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PERFORMANCE AND
SPECIFICATIONS
GROSS WEIGHT:
T&keoff
•
•
•
•
,
•
La.nding
.
.
.
.
.
SPEED BEST POWER MIXTURE:
Maximum - Sea Level
.
,
Maximum Recommended Cruise
75% Power at 7500
ft.
.
RANGE, RECOMMENDED LEAN MIXTURE:
Maximum Recommended Cruise
75% Power at 7500 ft.
600 lbs. , No Reserve ,
75'.£ Pow'er at 7500 ft.
978 lbs., No Reserve ,
75% Power at 7500
ft.
1218 lbs. , No Reserve
Maximum Range
10, 000
ft. ,
600 lbs. , No Reserve
10,000 ft., 978 lbs., No Reserve
10,000 ft., 1218 lbs., No Reserve
RATE-OF-CLHfB AT SEA LEVEL:
Twin Engine .
.
Single Engine
.
SERVICE CEILING:
Twin Engine .
TA~5;;i;E~~~~~cE:
·Takeoff
Spe~d
(s2 · KIAs, '150
Fiap~)
Ground Run
.
.
.
.
.
.
,
.
.
Total Distance Over 50-foot Obstacle
,
.
LANDING PERFORMANCE:
Approach Speed (93 KIAS, 5400 lbs)
Ground Roll ,
.
.
.
,
•
.
.
.
Total Distance Over 50-foot Obstacle
EMPTY WEIGHT:
(Approximate}
310
310 II
.
,
BAGGAGE ALLOWANCE:
WING LOADING:
POWER LOADING:
FUEL CAPACITY:
TOTAL
Sta:~~~dA~xiiia~y
Tanks (40°gai.
~sable)
With Auxiliary Tanks (63 gal. usable)
.
.
.
.
,
.
.
With Auxiliary Tanks (63 gal. usable) and Wing Locker Tanks
OIL CAPACITY:
TOTAL
ENGINES:
Continental 6-Cylinder
Fuel Inject ion Engines
285 Rated HP at 2700 RPM
PROPELLERS :
Constant Speed, Full Feathering
Three Blade 76. 5" Diameter ,
5500 lbs.
5400 lbs,
207 Knots
194 Knots
616 Naut. Mi.
3.19 hrs.
193 Knots
1006 Naut. Mi.
5.21 hrs.
193 Knots
1253 Na.ut. Mi.
6.49 hrs.
193 Knots
772 Naut. Mi.
4.98 hrs.
155 Knots
1258 Naut. Mi.
8.12 hrs.
155 Knots
1567 Naut. Mi,
10.11 hrs.
155 Knots
1662 fpm.
370 fpm.
19,750 ft.
7400 ft.
1335 ft.
1700 ft.
640
ft.
1790 ft.
3251 lbs.
3417 lbs.
950 lbs.
30.73 lbs./sq. ft.
9.65 lbs. /hp.
102 gals.
143 gals.
166 gals.
207 gals.
6.5 gals.
I0-520-M
3AF32C87 /82NC-5. 5
•Single engine service ceiling increases 300 feet for each 30 minutes of flight.
THIS OWNER'S MANUAL COVERS THE OPERATION OF THE 310 AND 31011 AIRCRAFT SERIAL
NUMBER 310R0001 THRU 310R0500
01518-13
COPYRIGHT
© 1985
Cessna Aircraft Company
Wichita, Kansas USA
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