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Sikorsky S-58
Photo: U.S. Army · Wikimedia Commons · Public domain Use of this image does not imply endorsement by the U.S. Department of Defense (DoD).
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SikorskyS-58

Utility / Transport Helicopters · United States · 1955
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SikorskyS-58

Sikorsky S-58
Sikorsky S-58 Photo: U.S. Army · Wikimedia Commons · Public domain Use of this image does not imply endorsement by the U.S. Department of Defense (DoD).
* Absolute score — assessed within category · no era adjustment
Payload / Capacity
75
Range
60
Versatility
80
Reliability
70
Speed
55
Survivability
40
Hot-and-High Performance
50
Maintainability
65
Technology
45
Cost-Effectiveness
85
Origin United States
ManufacturerSikorsky Aircraft Corporation, AgustaWestland, Sud-Aviation
CategoryUtility / Transport Helicopters
EraEarly Cold War
In service1955–1970
Operators24 countries
Quantity2,340
Data Quality88%
64
Utility / Transport Helicopters MASS Rating
8/42
Early Cold War
108/208
All-Time
Utility / Transport Helicopters · 10 axes scored
Payload / Capacity
75
Range
60
Versatility
80
Reliability
70
Speed
55
Survivability
40
Hot-and-High Performance
50
Maintainability
65
Technology
45
Cost-Effectiveness
85
ⓘ Regardless of era, the same scoring system applies to all units in the utility / transport helicopters category.
01 / Overview
Sikorsky S-58
Production
1955–1970
Quantity
2,340
Operators
Conflicts
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
UTILITY / TRANSPORT HELICOPTERS · EARLY COLD WAR
8
PERFORMANCE/PRICE
90
UNIT COST (2025 USD)
—
64
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 Year1955
  • Crew2
  • Passengers12
  • Primary Roleutility transport, anti-submarine warfare, search and rescue, VIP transport
  • In ServiceYes
◈Powerplant8MOD.8
  • Engine TypeWright R-1820-84 Cyclone
  • Number of Engines1
  • Engine Power (each)1,120 kW
  • Transmission Rating1,120 kW
  • Rotor Configurationsingle main rotor, tail rotor
  • Main Rotor Diameter17.07 m
  • Main Rotor Blades4
  • Anti-Torque Typetail rotor
▣Performance10MOD.10
  • Top Speed194 km/h
  • Cruise Speed158 km/h
  • Never-Exceed Speed (VNE)198 km/h
  • Service Ceiling3,500 m
  • Hover Ceiling (IGE)2,900 m
  • Hover Ceiling (OGE)2,300 m
  • Range330 km
  • Ferry Range1,090 km
  • Rate of Climb4.6 m/s
  • Endurance3
◇Dimensions & Weights7MOD.7
  • Fuselage Length14.25 m
  • Height4.85 m
  • Rotor Disc Area228.1
  • Empty Weight3,470 kg
  • Max Takeoff Weight6,350 kg
  • Useful Load2,770 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, warbird restorations
03 / History
SERVICE LIFESPANStill in Service
  1. 1945First deployment: Cold War
  2. 1955Production started
  3. 1970Production ended
71
years in service
15
years in production
2,340
units produced
21
countries operating
ⓘ The producing country still actively operates it. 3 countries retired it.
04 / Conflicts
SIKORSKY S-58 · 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 →