Cessna 1971 Super Skymaster - Alphabetical Index

EMERGENCY OPERATION.
(1) Elevator Trim Disengage Switch -- "DISENGAGE," (forward
position).
ALPHABETICAL INDEX
(2) Manual Trim -- As Required.
I AUTOMATIC PROPELLER SYNCHRONIZER I
An optional propeller synchronizer system is available to automatical-
ly match the propeller RPM of both engines. This provides proper pro-
peller synchronization and a Significant reduction in cabin noise level.
The system is comprised of a synchronizer "ON-OFF" control switch
mounted on top of the engine control pedestal, modified propeller gover-
nors, magnetic speed pick ups for each engine, flexible governor shafts
and other associated mechanical components.
When the synchronizer switch is turned "ON, " the propeller RPM of
the
"Slave" engine will automatically adjust to changes in RPM of the
"Master" engine over a limited range. This limiting feature prevents the
slave engine from lOSing more than 75 to 100 RPM in the event the master
engine is feathered wlth the synchronizer "ON". Placing the synchroniz-
er switch in the "OFF" position will automatically center a synchronizer
speed adjustment actuator so that the synchronizer will function normally
when the system is again turned "ON." Optimum operation will be ob-
tained by first manually synchronizing propeller RPM, with reference to
the panel mounted synchroscope (standard eqUipment) and then placing
the synchronizer switch "ON".
NOTE
The propeller synchronizer control switch should be
"OFF" during take-off, landing and single engine opera-
tion.
I
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l
A
Accelerate-Stop Distances Chart,
6-3
After Landing, 1-8
Aircraft File, 5-6
Airspeed Correction Table, 6-1
Airspeed Indicator Instrument
Markings, 4-2
Airspeed Limitations (CAS), 4-2
Alternator and Regulator Switches,
1-10
Alternator Restart Switch, 2-5
Alternators, 2-6
Alternator Start and Test Switches,
1-10
Alternator Switches, 2-5, 2-6
Alternator Warning Diode
Assembly, 2-6
Alternator Warning Lights, 1-10,
2-8
Ammeter, 1-10
selector switch, 2-6
Authorized Operations, 4-1
Automatic Propeller Synchronizer,
7-19
Autopilot Control Unit, 1-10
Autopilot-Omni Switch, 7-9, 7-10
Auxiliary Fuel Indicator Lights,
1-10, 2-3
Auxiliary Fuel Pumps, 2-2
switches, 1-10, 2-2, 2-3
Auxiliary Fuel System, 7-1
Auxiliary Fuel Tanks, 2-2
Auxiliary Mike Jack, 1-10
B
Balked Landing, 1-7, 2-25
Baggage Allowable, inside front
cover
Battery, 2-6
Battery Contactor, 2-6
Before Entering Airplane, 1-1
Before Landing, 1-7, 2-24
Before Starting Engines, 1-4
Before Take-Off, 1-5, 2-19
Boom Microphone, 7-11
Brake Master Cylinders, 5-10
,
C
Cabin Door Operation, 2-17
Cabin Heating, Ventilating and
Defrosting System, 2-15
control panel, 1-10
Care,
exterior, 5-3
interior, 5-4
landing gear, 5-4
propeller, 5-3
Cargo Pack, 4-9, 7-16
flight operation, 7-16
Center of Gravity Envelope, 4-8
Check List, Servicing Intervals,
5-10
Circuit Breakers/Fuses, 2-7,
2-9
Climb, 1-6, 2-21
maximum performance, 1-6
normal, 1-6
Climb Data Table, 6-4
Climb Speeds,
twin-engine, 2-21
Clock, 2-6
Cold Weather Equipment, 7-2
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Index-l
7-20