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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
Landing distance (m)
407
562
Weights
Max take off weight (kg)
1,157
1,490
1
↑
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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