Cessna Skyhawk Owner's Manual page 6

Registration Number,
1-6
Surfaces,
4 Regulator,
voltage, 2-4
aluminum,
4-2
Reverse Polarity
Contactor, 2-4,
painted,
4-2
6-2
System,
cabin
heating/ventilation,
2-5
electrical,
2-3
5
fuel,
2-1
6 owner
follow-up,
4-10
Sample Loading Problem,
3-4
gy
Secure Aircraft,
1-4
Selector
Valve, Fuel,
2-2
Service
Ceiling,
inside front cover
Servicing Intervals Check List,
4-8
Table of
Contents,
iii
Servicing
and Lubrication
Tachometer,
1-6, 3-3
EXTERIOR
Note
Procedures,
4-7
Take-Off, inside front cover, 1-2,
Servicing Requirements Table
2-8
INSPECTION h
u
aes
inSideback
cover
before, 1-2,
2-8
ud ge I au condi
Shimmy
Dampener,
4-8
crosswind,
2-9
nspecuen-
Shock Strut, Nose Gear, 4-9, inside
data,
5-3
1
K night
night
is planned,
back cover
maximum performance
1-2 gÊ,°iiie°iuan
Short
Field Landing,
2-12
normal,
1-2
flashlight is available.
Spark
Plugs,
4-8
performance
charts,
2-9
Specification and Grade,
power
check,
2-8
fuel,
inside back cover
wing flap settings,
2-9
hydraulic fluid,
inside
back
Taxiing,
2-6
cover
diagram,
2-7
oil, inside
back
cover
Throttle
1-6
2-2
a. Turn on
master
switch and check
fuel quan-
a possibility
that
Lhe fuel tank sumps contain I ?
Lity indicators, then
turn
master switch off.
waLer.
Thus, the fuel
tank
sump drain plugs
Specifications
-
Performance,
Tire
Pressures,
inside back cover
b. Check ignition switch
"OFF". and fuel line drain
plug should be removed
to
inSide
front cover
c. Check fuel selector valve handle
on "BUTH". check for Lhe presence of water.
. .
TOrque
Links, Nose Gear,
4-8
d. Remove control wheel lock.
c,
Check propeller and sµinner for nicks and
Speed, mside front cover
True Airspeed Indicator,
6-5
e. Check baggage door for security.
d.
seheucrk ny<>se
wheel strut and tire for proper
Speeds, Climb, 1-3, 2-10,
5-3
inna
=-
Split Bus Contactor,
2-4
a. Hemove rudder
gust lock, if installed.
e.
Disconnect
lie-down
rope.
b. Disconnect
Lail
tie-down.
f. Inspect airspeed static source hole
on
side of
Stalling Speeds Chart,
5-2
fuselage for stoppage
(lefL
side only)
Stalls,
2-11
iLn
e ire
on
proper
innation. a. Remove puoi tube
cover,
U instaHed, and
Starter,
2-4
Utility
Category, Maneuvers,
3-2
check pilot tube oµening for stoppnge.
Starter Contactor,
2-4
a. Check
oil level. Do not operate with less s
llanknient
oenening
>r
stoµpage
Starter/Ignition Switch,
1-8
than six quarts. Fill for extended
flight, stoppage. Starting Engine,
1-2, 2-5,
2-13
h. I3efore first flight of day and after each
re-
fueling, pull out strainer drain knob for
Static Pressure Alternate Source
V
about four seconds to
clear
fuel sLrniner
of Same as
Valve
1-6 6-2
possible water and
sediment. Check strainer i i
drainclosed. Ifwaterisobserved,there.is
Strainer, Fuel,
2-2,
4-7,
4-8
VacuumSystemAirFilter,
4-9
Suction Gage,
1-6
Vacuum System Oil Separator,
4-8
Syct.ion Relief
Valve
Inlet Screen, Valve,
Fuel Selector,
2-2
Figure
1-1.
4-8
Voltage Regulator,
2-4
.
Index-5
1V