Caproni Vizzola C22 Ventura

The Caproni Vizzola C22 Ventura was a light jet-powered aircraft developed in Italy for use as a military trainer.

The student and instructor sat side by side under an expansive canopy, and weapons hardpoints were provided under each of the slender, high mounted wings.

Specifications

Crew

Two

Length

6.19 m (20 ft 4 in)

Wingspan

10.00 m (32 ft 10 in)

Height

1.88 m (6 ft 2 in)

Wing area

8.75 m2 (94.2 sq ft)

Aspect ratio

11.42:1

Airfoil

Wortmann FX-67K-170

Empty weight

720 kg (1,587 lb)

Max take-off weight

1,135 kg (2,502 lb)

Fuel capacity

290 L (64 imp gal; 77 US gal)

Powerplant

2 × Micro turbo TRS 18-046 turbojets, 1.0 kN (220 lbf) thrust each

Performance

Maximum speed

480 km/h (300 mph, 260 kn) (max cruise, at sea level)

Cruise speed

324 km/h (201 mph, 175 kn) (econ cruise, at 3,000 m (10,000 ft))

Stall speed

120 km/h (75 mph, 65 kn) EAS, flaps down

Never exceed speed

560 km/h (350 mph, 300 kn)

Range

740 km (460 mi, 400 nmi) on internal fuel

Endurance

2 hr

Service ceiling

7,620 m (25,000 ft)

G limits

+6.0, −3.0

Rate of climb

9.2 m/s (1,810 ft/min)

Armament

Up to 200 kg (440 lb) of stores on under wing pylons.