SECTION
4
CESSNA
NORMAL PROCEDURES
MODEL
2088 (675 SHP)
I
PREFLIGHT INSPECTION
(Continued)
LEFT SIDE
(Continued)
-
2.
Main Landina Gear
-
CHECK Drouer tire inflation and condition of
-
-
.
.
gear.
3. Inboard Fuel Tank Sump and External Sump Quick-Drain Valves
-
DRAIN (using fuel sampler) to check for water, sediment, and
proper fuel before each flight and after each refueling. If water is
observed, take further samples until clear. Take repeated
samples from all fuel drain points until all contamination has been
removed.
@
LEFT WlNG Leading Edge
WARNING
IT IS ESSENTIAL IN COLD WEATHER TO REMOVE
EVEN SMALL ACCUMULATIONS OF FROST, ICE,
I
SNOW, OR SLUSH FROM THE WlNG AND CONTROL
SURFACES. TO ASSURE COMPLETE REMOVAL OF
CONTAMINATION, CONDUCT A VISUAL AND TACTILE
INSPECTION OF ALL SURFACES. ALSO, MAKE SURE
THE CONTROL SURFACES CONTAIN NO INTERNAL
ACCUMULATIONS OF ICE OR DEBRIS. PRIOR TO ANY
FLIGHT IN
ICING CONDITIONS, CHECK THAT PlTOTl
STATIC SOURCE AND STALL WARNING HEATERS
ARE WARM TO TOUCH AFTER TURNING
PITOTI
STATIC AND STALL HEAT SWITCHES ON FOR
30
SECONDS, THEN OFF. MAKE SURE THE PlTOT
COVERS ARE REMOVED.
1
1.
Wing Strut Deice Boots (if installed)
-
CHECK for tears, abrasion
and cleanliness.
2.
Wing Tie-Down
-
DISCONNECT.
1
3. Wing Deice Boots (if installed)
-
CHECK for tears, abrasion and
cleanliness.
4. Stall Warning Vane
-
CHECK freedom of movement, audible
1
warning and warmth. (For airplanes equipped with a stall warning
ground disconnect switch, check audible warning with elevator
control off forward stop).
1
5.
Pitot-Static Tube
-
CHECK security, openings for stoppage and
warmth.
6. Landing and Taxi Lights -CHECK condition and cleanliness.
(Continued Next Page)
Revision 23
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