Koolhoven F.K.50
The Koolhoven F.K.50 was a 1930s Dutch eight-passenger light transport monoplane designed and built by Koolhoven.
Koolhoven F.K.50 | |
---|---|
Role | Eight-passenger light transport monoplane |
Manufacturer | N.V.Koolhoven |
Designer | Frits Koolhoven |
First flight | 1935 |
Introduction | 1935 |
Retired | 1962 |
Primary user | Swiss Alpar |
Number built | 3 |
Development
The F.K.50 was designed to meet a requirement from the Swiss airline Swiss Alpar for a light transport capable of operating in Switzerland. The F.K.50 was a cantilever high-wing cabin monoplane with a fixed wide track tailwheel landing gear. The fuselage was of welded steel tube construction, covered with fabric. The tailplane was of similar construction. The wings were wooden construction, covered with plywood. It was powered by two Pratt & Whitney Wasp Junior T1B engines and had a conventional single fin and rudder. The first of two aircraft first flew on the 18 September 1935 and the second flew in March 1936.[1]
A third aircraft, designated F.K.50A, was built in 1938 with a re-designed tail unit with twin vertical tail surfaces. It had a longer nose and larger mainwheels, with a higher all-up weight.[1]
Two bomber variants, designated F.K.50B, were proposed but never built. The first was a straight conversion of the F.K.50; the second would have been powered by 830 horsepower (620 kW) Bristol Mercury VIS radial engines. It would have been operated by a crew of four and carried a 2,200 pounds (1,000 kg) bomb load.[1]
Operational history
The three aircraft operated a regular service between Swiss destinations and onwards to Lyons and Marseilles and charter flights to Paris and London.
F.K.50
- HB-AMI
The first to be built, the aircraft entered service in October 1935. During World War II, the aircraft operated weekly between Berne and Croydon, United Kingdom. The aircraft was scrapped in 1947.[1]
- HB-AMO
The second to be built, the aircraft crashed on landing 25 kilometers from Basle Airport on 10 September 1937 with the loss of three lives.[1]
Variants
Specifications (F.K.50)
Data from Jane's All the World's Aircraft 1938.[2]
General characteristics
- Crew: 2
- Capacity: 8 passengers
- Length: 14 m (45 ft 11 in)
- Wingspan: 18 m (59 ft 1 in)
- Height: 3.7 m (12 ft 2 in)
- Wing area: 44.7 m2 (481 sq ft)
- Empty weight: 2,730 kg (6,019 lb)
- Gross weight: 4,250 kg (9,370 lb)
- Fuel capacity: 410 kg (904 lb) fuel and oil
- Powerplant: 2 × Pratt & Whitney Wasp Junior T1B 9-cylinder air-cooled radial piston engines, 300 kW (400 hp) each
- Propellers: 2-bladed variable-pitch propellers
Performance
- Maximum speed: 265 km/h (165 mph, 143 kn) at sea level
- Cruise speed: 255 km/h (158 mph, 138 kn) at 2,500 m (8,202 ft)
- Landing speed: 95 km/h (59 mph; 51 kn)
- Range: 1,000 km (620 mi, 540 nmi)
- Service ceiling: 5,000 m (16,000 ft)
- Absolute ceiling: 5,500 m (18,045 ft)
- Absolute ceiling on one engine: 1,800 m (5,906 ft)
- Rate of climb: 4.75 m/s (935 ft/min)
- Time to altitude:
- 1,000 m (3,281 ft) in 3 minutes 12 seconds
- 2,000 m (6,562 ft) in 7 minutes 15 seconds
- 3,000 m (9,843 ft) in 12 minutes 42 seconds
- Wing loading: 95.1 kg/m2 (19.5 lb/sq ft)
- Power/mass: 0.15 kW/kg (0.09 hp/lb)
References
Sources
Wikimedia Commons has media related to Koolhoven F.K.50. |
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing. p. 2260.