Bell ARH-70

$9.6 million estimated if ever sold

Overview

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.

Specifications

Units
Engine
2 × Honeywell HTS900-2 turboshaft
Engine type
Turboshaft
Power
2 × 970 shp · 723 kW
Avionics
Wing tips
No winglets
Seats
6
Crew
Cabin width
Cabin height
Cabin length
Exterior length
34 ft 8 in  ·  10.57 m
Tail height
Fuselage diameter
Wing span
35 ft 0 in  ·  10.67 m
Baggage volume
Gross weight
Empty weight
Max takeoff weight
5,000 lb  ·  2,250 kg
Max landing weight
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
Maximum speed
Cruise speed
Approach speed
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
Takeoff distance
Landing distance
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A Bell 407 being used for early development of the ARH-70

Operational Context

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.