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