Cessna 1971 Super Skymaster - Page 59

Cold Weather Operation, 2-25
Compass, Magnetic, 1-10
Control Lever Friction Lock, 1-10
Correction Table, Airspeed, 6-1
Cowl Flap System, 2-13
Cruise Performance, 2-22 6-5,
6-6,
6-7, 6-8, 6-9, 6-10
CruiSing, 1-6, 2-22,
Cylinder Head Temperature Gages,
1-10, 4-3
D
De-Icing System, 7-6
after landing, 7-6
before entering airplane, 7-6
de-icer boot care, 7-7
during engine run-up, 7-13
ill flight, 7-6
operating details, 7-7
Dilution System, 7-3
dilution table, 7-4
Discontinued Take -Off Procedure,
3-3
Ditching, 3-16
Dome Lights, 2-11
Dual Economy Mixture Indicator,
1-10
E
Economy Mixture Indicator, 1-10,
7-16
operating instructions, 7-16
Electric Elevator Trim Disengage
Switch, 1-10
Index-2
Electric Elevator Trim System,
7-18
switch, 1-10
Electrical System, 2-4
alternator restart switch, 2-5
alternators, 2-6
alternator switches, 2-5
alternator warning diode
assembly, 2-6
alternator warning lights, 2-8
ammeter, 2-6
battery, 2-6, 5-10
battery contactor, 2-6
circuit breakers, 2-7, 2-9
clock, 2-6
electroluminescent lighting,
2-10
emergency operation, 3-13
flight hour recorder, 1-10, 2-6
fuses, 2-6, 2-9
ground service receptacle,
2-6, 7-2
high volt and battery discharge
lights, 2-8
ice detector light, 7-5
instrument flood lights, 2-10
Ignition/starter switches, 2-6
light test switch, 2-6
map light, 2-10
master switch, 1-10, 2-5, 2-6
magnetos, 2-6
post lights, 2 -10
propeller synchroscope, 2-12
reverse polarity contactor, 2-6
split bus contactor, 2-6
starter contactors, 2-6
starters, 2-6
voltage indicator lights, 2-6
voltage regulators, 2-6
voltage regulator selector
SWitch, 2-5, 2-6
voltage senSing assembly, 2-6
Electric Outside Air Temperature
Gage, 1-10
j
.inescent Lighting, 2-10
Elevator Trim Control Wheel,
1-10
Emergency Window Exit, 3-17
Empty Weight, inside front cover
Engine Failure During Take-Off,
3-1
Engine Instrument Group, 1-10
Engine Instrument Markings, 4-2
Engine Operation Limitations, 4-2
Engine-Out During Flight, 3-5
Engine Restarts In Flight (After
Feathering), 3-6
Engines, inside front cover
before starting, 1-4
instrument markings, 4-2
operation limitations, 4-2
starting, 1-4, 2-18
Exterior Inspection Diagram, 1-2
Exterior Lighting, 2-11
propeller synchroscope, 2-12
F
Fires, 3-14
electrical fire in flight, 3-14
engine fire in flight, 3-14
Flight Instrument Group, 1-10
Flight Hour Recorder, 1-10, 2-6
Flight in Icing Conditions, 3-15
Flyable Storage, 5-5
Forced Landing
complete power loss, 3-12
ditching, 3-16
precautionary landing with
power, 3-12
Fuel System, 2-1
auxiliary fuel pumps, 2-2
auxiliary fuel pump switches,
2-2, 2-3
auxiliary fuel system, 7-1
auxiliary fuel tanks, 2-2
auxiliary indicator lights, 1-10,
2-4
capacity, inside covers
fuel/air throttle units, 2-2
fuel distributors, 2-2
fuel flow indicators, 2-2, 4-3
fuel injection nozzles, 2-2
fuel instrument group, 1-10
fuel pump/mixture units, 2-2
fuel selector handles, 2-2
fuel selector valves, 2-2, 5-10
fuel tank. fillers, 5-8
main fuel tanks, 2-2
microswitch, 2-2
mixture controls, 1-10, 2-2
quantity indicators, 2-2, 4-2
quantity transmitter, 2-2
schematiC, 2-2
strainers and tank sump drains,
2-2, 2-3, 5-8, 5-10
throttles, 1-10, 2-2
Fuel Quantity and Oil Pressure
Indicators, 1-10
FuseS/Circuit Breakers, 2-6, 2-9
G
Graph,
center of gravity envelope, 4-8
loading, 4-7
Gross Weight, inside front cover
Ground Handling, 5-1
Ground Service Plug Receptacle,
2-6, 7-2
H
Hand Pump, Landing Gear
Emergency, 2-15
Index-3
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