Time Period: Post-WW2
Country of Origin: United Kingdom
Type: Airliner
Manufacturer: Airspeed Ltd.
Airspeed AS.57 Ambassador Aircraft Overview
The Airspeed AS.57 Ambassador was a British twin-engine airliner produced by Airspeed Limited in the late 1940s and early 1950s. It was one of the last aircraft designs developed by Airspeed before the company was absorbed by de Havilland Aircraft Company in 1948.
The AS.57 Ambassador was designed to meet the post-World War II demand for a modern and efficient airliner that could operate on medium-haul routes. It was a high-wing monoplane with a pressurized cabin, making it one of the first British airliners to offer such a feature, providing a more comfortable flying experience for passengers.
The aircraft made its maiden flight on July 10, 1947. It was initially powered by four Bristol Centaurus radial engines, but this configuration was later changed to two Rolls-Royce Dart turboprop engines, which provided improved performance and fuel efficiency.
The Ambassador had a seating capacity of around 40 to 50 passengers, depending on the specific airline’s interior configuration. It offered a range of approximately 1,500 miles (2,400 kilometers), making it suitable for regional and medium-haul routes.
Despite its promising design and features, the Ambassador faced challenges in the market. It suffered from delays in development and experienced competition from other contemporary airliners like the Vickers Viscount and the Douglas DC-6. Additionally, some early technical issues with the Dart engines affected the aircraft’s reputation.
While the Ambassador didn’t achieve widespread commercial success as initially hoped, it found service with a few airlines, including British European Airways (BEA). BEA operated the Ambassador on various routes, primarily within Europe, during the early 1950s.
In total, only 23 Airspeed AS.57 Ambassadors were produced, including both the original Ambassador and the later improved version known as the Ambassador 2. Despite its limited production and commercial success, the Ambassador contributed to the advancement of aviation technology and helped pave the way for the use of turboprop engines in future aircraft designs.
Today, no flying examples of the Airspeed AS.57 Ambassador exist, but its historical significance as one of the early British turboprop airliners remains notable in the aviation industry’s timeline.
Airspeed AS.57 Ambassador Specifications
- Crew: 3
- Capacity: Up to 60 passengers
- Length: 81 ft (25 m)
- Wingspan: 115 ft (35 m)
- Height: 18 ft 4 in (5.59 m)
- Wing area: 1,200 sq ft (110 m2)
- Aspect ratio: 11:1
- Airfoil: root: NACA; tip: NACA
- Empty weight: 35,884 lb (16,277 kg)
- Max takeoff weight: 52,000 lb (23,587 kg)
- Fuel capacity: 1,000 imp gal (1,200 US gal; 4,500 L) in two integral wing tanks, with provision for 600 imp gal (720 US gal; 2,700 L) in two centre-section bag tanks
- Powerplant: 2 × Bristol Centaurus 661 18-cylinder air-cooled sleeve-valve piston engines, 2,625 hp (1,957 kW) each.
Airspeed AS.57 Ambassador Performance
- Maximum speed: 312 mph (502 km/h, 271 kn) at 75% power with 11,650 lb (5,280 kg) payload
- Cruise speed: 300 mph (480 km/h, 260 kn) at 20,000 ft (6,100 m) at 50,000 lb (23,000 kg). 279 mph (242 kn; 449 km/h) at 60% power.
- Range: 720 mi (1,160 km, 630 nmi) with 11,650 lb (5,280 kg) payload and no reserves at 280 mph (240 kn; 450 km/h). 900 mi (780 nmi; 1,400 km) at 220 mph (190 kn; 350 km/h). 1,560 mi (1,360 nmi; 2,510 km) with 7,900 lb (3,600 kg) payload max. fuel at 280 mph (240 kn; 450 km/h). 1,950 mi (1,690 nmi; 3,140 km) with 7,900 lb (3,600 kg) payload max. fuel at 220 mph (190 kn; 350 km/h)
- Rate of climb: 1,520 ft/min (7.7 m/s) at 5,000 ft (1,500 m) at maximum weight
- Rate of climb on one engine: 420 ft/min (130 m/min) after take-off at maximum weight. 360 ft/min (110 m/min) at 5,000 ft (1,500 m) at maximum weight.
- Wing loading: 43.3 lb/sq ft (211 kg/m2) at 52,000 lb (24,000 kg)
- Power/mass: 0.1 hp/lb (0.16 kW/kg) at 52,000 lb (24,000 kg)
- Take-off distance to 50 ft (15 m): 3,270 ft (1,000 m) at maximum T.O weight
- Take-off distance to 50 ft (15 m) one engine: 4,950 ft (1,510 m) at maximum T.O weight
- Landing distance from 50 ft (15 m): 2,565 ft (782 m) at max landing weight.