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/ Comparison of Piper PA-30 Twin Comanche and Rockwell Commander 112 / 114
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Comparison of Piper PA-30 Twin Comanche and Rockwell Commander 112 / 114
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Attribute
Rockwell Commander 112 / 114
×
Piper PA-30 Twin Comanche
×
General
Manufacturer
Rockwell International
Piper Aircraft
Model
Rockwell Commander 112 / 114
Piper PA-30 Twin Comanche
Country
United States
United States
Manufactured from (year)
1972
1963
Manufactured to (year)
2005
1972
Type
Private Single Engine
Twin Turboprops
Icao
AC11
PA30
Performance
Engine
1x 1 × Lycoming IO-540-T4B5D
2x Lycoming O- 320
Power, hp (hp)
260
160
Avionics
Garmin GNC-300XL
-
Max cruise speed (km/h)
307
330
Approach speed (km/h)
104
111
Travel range (km)
1,356
1,852
Fuel economy (km/l)
5.083
-
Service ceiling (m)
5,304
5,669
Rate of climb (m/sec)
5.44
7.42
Take off distance (m)
655
470
Landing distance (m)
366
570
Weights
Max take off weight (kg)
1,479
1,690
1
↑
Max landing weight (kg)
1,424
1,690
Max payload (kg)
446
310
Fuel tank capacity (l)
265
454
Dimensions
Seats
4
4
Cabin height (m)
1.24
-
Cabin width (m)
1.19
-
Cabin length (m)
1.9
-
Exterior length (m)
7.63
7.67
Tail height (m)
2.57
2.5
Fuselage diameter (m)
1.3
1.2
Wing span (m)
9.98
11.22
Wing tips
No Winglets
No Winglets
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