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SikorskyH-34

Utility / Transport Helicopters · United States · 1954
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SikorskyH-34

Sikorsky H-34
Sikorsky H-34 Photo: Wikimedia Commons · CC BY-SA 3.0
* Absolute score — assessed within category · no era adjustment
Payload / Capacity
60
Range
55
Versatility
70
Reliability
80
Speed
50
Survivability
45
Hot-and-High Performance
50
Maintainability
75
Technology
30
Cost-Effectiveness
85
Origin United States
ManufacturerSikorsky Aircraft Corporation
CategoryUtility / Transport Helicopters
EraEarly Cold War
In service1954–1970
Operators22 countries
Quantity2,340
Data Quality88%
61
Utility / Transport Helicopters MASS Rating
13/42
Early Cold War
123/208
All-Time
Utility / Transport Helicopters · 10 axes scored
Payload / Capacity
60
Range
55
Versatility
70
Reliability
80
Speed
50
Survivability
45
Hot-and-High Performance
50
Maintainability
75
Technology
30
Cost-Effectiveness
85
ⓘ Regardless of era, the same scoring system applies to all units in the utility / transport helicopters category.
01 / Overview
Sikorsky H-34
Production
1954–1970
Quantity
2,340
Operators
Conflicts
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
UTILITY / TRANSPORT HELICOPTERS · EARLY COLD WAR
13
PERFORMANCE/PRICE
90
UNIT COST (2025 USD)
—
61
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 Flight1954
  • Service Entry Year1954
  • Crew2
  • Passengers12
  • Primary Roleutility transport, anti-submarine warfare, search and rescue, VIP transport
  • In ServiceYes
◈Powerplant8MOD.8
  • Engine TypePratt & Whitney R-1820-84 radial piston engine (early models); Wright Cyclone R-1820-84 (later models)
  • Number of Engines1
  • Engine Power (each)1,193 kW
  • Transmission Rating1,193 kW
  • Rotor Configurationsingle main rotor, tail rotor
  • Main Rotor Diameter17.07 m
  • Main Rotor Blades4
  • Anti-Torque Typetail rotor
▣Performance10MOD.10
  • Top Speed196 km/h
  • Cruise Speed163 km/h
  • Never-Exceed Speed (VNE)196 km/h
  • Service Ceiling1,495 m
  • Hover Ceiling (IGE)2,900 m
  • Hover Ceiling (OGE)2,300 m
  • Range390 km
  • Ferry Range1,000 km
  • Rate of Climb4.5 m/s
  • Endurance240
◇Dimensions & Weights7MOD.7
  • Fuselage Length14.63 m
  • Height4.85 m
  • Rotor Disc Area228.1
  • Empty Weight3,583 kg
  • Max Takeoff Weight6,350 kg
  • Useful Load2,767 kg
  • Cabin Volume6.23
◆Armament & Mission8MOD.8
▲Production2MOD.2
  • Total Built2,340
  • Variants10
◎Service History4MOD.4
  • Retirement Year1970
  • Production Start1954
  • Production End1970
  • Operational Statuslimited civil use in transport and external cargo lift roles; some restored as warbirds
03 / History
SERVICE LIFESPANRetired
  1. 1945First deployment: Cold War
  2. 1954Production started
  3. 1970Production ended
72
years in service
16
years in production
2,340
units produced
0
countries operating
ⓘ The producing country no longer actively operates it. 22 countries retired it.
04 / Conflicts
SIKORSKY H-34 · CONFLICTS SERVED IN50% win
Total Conflicts
2
Victories
1
Ongoing
0
Losses
0
ⓘ Shown only from conflicts recorded in our database.
05 / Operators
📖 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.
A mechanical device used to lift personnel or cargo via a cable, typically mounted on helicopters for rescue or recovery operations.
Aerodynamic containers mounted on aircraft, typically helicopters or fighter jets, that hold and launch unguided rockets in rapid succession.
These terms are listed automatically because they appear on this page.full encyclopedia →
📚 Sources
📖 ENCYCLOPEDIA Browse the Utility / Transport Helicopters entry →