Data from Flight, February 1923, French aircraft of the First World War
General characteristics
Crew: 3 (4)
Length: 19.98 m (65 ft 7 in)
Wingspan: 30 m (98 ft 5 in)
Height: 6.1 m (20 ft 0 in)
Wing area: 220 m² (2,400 sq ft)
Empty weight: 6,500 kg (14,330 lb) without fuel
Gross weight: 10,020 kg (22,090 lb) with 1,700 kg (3,700 lb) fuel
Powerplant: 4 × Lorraine-Dietrich 12Da water-cooled V-12, 280 kW (370 hp)  each
Propellers: 2-bladed tractor and pusher propellers.,
2.90 m (9 ft 6 in) diameter Lumière-Leitner-Watts ground-adjustable propellers also fitted during testing.

Performance
Maximum speed: 160 km/h (99 mph, 86 kn) at ground level
Range: 750 km (470 mi, 400 nmi)
Service ceiling: 5,000 m (16,000 ft) absolute
Time to altitude: 13 min to 2,000 m (6,600 ft)
Take-off distance: 300 m (980 ft)
Landing distance: 200 m (660 ft)
Landing speed: 80 km/h (50 mph; 43 kn)
Armament
2x 37 mm (1.46 in) and 1x 75 mm (2.95 in) cannon (proposed but not fitted)
Data from Flight, February 1923, French aircraft of the First World War
General characteristics
Crew: 3 (4)
Length: 19.98 m (65 ft 7 in)
Wingspan: 30 m (98 ft 5 in)
Height: 6.1 m (20 ft 0 in)
Wing area: 220 m² (2,400 sq ft)
Empty weight: 6,500 kg (14,330 lb) without fuel
Gross weight: 10,020 kg (22,090 lb) with 1,700 kg (3,700 lb) fuel
Powerplant: 4 × Lorraine-Dietrich 12Da water-cooled V-12, 280 kW (370 hp)  each
Propellers: 2-bladed tractor and pusher propellers., 2.90 m (9 ft 6 in) diameter Lumière-Leitner-Watts ground-adjustable propellers also fitted during testing.
Performance
Maximum speed: 160 km/h (99 mph, 86 kn) at ground level
Range: 750 km (470 mi, 400 nmi)
Service ceiling: 5,000 m (16,000 ft) absolute
Time to altitude: 13 min to 2,000 m (6,600 ft)
Take-off distance: 300 m (980 ft)
Landing distance: 200 m (660 ft)
Landing speed: 80 km/h (50 mph; 43 kn)
Armament
2x 37 mm (1.46 in) and 1x 75 mm (2.95 in) cannon (proposed but not fitted)
Schneider Henri-Paul