CESSNA SECTION
7
MODEL 2088 (675 SHP) AIRPLANE AND SYSTEMS DESCRIPTION
FUEL
SYSTEM
(Continued)
I
FUEL
QUANTITY
DATA
FUEL
I
'
I I
I
NOTE
I
POUNDS
I I
I I
1.
Poundslgallons in light-faced type are capacities for SIN
20880001 thru 20880089 not modified with SK208-52 (wing
tank external sump).
U.S.
GALLONS
2. Poundslgallons in bold-faced type are capacities for SIN
20880001 thru 20880089 modified with SK208-52 (wing tank
external sump) and SIN 20880090 and On.
3.
Pounds are based on a fuel specific weight of
6.7
pounds per
U.S. gallon.
FULL
(OUTBOARD
FILLERS)
1122.25
1124.25
WARNING
I
FULL
(OUTBOARD
FILLERS)
167.5
167.8
TO ACHIEVE FULL CAPACITY, FILL FUEL TANK TO
THE
TOP OF THE FUEL FILLER NECK. FILLING FUEL
2244.5
2248.5
TA~K~'T~'
TK.ETOM-OF
THE
FUEL
FILLER
COLLARE (LEVEL WITH THE FLAPPER VALVE)
ALLOWS SPACE FOR THERMAL EXPANSION AND
RESULTS IN A DECREASE IN FUEL CAPACITY OF
FOUR GALLONS PER
SIDE (EIGHT GALLONS
335
335.6
TOTAL).
Figure 7-1 3. Fuel Quantity Data
20.1
24.1
Fuel rejected by the engine on shutdown drains into a fireproof fuel can
located on the front left side of the firewall. The can should be drained
during preflight inspection. If left unattended, the can fuel will overflow
overboard.
2224.4
2224.4
3.0
3.6
(Continued Next Page)
332
332
U.S. 7-73
To Next Page
Loading...
