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Bell 430

American commercial helicopter, actively utilized globally for medical services and executive transportation since the late 20th century. Key figures: top speed 278 km/h, range 600 km, service ceiling 6,096 m, max takeoff weight 4,218 kg, unit price $10M, built 136. In service with 3 air forces as of 2026 β€” Ecuador (4), Dominican Republic (1), Paraguay (1).

Max speed
278km/h
Range
600km
Produced
136units
Avg unit price
$10 million
Active worldwide
6
Bell 430 military helicopters side profile drawing
Side profile Β· Bell 430 Β· length 15.3 m
Technical SpecificationsVersion: Bell 430
Crew1
Length15.3 m (50.2 ft)
Wingspan12.8 m (42.0 ft)
Height3.8 m (12.3 ft)
Empty weight2,406 kg (5,304 lbs)
Max. takeoff weight4,218 kg (9,299 lbs)
Powerplant2 Γ— turboshafts Allison 250-C40B 585 kW each
PerformanceVersion: Bell 430
Maximum speed278 km/h (173 mph)
Operational range600 km (373 mi)
Service ceiling6,096 m (20,000 ft)
Climb rate6.858 m/s (22.5 ft/s)
Operators β€” 2026
ActiveOn order
All Operators
πŸ‡©πŸ‡΄ Dominican RepublicΒ· πŸ‡ͺπŸ‡¨ EcuadorΒ· πŸ‡΅πŸ‡Ύ ParaguayΒ· πŸ‡ΊπŸ‡Έ United States

Description

The Bell 430 is an American-Canadian light-medium twin-engine helicopter built by Bell Helicopter. A stretched and re-engined derivative of the Bell 230, itself developed from the Bell 222, it entered service in 1996 in passenger transport, executive transport and medical evacuation roles. It is distinguished by its hingeless, bearingless four-blade main rotor and by the round-the-world helicopter record set in 1996.

Development

While developing the re-engined Model 222 into the 230, Bell began preliminary studies in 1991 of a stretched version fitted with a four-blade main rotor. The Bell 430 was officially launched in February 1992, with two prototypes converted from Bell 230 airframes. The first flew in its new configuration on 25 October 1994, the second, fitted with the full 430 avionics suite, on 19 December 1994. Bell 230 production ended in August 1995 and 430 production began; the first production aircraft was completed the same year. Canadian certification was obtained on 23 February 1996 and deliveries began in the middle of that year. On 24 January 2008, Bell announced the end of production once the outstanding orders were fulfilled. Production ended after 136 aircraft, the last being delivered in May 2008.

Design

The main change from the 230 is the composite hingeless, bearingless four-blade main rotor. Both the 230 and the 430 use Rolls-Royce (Allison) 250 turboshaft engines, those of the 430 delivering 10% more power. The fuselage is lengthened by 46 cm, allowing two seats to be added. An EFIS cockpit is offered as an option, as is the choice between skids and retractable wheeled landing gear. The standard configuration seats ten occupants: a pilot, a co-pilot and eight passengers in three rows in the main cabin. Six- and eight-seat executive interiors are also offered. In the medical configuration, the aircraft carries one or two stretchers accompanied by four or three medical attendants respectively. The maximum external load is 1,600 kg (3,500 lb).

Operational History

The Bell 430 entered service in 1996, with thirteen aircraft delivered that year. By 1998, some fifty examples were in service, totalling 9,000 flight hours. On 3 September 1996, Americans Ron Bower and John Williams broke the round-the-world helicopter record aboard the second Bell 430, departing the United Kingdom westbound, in 17 days, 6 hours and 14 minutes. Military users include the Bulgarian Air Force, the Dominican Air Force and the Ecuadorian Navy. Civil operators include Pelita Air in Indonesia, as well as AirMed, the New York State Police, Lee County EMS, GrandView Aviation, the Louisiana State Police and Uber Elevate in the United States. On 2 September 2009, a Bell 430 of the Andhra Pradesh government carrying Chief Minister Y. S. Rajasekhara Reddy crashed on a hill in the Nallamala Hills, killing all five occupants.

Wikipedia (CC BY-SA) and other open sources. Illustrations generated by AI. Last updated on 30 August 2026. Suggest a change

Frequently Asked Questions

What type of aircraft is the Bell 430?
The Bell 430 is a military helicopters aircraft developed by Bell and entered service in 1995.
What is the maximum speed of the Bell 430?
The Bell 430 has a maximum speed of 278 km/h (172 mph).
What is the range of the Bell 430?
The Bell 430 has an operational range of 600 km (372 miles). This range can vary based on payload, altitude, and mission profile.
When did the Bell 430 first fly?
The Bell 430 made its first flight on October 25, 1994. It entered operational service in 1995.
How many Bell 430 have been built?
Approximately 136 units of the Bell 430 have been produced since it entered service in 1995.
Which countries operate the Bell 430?
The Bell 430 is operated by 3 countries with approximately 6 aircraft in active service. The largest operators include Ecuador, Dominican Republic, and Paraguay.
How much does a Bell 430 cost?
The Bell 430 has an estimated unit cost of approximately $10.0 million. Actual prices vary based on configuration, quantity ordered, and included support packages.
What is the service ceiling of the Bell 430?
The Bell 430 has a service ceiling of 6,096 meters (20,000 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
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Latest Data Updates
  1. AUG 302026 Updated Description updated
  2. AUG 52026 Updated Powerplant updated in a site-wide editorial pass
  3. APR 72026 Updated Picture credits updated in a site-wide editorial pass
  4. FEB 72026 Updated Wingspan added
  5. JAN 122026 Updated Range updated in a site-wide editorial pass