The durability, safety, flying ease and proven heritage of the AT-401B makes it the choice of operators looking for an affordable upgrade to a high capacity, low maintenance piston engine ag plane. Here is an aircraft with an ...
Engine: P&W R1340
Horses: 600 SHP @ 2250 RPM
Helix: 12D40 hub 6101A-12 blades
Maximum takeoff weight: 3.565 kg (7,860 lbs)
Maximum landing weight: 2.722 kg (6,000 lbs)
Empty weight with firefighting equipment: 1.925 kg (4,244 lbs)
Payload: 1.640 kg (3,616 lbs)
Tank Capacity: 1.514 L (400 U.S. gal)
Fuel Capacity: 476 L (126 U.S. gal)
Scale: 15,54 m (51 ft)
Wing surface: 28,45 m2 (306 sq. ft)
Main Wheel Size: 8.50 x 10
Size tailwheel: 5.00 x 5
Cruising speed: 230 km/h (143 mph) at 1.219 m (4,000 ft)
Stall speed with flaps up: 117 km/h (73 mph) at 2.722 kg (6,000 lbs)
Stall speed with flaps down: 98 km/h (61 mph) at 2.722 kg (6,000 lbs)
Landing speed: 87 km/h (54 mph)
Rate of Climb: 158 mpm (520 fpm) at 3.565 kg (7,860 lbs)
Takeoff speed: 402 m (1,318 ft) at 3.565 kg (7,860 lbs)
Reach economical speed (8000 feet): 1.014 km (630 mi)