Koolhoven F.K.48
Koolhoven F.K.48 is a topic that has captured the attention of millions of people around the world. Since its emergence, it has been the subject of debate, discussion and exploration, as experts, scholars and the general public attempt to understand its impact on contemporary society. This article dives into Koolhoven F.K.48, examining its origins, evolution, and current relevance. Through a detailed and insightful analysis, we seek to shed light on this phenomenon, providing a complete and updated vision of its meaning and influence in various areas. By approaching Koolhoven F.K.48 from different angles, the aim is to offer a panoramic view that allows the reader to delve into this topic with a broad and deep understanding.
 | This article includes a list of general references, but it lacks sufficient corresponding inline citations. (February 2015) |
| F.K.48 | |
|---|---|
| |
| Role | Airliner |
| National origin | Netherlands |
| Manufacturer | Koolhoven |
| Designer | Frederick Koolhoven |
| First flight | 24 May 1934 |
| Primary user | KLM |
| Number built | 1 |
The Koolhoven F.K.48 was an airliner built in the Netherlands in 1934 for KLM.
Design and development
The F.K.48 was a conventional, semi-cantilever high-wing monoplane, powered by two engines mounted on the wing leading edges. The undercarriage was of fixed, tailskid type with divided main units. The fuselage was of welded steel tube construction, covered in fabric, which was oval in cross-section at the nose, transitioning to a rectangular cross-section for the passenger cabin. The wings were wooden structures skinned in plywood.[1]
The sole example built was registered PH-AJX and quickly gained the nickname Ajax. It was used by KLM on the Rotterdam-Eindhoven route until 1936, when it was retired to training and instructional duties within the airline.
Specifications
Data from Flight:A Continental Feeder-Line Type.[1]
General characteristics
- Crew: Two pilots
- Capacity: 8 passengers / 1,000 kg (2,200 lb) payload
- Length: 11.0 m (36 ft 1 in)
- Wingspan: 15.2 m (49 ft 10 in)
- Height: 2.65 m (8 ft 8 in)
- Wing area: 31.15 m2 (335.3 sq ft)
- Empty weight: 1,150 kg (2,535 lb)
- Gross weight: 2,150 kg (4,740 lb)
- Powerplant: 2 × de Havilland Gipsy Major 4-cylinder inverted air-cooled in-line piston engines, 97 kW (130 hp) each
- Propellers: 2-bladed fixed pitch propellers
Performance
- Maximum speed: 206 km/h (128 mph, 111 kn)
- Cruise speed: 187 km/h (116 mph, 101 kn)
- Landing speed: 95 km/h (59 mph; 51 kn)
- Range: 850 km (530 mi, 460 nmi)
- Service ceiling: 4,200 m (13,800 ft) theoretical
- Service ceiling: 3,400 m (11,200 ft)
- Rate of climb: 3 m/s (590 ft/min)
References
- ^ a b "A Continental Feeder-Line Type". Flight. XXVII (1360): 77–78. 17 January 1935. Retrieved 20 October 2018.
Further reading
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 561.
- "Another Feeder-Line Machine". Flight: 608. 21 June 1934. Retrieved 2008-09-12.
External links
