Cessna 210B - Index

Optional Systems
located on the left side of the utility
shelf near the baggage door.
IMPORTANT
Oil, grease , or other lubricants
in contact with oxygen create a
serious fire hazard, and such con-
tact must be avoided. Only a
thread compound approved under
MIL-T-5542 can be used safely
on oxygen systems. Apply only
to the first three threads of male
fittings to prevent thread seizure.
The face masks used with the oxy-
gen system are the partial-rebreath-
ing, disposable type. The masks are
durable and the frequent user can
mark his mask for identification and
reuse it many tim es. Additional
masks and hoses are available from
your Cessna Dealer.
alphabetilal indeH
.- ~ ~~~~~~~~~~~~~~~~~~~~~==~~~~==========
A
Alter Landing, 2-4
Aller Take-Off, 3-5
Air-plane,
before entering, 2-1
file, 6- 5
mooring, 6-1
A irspeed Correction Table, 7-1
AI rspeed Limitations, 5-1
Ammeter, 1-7
Authorized Operations, 5-1
Auxiliary Fuel Pump, 1-5
switch, 1-4
8
Baggage, inSide cover
Battery, 1-7
fla ttery Solenoid, 1-7
A efore Entering Airplane, 2-1
Ilefore Landing, 2-4, 3-8
Be fore Starting Engine, 2-1
Before Take-Off, 2-2, 3-4
c
Cabin Heating and Ventilating
System, 1-10
Cap, Fuel Filler, 1-5
Capacity,
fuel, inside cover
oil, inside cover
Care,
interior, 6-4
landing gear, 6-3
propeller, 6-3
Center of Gravity Moment
Envelope, 5-5
Check, Preflight, 3-1
Circuit Breakers, 1-6
Climb, 2-3, 3-5
maximum performance, 2-3
normal, 2-3
Clock, 1-7
Cold Weather Operation, 3-8
Controls, Engine, 1-1
Correction Table, Airspeed, 7-1
Cowl Flaps, 1-3
Cruise Performance, Optimum, 3-7
Cruise Performance, 7-4, 7-5,
7-6, 7-7, 7-8
CruiSing, 2-4, 3-6
D
Dealer Follow-Up System, 6-6
Diagram,
electrical power distribution,
1-7
exterior inspection, 1-12
fuel flow settings, 1-2
fuel system schematic, 1-5
internal cabin dimensions, 1-11
landing, 7-9
principal dimenSions, iv
servicing, 6-7
Dilution System, Oil, 3-9
dilution table, 3-10
Index-1
8-10