OH-6A Cayuse
AH-6J Little Bird
Defender 500
Specifications
Variants in "( )" | |
---|---|
Country of Origin | USA |
Builder | McDONNELL DOUGLAS |
Role | ASW, scout, antitank, multimission |
Similar Aircraft | BO 105, Alouette II |
Blades |
Main rotor: 4 or 5 (see VARIANTS) Tail rotor: 2 or 4 (see VARIANTS) |
Rotor diameter | 26 ft, 4 in (8 m) |
Length |
Length (rotors turning): 9.4 m (500), 9.8 m (530) Length (fuselage): 7.6 m (500), 7.3 m (530) |
Height | 2.6 m (500), 3.4 m (530 over mast-mounted sight) |
Width | 1.9 m |
Rotor Diameter |
Main Rotor Diameter: 8.0 (500), 8.3 (530) Tail Rotor Diameter: 1.4 |
Cargo Compartment Dimensions |
Floor Length: 2.4 m Width: 1.3 m Height: 1.5 m |
Weight |
Maximum Gross: 1,361 kg (500), 1,610 kg (530) Normal Takeoff: 1,090 kg Empty: 896 kg |
Engine | one 317 shp Allison T63-A-5A or T63-A-700 turboshaft engine, derated to 252.5 shp |
Fuel |
Internal: 240 liters Internal Aux Tank: 80 liters |
Speed |
Maximum (level): 241 km/h (500), 282 km/h (530) Cruise: 221 km/h (500), 250 km/h (530) |
Range | Normal Load (est.): 485 km (500), km 430 (530) |
Ceiling |
Service: 4,635 m (500), 4,875 m (530) Hover (out of ground effect): 1,830 m (500), 3,660 m (530) Hover (in ground effect): 2,590 m (500), 4,360 m (530) |
Vertical Climb Rate | 8.4 m/s (500), 10.5 m/s (530) |
Standard Payload |
Internal load: INA External load: 550 kg Transports 2 or 3 troops or cargo internally, or 6 on external platforms in lieu of weapons. |
Armament |
Most Probable Armament |
Survivability |
|
AVIONICS |
|
Crew | 1 or 2 (pilots) |
Cost | |
User Countries | At least 22 countries --
Argentina, Bahrain, Bolivia, Colombia, Costa Rica, Denmark, Dominican Republic, El Salvador, Honduras, Indonesia, Iraq, Israel, Jordan, Kenya, North Korea, South Korea, Spain, Taiwan, USA
|
NEWSLETTER
|
Join the GlobalSecurity.org mailing list |
|
|