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/ Comparison of Cessna 310 and Rockwell Commander 112 / 114
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Comparison of Cessna 310 and Rockwell Commander 112 / 114
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Attribute
Rockwell Commander 112 / 114
×
Cessna 310
×
General
Manufacturer
Rockwell International
Cessna
Model
Rockwell Commander 112 / 114
Cessna 310
Country
United States
United States
Manufactured from (year)
1972
1954
Manufactured to (year)
2005
1980
Type
Private Single Engine
Twin Turboprops
Icao
AC11
C310
Performance
Engine
1x 1 × Lycoming IO-540-T4B5D
2x Continental IO-470-M
Power, hp (hp)
260
240
Avionics
Garmin GNC-300XL
-
Max cruise speed (km/h)
307
352
Approach speed (km/h)
104
126
Travel range (km)
1,356
1,611
Fuel economy (km/l)
5.083
-
Service ceiling (m)
5,304
6,096
Rate of climb (m/sec)
5.44
8.64
Take off distance (m)
655
507
Landing distance (m)
366
546
Weights
Max take off weight (kg)
1,479
2,087
Max landing weight (kg)
1,424
1,293
Max payload (kg)
446
790
Fuel tank capacity (l)
265
473
1
↑
Baggage volume (m³)
-
1
Dimensions
Seats
4
5
Cabin height (m)
1.24
1.2
Cabin width (m)
1.19
1.2
Cabin length (m)
1.9
2.4
Exterior length (m)
7.63
8.3
Tail height (m)
2.57
3.25
Fuselage diameter (m)
1.3
1.3
Wing span (m)
9.98
10.7
Wing tips
No Winglets
No Winglets
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