belts, Shoulder Harnesses
-
SECURE
2.
Power Lever
-
IDLE.
3. Propeller Control Lever
-
MAX (full foiward)
4. Wing Flaps
-
UP.
5. Weights and Airspeed:
8750 Pounds
-
148 KlAS
7500 Pounds
-
137 KlAS
6250 Pounds
-
125 KlAS
5000 Pounds
-
112 KlAS
(Continued Next Page)
1
3-26 U.S.
Revision 23

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