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ShinMaywa US-2

The ShinMaywa US-2 is a Japanese large STOL amphibious aircraft designed for air-sea rescue (SAR) work. Operated by the Japan Maritime Self-Defense Force, the US-2 is scheduled to replace the older Shin Meiwa US-1A in Japanese service.

Specifications (US-2)

General characteristics
  • Crew: 11
  • Capacity: 20 passengers or 12 stretchers
  • Length: 33.46 m (109 ft 9 in)
  • Wingspan: 33.15 m (108 ft 9 in)
  • Height: 9.8 m (32 ft 2 in)
  • Wing area: 135.8 m2 (1,462 sq ft)
  • Empty weight: 25,630 kg (56,504 lb)
  • Gross weight: 43,000 kg (94,799 lb) water take-off
  • Max takeoff weight: 47,700 kg (105,160 lb) land take-off
  • Powerplant: 4 × Rolls-Royce AE 2100J turboprop, 3,424 kW (4,592 hp) each
  • Powerplant: 1 × LHTEC T800 turboshaft Boundary layer control compressor, 1,017 kW (1,364 hp)
  • Propellers: 6-bladed Dowty R414
Performance
  • Maximum speed: 560 km/h (348 mph; 302 kn)
  • Cruise speed: 480 km/h (298 mph; 259 kn) at 6,000 m (20,000 ft)
  • Range: 4,700 km (2,920 mi; 2,538 nmi)
  • Service ceiling: 7,195 m (23,606 ft)
  • Takeoff distance on ground at MTOW: 490 m (1,610 ft)
  • Landing distance on ground at MTOW: 1,500 m (4,900 ft)
  • Takeoff distance on water at Loaded weight: 280 m (920 ft)
  • Landing distance on water at Loaded weight: 330 m (1,080 ft)

Beriev Be-200

The Beriev Be-200 Altair (Russian: Бериев Бе-200) is a multipurpose amphibious aircraft designed by the Beriev Aircraft Company and manufactured by Irkut. Marketed as being designed for fire fighting, search and rescue, maritime patrol, cargo, and passenger transportation, it has a capacity of 12 tonnes (12,000 litres, 3,170 US gallons) of water, or up to 72 passengers.
The name Altair was chosen after a competition amongst Beriev and Irkut staff in 2002/2003. The name Altair was chosen as it is not only the name of the alpha star in the Eagle constellation, but also because "Al" is the first part of the name of the Beriev A-40 Albatross amphibious aircraft, whose layout was the development basis for the creation of the Be-200, "ta" stands for Taganrog, and "ir" stands for Irkutsk.

Variants
Be-200: Basic multirole model
Be-200ChS (as it is more often known, a transcription of the Russian Бе-200ЧС) or Be-200ES (Emergency Situations): Multirole model fitted to the requirements of the Russian Ministry of Emergency Situations
Be-200E: English cockpit version of the Be-200ES[36]
Be-200RR: Designation of projected Rolls-Royce engined variant, since shelved.
Be-210: Projected passenger-only model
Be-220: Projected maritime patrol variant

Specifications (Be-200)

General characteristics
  • Crew: 2
  • Length: 32.0 m (105 ft 0 in)
  • Wingspan: 32.8 m (107 ft 7 in)
  • Height: 8.9 m (29 ft 2 in)
  • Wing area: 117.4 m² (1,264 ft²)
  • Empty weight: 27,600 kg (60,850 lb)
  • Max Take Off Weight (Land): 41,000 kg (90,390 lb)
  • Max Take Off Weight (Water): 37,900 kg (83,550 lb)
  • Max Capacity (Water or Retardant): 12,000 kg (26,450 lb)
  • Max Capacity (Cargo): 7,500 kg (16,530 lb)
  • Max Capacity (Passengers): 44 (Be-200ES) 72 (Be-210)
  • Powerplant: 2 × Progress D-436TP turbofans, 7,500 kgf (16,534 lbf) each
Performance
  • Maximum speed: 700 km/h (435 mph)
  • Cruise speed: 560 km/h (348 mph)
  • Economy speed: 550 km/h (342 mph)
  • Landing speed: 200 km/h (124 mph)
  • Takeoff speed: 220 km/h (137 mph)
  • Minimum speed (Flaps 38°): 157 km/h (98 mph)
  • Range: 2,100 km (1,305 mi)
  • Ferry range (One Hour Reserve): 3,300 km (2,051 mi)
  • Service ceiling: 8,000 m (26,246 ft)
  • Rate of climb: 13 m/s (2,600 ft/min) (At Sea Level and MTOW—Flaps 20°)
  • Rate of climb: 17 m/s (3,350 ft/min) (At Sea Level and MTOW—Flaps 0°)

AVIC AG600

The AVIC AG600, code named Kunlong (鲲龙), also known as TA-600, is the largest amphibious aircraft currently flying. It is designed by the Aviation Industry Corporation of China (AVIC). The aircraft made its first flight in Zhuhai, Guangdong on 24 December 2017. The AG600 is one of China's three state-approved "big plane projects".

Specifications (AG600)

General characteristics
  • Capacity: 50 passengers
  • Length: 36.9 m (121 ft 1 in)
  • Wingspan: 38.8 m (127 ft 4 in)
  • Height: 12.1 m (39 ft 8 in)
  • Max takeoff weight: 53,500 kg (117,947 lb)
  • Powerplant: 4 × WJ-6 turboprops, 3,805 kW (5,103 hp) each
  • Propellers: 6-bladed constant speed propellers
Performance
  • Maximum speed: 570 km/h (354 mph; 308 kn)
  • Range: 5,500 km (3,418 mi; 2,970 nmi)
  • Service ceiling: 10,500 m (34,400 ft)
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