CESSNA
SECTION
7
MODEL 2088 (675 SHP) AIRPLANE AND SYSTEMS DESCRIPTION
10.AUXILIARY FUEL PUMP ON (AMBER)
-
lndicates the auxiliary
fuel pump is operating.
11.STANDBY ELECTRICAL POWER ON (AMBER)
-
lndicates the
standby alternator is supplying electrical power to the bus.
12.FUEL PRESSURE LOW (AMBER)
-
lndicates fuel pressure in
the fuel manifold assembly is below
4.75
psi.
13.NOT USED. (Some Airplanes); INVERTER INOP (AMBER)
-
lndicates the selected inverter is not operating (Airplanes with
KFC-250 Autopilot).
14.STARTER ENERGIZED (GREEN)
-
lndicates the starter-
generator is operating in the starter mode.
15.FUEL SELECT OFF (RED)
-
lndicates one or both fuel tank
selectors are off.
16.IGNITION ON (GREEN)
-
lndicates electrical power is being
supplied to the engine ignition system.
17.DE-ICE PRESSURE (GREEN)
-
lndicates pressure in the de-ice
boot system has reached approximately 15 psig.
18.WINDSHIELD ANTI-ICE (GREEN)
-
lndicates electrical power is
being supplied to the windshield anti-ice power relay.
ISSTANDBY ELECTRICAL POWER INOPERATIVE (AMBER)
-
lndicates electrical power is not available from the standby
alternator.
20.CHIP DETECTOR (AMBER)
-
lndicates that metal chips have
been detected in either the reduction gearbox case, or accessory
gearbox case.
21 .BATTERY HOT (AMBER)
-
lndicates the electrolyte temperature
in the optional Ni Cad battery is excessively high.
22.BATTERY OVERHEAT (RED)
-
lndicates the electrolyte
temperature in the optional Ni Cad battery is critically high.
23.NOT USED.
24.DOOR WARNING (RED)
-
lndicates the upper cargo door and1
or upper aft passenger doors (Passenger Version only) are not
latched.
Figure
7-6. Typical Annunciator Panel (Sheet 2 of 2)
-
Revision 23
=,
U.S. 7-23
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