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/ Comparison of Cessna 172 Skyhawk and Grob G-120A
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Comparison of Cessna 172 Skyhawk and Grob G-120A
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Attribute
Cessna 172 Skyhawk
×
Grob G-120A
×
General
Manufacturer
Cessna
Grob Aircraft
Model
Cessna 172 Skyhawk
Grob G-120A
Country
United States
Germany
Manufactured from (year)
1956
1999
Type
Private Single Engine
Aerobatic
Icao
C172
G120
Performance
Engine
1x Lycoming O-360 L2A
1x 1 × Lycoming AEIO-540-D4D5 6-cylinder
Power, hp (hp)
160
260
Avionics
Garmin G1000 glass cockpit
IFR instrumentation with EFIS and King / Bendix components
Max cruise speed (km/h)
228
319
Approach speed (km/h)
87
104
Travel range (km)
1,272
1,537
Fuel economy (km/l)
12.916
6.996
Service ceiling (m)
4,115
5,486
Rate of climb (m/sec)
3.71
6.5
Take off distance (m)
497
707
1
↑
Landing distance (m)
407
562
Weights
Max take off weight (kg)
1,157
1,490
Max landing weight (kg)
1,157
1,440
Max payload (kg)
398
220
Fuel tank capacity (l)
212
252
Baggage volume (m³)
0.85
-
Dimensions
Seats
4
2
Cabin height (m)
1.2
-
Cabin width (m)
1
-
Cabin length (m)
3.6
-
Exterior length (m)
8.3
8.11
Tail height (m)
2.72
2.66
Fuselage diameter (m)
1.1
1.3
Wing span (m)
11
10.18
Wing tips
No Winglets
No Winglets
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