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Bell 430
Photo: J o · Wikimedia Commons · CC BY-SA 3.0
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Bell430

Utility / Transport Helicopters · United States · 1996
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Bell430

Bell 430
Bell 430 Photo: J o · Wikimedia Commons · CC BY-SA 3.0
* Absolute score — assessed within category · no era adjustment
Payload / Capacity
65
Range
60
Versatility
75
Reliability
70
Speed
65
Survivability
55
Hot-and-High Performance
60
Maintainability
70
Technology
75
Cost-Effectiveness
65
Origin United States
ManufacturerBell Textron
CategoryUtility / Transport Helicopters
EraPost-Cold War
In service1996–2008
Operators5 countries
Quantity136
Data Quality86%
66
Utility / Transport Helicopters MASS Rating
23/28
Post-Cold War
98/208
All-Time
Utility / Transport Helicopters · 10 axes scored
Payload / Capacity
65
Range
60
Versatility
75
Reliability
70
Speed
65
Survivability
55
Hot-and-High Performance
60
Maintainability
70
Technology
75
Cost-Effectiveness
65
ⓘ Regardless of era, the same scoring system applies to all units in the utility / transport helicopters category.
01 / Overview
Bell 430
Prime contractor
Production
1996–2008
Quantity
136
Operators
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
UTILITY / TRANSPORT HELICOPTERS · POST-COLD WAR
23
PERFORMANCE/PRICE
60
UNIT COST (2025 USD)
—
66
utility / transport helicopters category
ⓘ Performance/Price and MASS score are computed across all units in the utility / transport helicopters category, regardless of era.
02 / Specs & Design
◎General6MOD.6
  • First Flight1994
  • Service Entry Year1996
  • Crew2
  • Passengers8
  • Primary RoleLight-medium utility helicopter
  • In ServiceYes
◈Powerplant7MOD.7
  • Engine TypeRolls-Royce 250-C40B
  • Number of Engines2
  • Engine Power (each)583 kW
  • Rotor Configurationfour-bladed, bearingless, hingeless, composite main rotor
  • Main Rotor Diameter12.8 m
  • Main Rotor Blades4
  • Anti-Torque Typetail rotor
▣Performance5MOD.5
  • Top Speed259 km/h
  • Service Ceiling4,450 m
  • Hover Ceiling (IGE)3,460 m
  • Range600 km
  • Rate of Climb6.86 m/s
◇Dimensions & Weights4MOD.4
  • Fuselage Length13.44 m
  • Height3.73 m
  • Empty Weight2,406 kg
  • Max Takeoff Weight4,218 kg
◆Armament & Mission6MOD.6
▲Production2MOD.2
  • Total Built136
  • Variants0
◎Service History3MOD.3
  • Production Start1996
  • Production End2008
  • Operational Statusin service
03 / History
SERVICE LIFESPANStill in Service
  1. 1996Production started
  2. 2008Production ended
30
years in service
12
years in production
136
units produced
3
countries operating
ⓘ The producing country still actively operates it. 2 countries retired it.
04 / Operators
📖 TERMS ON THIS PAGE1terms
A glass cockpit is an aircraft cockpit featuring electronic instrument displays, typically LCD or CRT screens, replacing traditional analog gauges.
These terms are listed automatically because they appear on this page.full encyclopedia →
📚 Sources
📖 ENCYCLOPEDIA Browse the Utility / Transport Helicopters entry →