Reggiane_Re.2003 Knowpia

Maximum speed: 510 km/h (320 mph, 280 kn)
Range: 720 km (450 mi, 390 nmi)
Service ceiling: 9,800 m (32,200 ft)

Re.2003
Role	Reconnaissance
National origin	Italy
Manufacturer	Reggiane
First flight	29 June 1941
Status	Retired
Primary user	Regia Aeronautica
Number built	1
Variants	Reggiane Re.2002

The Reggiane Re.2003 was a development from the Reggiane Re.2002 fighter bomber that first flew on 29 June 1941. It was designed to replace the outdated IMAM Ro.37 used at the time. Unlike the Re.2002, it had room for a second crewman who sat behind the pilot. It was equipped with onboard camera equipment. The Fiat A.74 RC.38 engine was intended to be used originally, but the Piaggio P. XI RC 40 bis was chosen instead. Only one was ever produced, and production for a second started, but never finished. The Regia Aeronautica (Italian Air Force) made an order of 200, but cancelled the order as Allied bombing raids made the Air Force's focus switch to fighter aircraft.

Specifications edit

Data from ^{[citation needed]}

General characteristics

Crew: 2
Length: 8.08 m (26 ft 6 in)
Wingspan: 11 m (36 ft 1 in)
Height: 3.2 m (10 ft 6 in)
Wing area: 20.4 m² (220 sq ft)
Airfoil: N-38^[1]
Empty weight: 5,445 kg (12,004 lb)
Gross weight: 7,319 kg (16,136 lb)
Powerplant: 1 × Piaggio P.XI R.C.40 bis 14-cylinder air-cooled radial piston engine, 876 kW (1,175 hp)
Propellers: 3-bladed constant-speed propeller