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Agusta CP-110 & CP-111

In 1951, the Agusta CP-110, also referred to as CVV P.110 or Politecnico P.110, took its first flight as a prototype Italian four-seat light aircraft.

Despite being evaluated by the Italian Air Force, the aircraft did not garner attention from either civil or military operators.

The original design was created by CVV (Centro Volo a Vela del Politecnico di Milano), with plans for production aircraft to be manufactured by Agusta.

However, due to a lack of interest, production did not proceed.

Variants

CP-111

The Agusta CP-111, a three-seat version of the CP-110, was designed by engineer Ermenegildo Preti and first took flight in 1951.

It was constructed with a wooden frame covered in plywood.

Setting it apart from its predecessor, the CP-111 featured a fixed landing gear and an upgraded power plant equipped with an Avco Lycoming 0-435-1 engine.

However, despite the more powerful engine, the CP-111’s flight performance suffered in comparison to the CP-110 at the same take-off weight due to increased drag caused by the fixed landing gear and wider engine.

Specifications

CP-110

Crew

1

Capacity

3 passengers

Length

7.30 m (23 ft 11 in)

Wingspan

10.60 m (34 ft 9 in)

Wing area

16.0 m2 (172 sq ft)

Empty weight

680 kg (1,499 lb)

Gross weight

1,100 kg (2,425 lb)

Powerplant

1 × Alfa Romeo 110-ter,

Four-cylinder air-cooled inverted inline engine,

108 kW (145 hp)

Performance

Maximum speed

275 km/h (171 mph, 148 kn)

Cruise speed

240 km/h (150 mph, 130 kn)

Stall speed

90 km/h (56 mph, 49 kn)

Range

1,000 km (620 mi, 540 nmi)

Take-off run.

170 m (560 ft)

Landing run

170 m (560 ft).

Sources

Jane’s Encyclopedia of Aviation-M J H Taylor.

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