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Shin Meiwa developed the Amphibious Air Transport System during the late 1980s/early 1990s and was looking for partners to complete development as late as 1999.
The aircraft was a 30/50-seat airliner powered by two wing-mounted turbofans with upper surface blowing. Range would be between 500nm with full payload to 1,200nm with full fuel. Take-off distance was estimated as 1,000m on water and 800m on soft ground. Cruising speed 345-414mph (556-667 km/h).
Source: Jane's Civil and Military Upgrades 1993-94
The aircraft was a 30/50-seat airliner powered by two wing-mounted turbofans with upper surface blowing. Range would be between 500nm with full payload to 1,200nm with full fuel. Take-off distance was estimated as 1,000m on water and 800m on soft ground. Cruising speed 345-414mph (556-667 km/h).
Source: Jane's Civil and Military Upgrades 1993-94