Comparison of Grob G-120A and Piper PA-28 Cherokee

Attribute	Piper PA-28 Cherokee ×	Grob G-120A ×
General
Manufacturer	Piper Aircraft	Grob Aircraft
Model	Piper PA-28 Cherokee	Grob G-120A
Country	United States	Germany
Manufactured from (year)	1961	1999
Type	Private Single Engine	Aerobatic
Icao	PA28	G120
Performance
Engine	1x Lycoming O-320-E2A	1x 1 × Lycoming AEIO-540-D4D5 6-cylinder
Power, hp (hp)	150	260
Avionics	-	IFR instrumentation with EFIS and King / Bendix components
Max cruise speed (km/h)	200	319
Approach speed (km/h)	87	104
Travel range (km)	861	1,537
Fuel economy (km/l)	-	6.996
Service ceiling (m)	4,359	5,486
Rate of climb (m/sec)	3.35	6.5
Take off distance (m)	502	707
Landing distance (m)	564	562
Weights
Max take off weight (kg)	975	1,490
Max landing weight (kg)	975	1,440
Max payload (kg)	421	220
Fuel tank capacity (l)	189	252
Baggage volume (m³)	0.6	-
Dimensions
Seats	4	2
Cabin height (m)	1.09	-
Cabin width (m)	1.01	-
Cabin length (m)	2.5	-
Exterior length (m)	7.1	8.11
Tail height (m)	2.22	2.66
^1↑Fuselage diameter (m)	1.15	1.3
Wing span (m)	9.14	10.18
Wing tips	No Winglets	No Winglets