PAH-1 BO 105
| Specifications | |
|---|---|
| Country of Origin | Germany |
| Builder | Eurocopter |
| Date of Introduction | 1972 |
| Role | Observation, antitank, utility |
| Similar Aircraft | OH-6 Cayuse, Defender 500MD, Alouette III, Mi-4 Hound |
| Blades |
Main rotor: 4 Tail rotor: 2 |
| Rotor diameter |
Main Rotor Diameter: 9.8 / 32 ft, 3 in Tail Rotor Diameter: 1.9 |
| Length |
Length (rotors turning): 11.9 m / 39 ft Length (fuselage): 8.8m |
| Height | 3.0 m |
| Width | 2.5 m |
| Cargo Compartment Dimensions |
Floor Length: 1.9 m Width: 1.4 m Height: 1.3 m |
| Weight |
Maximal with external load 2,600 kg/5,732 lb Maximum Gross: 2,500 kg / 5,512 lb Normal Takeoff: 2,000 kg Empty: 1,301 kg, 1,913 kg (PAH1) |
| Engine | 2x 420-shp Allison 250-C20B turboshaft |
| Fuel |
Internal: 570 liters Internal Aux Tank: 200 liters ea. (max 2x) |
| Maximum speed | 242 km/h - 131 kts |
| Cruising speed | 205 km/h |
| Range |
Normal Load: 555 km With Aux Fuel: 961 km |
| Ceiling |
Service: 3,050 m Hover (out of ground effect): 457 m Hover (in ground effect): 1,525 m |
| Vertical Climb Rate | 7.5 m/s |
| Armament |
Most Probable Armament:
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| Standard Payload |
Internal load: 690 kg External on sling only: 1,200 kg Transports 3 troops or 2 litters, or cargo. |
| Survivability/Countermeasures |
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| AVIONICS |
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| Crew | 1 or 2 (pilots) |
| Cost | |
| User Countries | At least 40 countries -- Bahrain, Brunei, Chile, Colombia, Germany, Indonesia, Iraq, Mexico, Netherlands, Nigeria, Philippines, USA |
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