From old site on Net,about Arsenal-Delanne 10C2,
Tactical and technical data (approximate):
Design: single-engine, two-seat tandem biplane (the front wing is a strut-shaped high-wing configuration, the rear wing is a cantilever low-wing configuration) with an enclosed cockpit and retractable tricycle landing gear with a tailwheel. All-metal construction. Twin vertical stabilizers at the tips of the rear wing.
Dimensions
span 10.10-10.50 m (according to [4] 10.11 m)
length 7.30-7.35 m (according to [4] 7.33 m)
height 3.00 m (according to [4] 3.06 m)
supporting surface 22.35-22.50 m 2
Masses
take-off weight 2850 kg (according to [4] 2880 kg)
Loads
load on the supporting surface approx. 127.52 kg/ m2
power load 4.51 kg/kW (3.31 kg/hp)
Performance
maximum speed 550 km/h at an altitude of 4,500 m
climb time to 5000 m - 6 minutes 30 seconds
ceiling 10,000 m
flight duration 1 hour 30 minutes
Propulsion: one 12-cylinder, liquid-cooled, V-shaped Hispano-Suiza HS-12Ycrs engine, 632 kW (860 hp), driving a 3-blade Ratier metal adjustable propeller
Armament (planned for the serial version): one fixed 20 mm Hispano-Suiza HS-404 cannon in the front of the fuselage (firing through the propeller axis), two fixed 7.5 mm MAC M-39 wz.34 machine guns in the front wing and one double-barreled movable 7.5 mm MAC M-39 wz.34 machine gun in the firing position at the end of the fuselage
Crew: 2 people (pilot + gunner)
Manufacturer: Arsenal de l'Aéronautique, Villacoublay, France
Production: 1 prototype
Users: France, Germany