OV-1D Mohawk  
Initial Operational Capability (IOC): 1959
Total Production: 380
Also Known As: OV-1A, OV-1B, OV-1C, RV-1C, RV-1D and RV-1D Quick Look II
Origin: United States of America
Corporations: Northrop Grumman
Parent System: OV-1 Mohawk
Initial Operational Capability (IOC): 1959
Total Production: 380
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Description: Grumman OV-1 Mohawk was developed to serve the US Army and Marine Corps as an observation and electronic reconnaissance aircraft. It is powered by two turboprop engines and carries a crew of two-man. It was deployed for the last time during the Desert Shield/Desert Storm in 1990-91. RV-1C and RV-1D were outfitted for electronic surveillance missions. RV-1D Quick Look II was an Electronic Intelligence (ELINT) aircraft. All OV-1Ds operated by the United States were retired from service and replaced by RC-12 aircraft in the mid-1990s.

OV-1D Mohawk Specifications

Crew: 2
Number of Engines: 2
Height: 3.90 meter (12.8 foot)
Length: 12.5 meter (41 foot)
Wingspan: 12.8 meter (42 foot)
Ceiling: 9,150 meter (30,020 foot)
Max Range: 710 kilometer (383 nautical mile)
Max Power at TakeOff: 2,300 shp
Cruise Speed: 133 mps (479 kph)
Top Speed at High Altitude: 138 mps (497 kph)
Max Takeoff Weight: 6,985 kilogram (15,399 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)

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