Caproni Vizzola C22 Ventura

1st Flight 1980

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 hard points 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.

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