Pilatus P-4
The Pilatus P-4 was a Swiss five-seat cabin monoplane designed and built by Pilatus, but had little sales success.
| P-4 | |
|---|---|
![]()  | |
| Model of the Pilatus P-4 | |
| Role | Five-seat cabin monoplane | 
| National origin | Switzerland | 
| Manufacturer | Pilatus | 
| First flight | 1948 | 
| Retired | 1957 | 
| Number built | 1 | 
Design and development
    
The P-4 was not designed specifically as a passenger aircraft, but rather as a versatile working aircraft. The aim was to build a robust aircraft with good slow-flying handling, requiring only short takeoff and landing runs and little maintenance. The P-4 HB-AET took off for its maiden flight on 22 March 1948. Series production never went ahead due to capacity bottlenecks.
The P-4 was unveiled to a wide international public at the 18th Paris Air Show in 1949, and attracted much interest. There were plans to fit the P-4 with floats, or a combination wheel-ski landing gear.
The P-4 was also destined for agricultural work.
On 13 October 1957, the P-4 crashed in the Susten Pass region while on an exercise with the Swiss Air Rescue Service, and was completely written off. Pilatus Aircraft Ltd had always owned the P-4 until that time.
Comparing the P-4 to the PC-6, which was built eleven years later, the P-4 was clearly an intermediate stage on the way to the mature endproduct, the Pilatus Porter PC-6.
Specifications (P-4)
    
Data from Jane's All The World's Aircraft 1951–52[1]
General characteristics
- Crew: one
 - Capacity: four passengers
 - Length: 8.6 m (28 ft 3 in)
 - Wingspan: 11.85 m (38 ft 11 in)
 - Height: 2.5 m (8 ft 2 in)
 - Wing area: 20.9 m2 (225 sq ft)
 - Empty weight: 910 kg (2,006 lb)
 - Gross weight: 1,500 kg (3,307 lb)
 - Fuel capacity: 230 L (61 US gal; 51 imp gal)
 - Powerplant: 1 × Lycoming O-435 , 140 kW (190 hp)
 
Performance
- Maximum speed: 245 km/h (152 mph, 132 kn)
 - Cruise speed: 152 km/h (94 mph, 82 kn)
 - Range: 1,000 km (620 mi, 540 nmi)
 - Service ceiling: 5,000 m (16,000 ft)
 - Rate of climb: 4.5 m/s (890 ft/min)
 
References
    
Notes
- Bridgman 1951, p. 190c.
 
Sources
- Bridgman, Leonard (1951). Jane's All The World's Aircraft 1951–52. London: Sampson Low, Marston & Company, Ltd.
 - Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
 - The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
 
