Crew: one
Capacity: one passenger (plus two children not exceeding 120 lb (54 kg) on optional bench seat in baggage space)
Length: 23 ft 11 in (7.29 m)
Wingspan: 33 ft 2 in (10.11 m)
Height: 8 ft 6 in (2.59 m)
Wing area: 160 sq ft (15 m2)
Aspect ratio: 6.7:1
Airfoil: NACA 2412
Empty weight: 1,122 lb (509 kg)
Max takeoff weight: 1,600 lb (726 kg)
Fuel capacity: 22.5 US gal (18.7 imp gal; 85 L) usable internal fuel

Powerplant: Continental O-200-A air-cooled horizontally-opposed engine, 100 hp (75 kW)
Propeller: 2-bladed McCauley 1A102/OCM metal fixed-pitch propeller, 5 ft 9 in (1.75 m) diameter [9]

Performance
Maximum speed: 109 kn (125 mph, 202 km/h) at sea level
Cruise speed: 82 kn (94 mph, 152 km/h) at 10,000 ft (3,050 m) (econ cruise)
Stall speed: 42 kn (48 mph, 78 km/h) (flaps down, power off)
Never exceed speed: 140 kn (160 mph, 260 km/h)
Range: 420 nmi (480 mi, 780 km) (econ cruise, standard fuel)
Service ceiling: 14,000 ft (4,300 m)
Rate of climb: 670 ft/min (3.4 m/s)
Take-off run to 50 ft (15 m): 1,385 ft (422 m)
Landing run from 50 ft (15 m): 1,075 ft (328 m)

Airplane time state:
TTAF 2958
TTE 1569

VFR avionics

9/10

10/10

All documentation is in perfect order.
For any test contact me.