ShinMaywa US-2
Explore the ShinMaywa US-2 in side view and top view to compare its silhouette and proportions.
From Wikipedia
The ShinMaywa US-2 is a large Japanese short takeoff and landing turboprop amphibious aircraft that employs boundary layer control technology for enhanced STOL and stall suppression performance. Manufactured by seaplane specialist ShinMaywa, it was developed from the earlier Shin Meiwa US-1A seaplane, which was introduced in the 1970s.
Summary of “ShinMaywa US-2” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.
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Drawing of the ShinMaywa US-2 by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/US2/), CC BY 4.0Specifications
- Length
- 33.46 m109.8 ft
- Wingspan
- 33.15 m108.8 ft
- Max take-off weight
- 47.7 t105,200 lb
- Cruise speed
- 480 km/h298 mph
- Max speed
- 560 km/h348 mph
- Range
- 4,700 km2,920 mi
- Ceiling
- 7,195 m23,600 ft
- Engines
- 4 × Rolls-Royce AE 2100 J turboprop
- Power
- 3,424 kW (4,592 hp) each
- First flight
- 2003
- In service
- 2007
From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.