Arwico Collectors Edition – Pilatus PC-6 Turbo-Porter , ‚V-632‘ SWISS AIR FORCE
2,399 Kč
Skladem
Výrobce: Arwico Collectors EditionMěřítko: 1:72Letecká společnost: Swiss Air ForcePopis
-sběratelský model letadla Pilatus PC-6 Porter 1/72 -provedení: kovový model s plastovými částmi -model je v kvalitním provedení -součástí balení je stojánek
Pilatus PC-6 Porter
The Pilatus PC-6 Porter is a single-engined STOL utility aircraft designed by Pilatus Aircraft of Switzerland. First flown in 1959, the PC-6 continues in production at Pilatus Flugzeugwerke in Stans, Switzerland. It has been built in both piston engine – and turboprop-powered versions and was produced under licence for a time by Fairchild Hiller in the United States. After around 600 deliveries in six decades, Pilatus will produce the last one in early 2019.
Role | STOL passenger and utility aircraft |
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Manufacturer | Pilatus Aircraft Fairchild Aircraft |
First flight | Porter – 4 May 1959 Turbo-Porter – 2 May 1961. |
Status | In service |
Primary users | Civil aviation Austrian Air Force, Myanmar Air Force, Swiss Air Force |
Produced | 1959–2019 |
Number built | 595 (As of August 2017) |
Unit cost |
$55,000 (1962)
$1,900,000 (2010) |
Variants | Fairchild AU-23 Peacemaker |
General characteristics
- Crew: one, pilot
- Capacity: up to ten passengers
- Payload: 1,130 kg (2,491 lb)
- Length: 11.00 m (36 ft 1 in)
- Wingspan: 15.87 m (52 ft 0¾ in)
- Height: 3.20 m (10 ft 6 in)
- Wing area: 30.15 m² (324.5 sq ft)
- Airfoil: NACA 64-514
- Aspect ratio: 8.4:1
- Empty weight: 1,270 kg (2,800 lb)
- Max. takeoff weight: 2,800 kg (6,173 lb)
- Powerplant: 1 × Pratt & Whitney Canada PT6A-27 turboprop, 410 kW (550 shp)(downrated from 507 kW (680 shp))
Performance
- Never exceed speed: 280 km/h (151 knots, 174 mph)
- Maximum speed: 232 km/h (125 knots, 144 mph)
- Cruise speed: 213 km/h (115 knots, 132 mph) at 3,050 m (10,000 ft)
- Stall speed: 96 km/h (52 knots, 60 mph) (flaps down, power off)
- Range: 730 km (394 nmi, 453 mi) with maximum payload
- Ferry range: 1,612 km (870 nmi, 1,002 mi) with maximum internal and underwing fuel
- Service ceiling: 8,197 m (25,000 ft)
- Rate of climb: 4.8 m/s (941 ft/min)
Další informace
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