OV-10E Bronco

There are 3 images added on 22 June 2009

OV-10E Bronco

Initial Operational Capability (IOC): 1966
Total Production: ?
Also Known As: OV-10A, OV-10B, OV-10C and OV-10D
Origin: United States of America

Parent System: OV-10 Bronco
Initial Operational Capability (IOC): 1966
Total Production: ?

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Description: Rockwell OV-10 Bronco is a light twin-engine turboprop aircraft developed for the United States Marine Corps in the 1960s. It accommodates a crew of two-man in a tandem cockpit and up to five passengers in the rear fuselage. It is equipped with four 7.62mm machine guns. This aircraft was procured by the United States Air Force (USAF), Navy and Marine Corps. Along its career OV-10s served as light attack and Forward Air Control (FAC) aircraft. It was deployed in Vietnam and during the Gulf War. The United States OV-10s were withdrawn from service in the 1990s. Currently, OV-10s are only in service with international customers.

OV-10E Bronco Specifications

Crew: 2
Number of Engines: 2
Passengers: 5
Dimensions
Height: 4.62 meter (15.2 foot)
Length: 12.7 meter (42 foot)
Main Gun Caliber: 7.62 millimeter
Wingspan: 12.2 meter (40.0 foot)
Performance
Ceiling: 7,315 meter (23,999 foot)
Max Range: 2,300 kilometer (1,242 nautical mile)
Power
Max Power at TakeOff: 1,430 shp
Speed
Top Speed at High Altitude: 126 mps (454 kph)
Weight
Empty Weight: 3,160 kilogram (6,966 pound)
Max Takeoff Weight: 6,552 kilogram (14,444 pound)

CEP: Circular Error Probable
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
Shaft-Horse-Power (shp)