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North American Rockwell OV-10 Bronco
Specifications

Type: Light attack and observation aircraft
Crew: 2
Manufacturer: North American Rockwell
Models: see variants
Number built: N/A
   Maiden flight: July 16, 1965
Service Delivery: Oct. 1969
Primary Users: U.S. Marine Corps, U.S. Air Force, U.S. Navy, Philippine Air Force, Royal Thai Air Force.
Specifications:
Powerplant:
 Model:
  Garrett-AiResearch T76-G-412 &-413
 Type: Turboprop
 Number: Two
 Horsepower: 715 shaft horsepower each
Dimensions:
 Length: 41 ft, 7 in (12.67 m)
 Wingspan: 40 ft (12.19 m)
 Height: 15 ft, 2 in (4.62 m)
 Wing area: 290.95 ft² (27.03 m²)
 Tailplane Span: 14 ft, 7 in (4.45 m)

Weights:
 Empty: 6,969 lb (3,161 kg)
 Loaded: 9,908 lb (4,494 kg)
 Max takeoff: 14,466 lb (6,563 kg)

   Performance:
 Max. Speed: at sea level, no weapons
– Typical: 281 mph (452 kph)
– OV-10D+: 276 mph (444 kph)
 Max. Speed: at 10,000 ft
– OV-10B: 278 mph (447 kph)
– OV-10D: 393 mph (632 kph)
 Range: Max. Weapons
– 228 mi (367 km)
 Ferry Range:
– 1,428 mi (2,298 km) w. Aux. fuel
 Service ceiling: N/A
 Rate of climb: N/A
 Takeoff Run:
– OV-10B: at normal weight: 740 ft (226 m)
– OV-10B: at 12,000 lb: 1,130 ft (344 m)
– OV-10D: at 12,000 lb: 550 ft (168 m)
– OV-10D+: at 13,284 lb: 1,110 ft (338 m)
 Landing Run:
– Typical: at normal wt: 740 ft (226m)
– Typical: at overload wt: 1,250 ft (381 m)
– OV-10D+: at landing wt: 800 ft (244 m)
Sources:
Wikipedia: OV-10 Bronco
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