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Bell 212
Photo: own work · Wikimedia Commons · CC BY 2.5
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Bell212

Utility / Transport Helicopters · United States · 1968
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Bell212

Bell 212
Bell 212 Photo: own work · Wikimedia Commons · CC BY 2.5
* Absolute score — assessed within category · no era adjustment
Payload / Capacity
45
Range
50
Versatility
70
Reliability
80
Speed
55
Survivability
40
Hot-and-High Performance
65
Maintainability
70
Technology
45
Cost-Effectiveness
75
Origin United States
ManufacturerBell Textron
CategoryUtility / Transport Helicopters
EraCold War
In service1968–1998
Operators16 countries
Quantity204
Data Quality87%
59
Utility / Transport Helicopters MASS Rating
42/61
Cold War
132/208
All-Time
Utility / Transport Helicopters · 10 axes scored
Payload / Capacity
45
Range
50
Versatility
70
Reliability
80
Speed
55
Survivability
40
Hot-and-High Performance
65
Maintainability
70
Technology
45
Cost-Effectiveness
75
ⓘ Regardless of era, the same scoring system applies to all units in the utility / transport helicopters category.
01 / Overview
Bell 212
Prime contractor
Production
1968–1998
Quantity
204
Operators
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
UTILITY / TRANSPORT HELICOPTERS · COLD WAR
42
PERFORMANCE/PRICE
80
UNIT COST (2025 USD)
—
59
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 Flight1968
  • Service Entry Year1968
  • Crew1
  • Passengers14
  • Primary RoleUtility transport helicopter
  • In ServiceYes
◈Powerplant8MOD.8
  • Engine TypePratt & Whitney Canada PT6T-3 or -3B
  • Number of Engines2
  • Engine Power (each)1,342 kW
  • Transmission Rating1,342 kW
  • Rotor ConfigurationTwo-bladed semi-rigid main rotor
  • Main Rotor Diameter14.63 m
  • Main Rotor Blades2
  • Anti-Torque TypeTail rotor
▣Performance10MOD.10
  • Top Speed220 km/h
  • Cruise Speed185.184 km/h
  • Never-Exceed Speed (VNE)259 km/h
  • Service Ceiling5,303.52 m
  • Hover Ceiling (IGE)3,353 m
  • Hover Ceiling (OGE)2,896 m
  • Range420 km
  • Ferry Range1,000 km
  • Rate of Climb8.1 m/s
  • Endurance180
◇Dimensions & Weights7MOD.7
  • Fuselage Length17.42 m
  • Height4.57 m
  • Rotor Disc Area168.1
  • Empty Weight2,961.554 kg
  • Max Takeoff Weight5,080 kg
  • Useful Load2,160 kg
  • Cabin Volume6.23
◆Armament & Mission4MOD.4
  • Hardpoints0
  • Weapons Payload2,268 kg
  • Sling Load Capacity2,268 kg
  • Rescue HoistYes
⬢Production1MOD.1
  • Variants1
▲Service History2MOD.2
  • Production Start1968
  • Production End1998
03 / History
SERVICE LIFESPANStill in Service
  1. 1968Production started
  2. 1971Entered service
  3. 1998Production ended
58
years in service
30
years in production
204
units produced
15
countries operating
ⓘ The producing country still actively operates it. 1 countries retired it.
04 / Operators
Operator Inventory1country · 6units
6active
📖 TERMS ON THIS PAGE3terms
Autopilot/AFCS (Automatic Flight Control System) is an avionics suite that automatically controls a helicopter’s attitude, navigation and flight path, providing stability augmentation and reducing pilot workload.
Combined forward-looking infrared (FLIR) and electro-optical (EO) sensor turret for target acquisition and tracking, typically mounted on aircraft or ground vehicles.
A mechanical device used to lift personnel or cargo via a cable, typically mounted on helicopters for rescue or recovery operations.
These terms are listed automatically because they appear on this page.full encyclopedia →
📚 Sources
📖 ENCYCLOPEDIA Browse the Utility / Transport Helicopters entry →