Bell · United States · 2005–2008 ·
$9.6 million

The Bell ARH-70 was being developed in the early 2000’s as the successor of the OH-58D Kiowa Warrior. Four prototypes were built, and the model had its first flight in July 2006. In October 2008 the project was canceled.

Live fleet data is currently unavailable for this aircraft.

Engine:
2× Honeywell HTS900-2 turboshaft
Engine type:
Turboshaft
Power:
2 × 970 shp  ·  723 kW
Wing Tips:
No winglets
Seats:
6
Exterior length:
34 ft 8 in · 10.57 m
Wing span / rotor:
35 ft 0 in · 10.67 m
Max takeoff weight:
5,000 lb  ·  2,250 kg
Max Payload:
1,850 lb  ·  850 kg
Fuel capacity:
70 gal  ·  300 L  ·  200 kg  (Jet A)
Max cruise speed:
140 kt  ·  161 mph  ·  259 km/h
Range:
162 nm  ·  190 mi  ·  300 km
Fuel burn:
2.31 nm/gal  ·  1.13 km/L
Ceiling:
20,000 ft  ·  6,100 m
Rate of climb:
2,000 ft/min  ·  10 m/s
Live Fleet Activity Details (N/A)
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One of the prototypes made an autorotational emergency landing after which the aircraft was damaged beyond repair. After this incident the Army issued a Stop Work Notice. With the new 2008 defense budget there was no budget to develop this project any further and it got canceled as a consequence of the global financial crisis.

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