For comparrison:
General characteristics A-20
Crew: 2-3
Length: 47 ft 6 in (14.5 m)
Wingspan: 61 ft 4 in (18.7 m)
Height: 17 ft 7 in (5.4 m)
Wing area: 465 ft² (43.2 m²)
Empty weight: 15,051 lb (6,827 kg)
Max takeoff weight: 20,320 lb (9,215 kg)
Powerplant: 2× Wright R-2600-A5B "Double Cyclone" radial engines, 1,600 hp (1,200 kW) each
Performance
Maximum speed: 338 mph (294 knots, 544 km/h) at 12,500 ft (3,800 m)
Range: 1,050 mi (912 nm, 1,690 km)
Service ceiling: 27,600 ft (8,400 m)
Rate of climb: 2,000 ft/min (10.2 m/s)
General characteristics - de Havilland Mosquito
Crew: 2: pilot, bombardier/navigator
Length: 44 ft 6 in (13.57 m)
Wingspan: 54 ft 2 in (16.52 m)
Height: 17 ft 5 in (5.3 m)
Wing area: 454 ft² (42.18 m²)
Empty weight: 14,300 lb (6,490 kg)
Loaded weight: 18,100 lb (8,210 kg)
Max takeoff weight: 25,000 lb (11,000 kg)
Powerplant: 2× Rolls-Royce Merlin 76/77 (left/right) liquid-cooled V12 engine, 1,710 hp (1,280 kW) each
Performance
Maximum speed: 361 knots (415 mph, 668 km/h) at 28,000 ft (8,500 m)
Range: 1,300 nm (1,500 mi, 2,400 km) with full weapons load
Service ceiling: 37,000 ft (11,000 m)
Rate of climb: 2,850 ft/min (14.5 m/s)
Wing loading: 39.9 lb/ft² (195 kg/m²)
Power/mass: 0.189 hp/lb (311 W/kg)
The Mosquito and the A-20 are largely comparable. True Statement?