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

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