SECTION 4
NORMAL PROCEDURES
,-
CESSNA
MODEL
2088 (675 SHP)
I
PREFLIGHT INSPECTION
(Continued)
0
RIGHT WlNG Leading Edge
WARNING
IT IS ESSENTIAL IN COLD WEATHER TO REMOVE
EVEN SMALL ACCUMULATIONS OF FROST, ICE,
I
SNOW OR SLUSH FROM THE WING 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.
1. Navigation and Strobe Lights
-
CHECK condition and cleanliness.
2. Fuel Quantity
-
VISUALLY CHECK. See Figure 4-2 for fuel
I
quantity versus depth if using Universal XL Fuel Gage.
-
3.
Fuel ~iller Cap -SECURE.
4. Outboard Fuel Tank Sump Quick-Drain Valve (if installed and
air~lane ~arked with one wing low on a slo~ina ram)
-
DRAIN
(using fuel sampler) to check for water, sedime6t and'proper fuel
before each
fliaht and after each refuelma. If
water
is
observed,
take further
sahples until clear. Take repeated samples from all
fuel drain
Doints until all contamination has been removed.
5.
pitoffstatic Tube
-
CHECK security, openings for stoppage and
warmth.
6.
Landing and Taxi Lights
-
CHECK condition and cleanliness.
1
7. Wing Deice Boots (if installed)
-
CHECK for tears, abrasion and
cleanliness.
1
8. Radome (if installed)
-
CHECK condition and security.
9.
Wing Tie-Down
-
DISCONNECT.
1
10.Wing Strut Deice Boots (if installed)
-
CHECK for tears, abrasion,
and cleanliness.
I1 .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.
12.Main Landing Gear
-
CHECK proper tire inflation and condition of
gear.
(Continued Next Page)
1
4-12 U.S.
Revision
23
To Next Page
Loading...
