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Sikorsky H-53
Photo: U.S. Navy · Wikimedia Commons · Public domain Use of this image does not imply endorsement by the U.S. Department of Defense (DoD).
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SikorskyH-53

Utility / Transport Helicopters · United States · 1959
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SikorskyH-53

Sikorsky H-53
Sikorsky H-53 Photo: U.S. Navy · 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
85
Range
75
Versatility
90
Reliability
80
Speed
70
Survivability
65
Hot-and-High Performance
85
Maintainability
75
Technology
70
Cost-Effectiveness
80
Origin United States
ManufacturerSikorsky Aircraft Corporation
CategoryUtility / Transport Helicopters
EraEarly Cold War
In service1959–1976
Operators7 countries
Quantity400
Data Quality88%
79
Utility / Transport Helicopters MASS Rating
1/42
Early Cold War
21/208
All-Time
Utility / Transport Helicopters · 10 axes scored
Payload / Capacity
85
Range
75
Versatility
90
Reliability
80
Speed
70
Survivability
65
Hot-and-High Performance
85
Maintainability
75
Technology
70
Cost-Effectiveness
80
ⓘ Regardless of era, the same scoring system applies to all units in the utility / transport helicopters category.
01 / Overview
Sikorsky H-53
Production
1959–1976
Quantity
400
Operators
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
UTILITY / TRANSPORT HELICOPTERS · EARLY COLD WAR
1
PERFORMANCE/PRICE
88
UNIT COST (2025 USD)
—
79
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 Flight1959
  • Service Entry Year1966
  • Crew2
  • Passengers38
  • Primary RoleUtility / Transport Helicopter
  • In ServiceYes
◈Powerplant8MOD.8
  • Engine TypeTurboshaft
  • Number of Engines2
  • Engine Power (each)2,927 kW
  • Transmission Rating5,595 kW
  • Rotor ConfigurationSingle main rotor with tail rotor
  • Main Rotor Diameter22.02 m
  • Main Rotor Blades6
  • Anti-Torque TypeTail rotor
▣Performance10MOD.10
  • Top Speed315 km/h
  • Cruise Speed278 km/h
  • Never-Exceed Speed (VNE)315 km/h
  • Service Ceiling5,640 m
  • Hover Ceiling (IGE)3,385 m
  • Hover Ceiling (OGE)2,560 m
  • Range1,000 km
  • Ferry Range1,600 km
  • Rate of Climb12.7 m/s
  • Endurance180
◇Dimensions & Weights7MOD.7
  • Fuselage Length17 m
  • Height5.32 m
  • Rotor Disc Area380.9
  • Empty Weight10,740 kg
  • Max Takeoff Weight19,100 kg
  • Useful Load8,360 kg
  • Cabin Volume21.3
◆Armament & Mission7MOD.7
▲Production2MOD.2
  • Total Built400
  • Variants5
◎Service History4MOD.4
  • Retirement Year1990
  • Production Start1959
  • Production End1976
  • Operational StatusRetired from frontline service
03 / History
SERVICE LIFESPANStill in Service
  1. 1959Production started
  2. 1976Production ended
67
years in service
17
years in production
400
units produced
5
countries operating
ⓘ The producing country still actively operates it. 2 countries retired it.
04 / Operators
📖 TERMS ON THIS PAGE3terms
Armored protective panels installed in the cockpit area of an attack helicopter to shield the crew from small arms fire and shrapnel.
Seats designed to absorb crash forces, reducing injury to occupants.
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 →