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Sikorsky H-53 Sea Stallion
Photo: Staff Sgt. Raul Gonzalez, USMC · Wikimedia Commons · Public domain
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SikorskyH-53SeaStallion

Heavy Lift Helicopters · United States · 1966
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SikorskyH-53SeaStallion

Sikorsky H-53 Sea Stallion
Sikorsky H-53 Sea Stallion Photo: Staff Sgt. Raul Gonzalez, USMC · Wikimedia Commons · Public domain
* Absolute score — assessed within category · no era adjustment
Lift Capacity
90
Sling-Load Capability
88
Range
75
Cargo Volume
85
Reliability
80
Hot-and-High Performance
70
Versatility
95
Survivability
65
Technology
70
Cost-Effectiveness
85
Origin United States
ManufacturerSikorsky Aircraft Corporation
CategoryHeavy Lift Helicopters
EraCold War
In service1966–1978
Operators6 countries
Data Quality87%
MASS(Military Archive Scoring System)
82
Heavy Lift Helicopters MASS Rating
5/9
Cold War
13/28
All-Time
Heavy Lift Helicopters · 10 axes scored
Lift Capacity
90
Sling-Load Capability
88
Range
75
Cargo Volume
85
Reliability
80
Hot-and-High Performance
70
Versatility
95
Survivability
65
Technology
70
Cost-Effectiveness
85
ⓘ Regardless of era, the same scoring system applies to all units in the heavy lift helicopters category.
01 / Overview
Sikorsky H-53 Sea Stallion
Production
1966–1978
Operators
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
HEAVY LIFT HELICOPTERS · COLD WAR
5
PERFORMANCE/PRICE
87
UNIT COST (2025 USD)
—
82
heavy lift helicopters category
ⓘ Performance/Price and MASS score are computed across all units in the heavy lift helicopters category, regardless of era.
02 / Specs & Design
◎General6MOD.6
  • First Flight1964
  • Service Entry Year1966
  • Crew2
  • Passengers55
  • Primary RoleHeavy-lift transport cargo helicopter
  • In ServiceYes
◈Powerplant8MOD.8
  • Engine TypeGeneral Electric T64-GE-413
  • Number of Engines2
  • Engine Power (each)2,109 kW
  • Transmission Rating3,356 kW
  • Rotor ConfigurationSingle main rotor with tail rotor
  • Main Rotor Diameter22.02 m
  • Main Rotor Blades6
  • Anti-Torque TypeTail rotor
▣Performance10MOD.10
  • Top Speed314.813 km/h
  • Cruise Speed278 km/h
  • Never-Exceed Speed (VNE)315 km/h
  • Service Ceiling5,105.4 m
  • Hover Ceiling (IGE)3,520 m
  • Hover Ceiling (OGE)2,590 m
  • Range1,000 km
  • Ferry Range1,640 km
  • Rate of Climb12.7 m/s
  • Endurance180
◇Dimensions & Weights7MOD.7
  • Fuselage Length20.422 m
  • Height7.6 m
  • Rotor Disc Area380.6
  • Empty Weight10,740 kg
  • Max Takeoff Weight19,100 kg
  • Useful Load8,360 kg
  • Cabin Volume31.9
◆Armament & Mission5MOD.5
  • Hardpoints0
  • Weapons Payload3,630 kg
  • Gun0.50-inch machine guns (RH-53D)
  • Sling Load Capacity9,100 kg
  • Rescue HoistYes
▲Production2MOD.2
  • Total Built412
  • Variants53
◎Service History4MOD.4
  • Retirement Year2012
  • Production Start1964
  • Production End1978
  • Operational StatusLimited service with some operators
03 / History
SERVICE LIFESPANStill in Service
  1. 1966Production started
  2. 1978Production ended
60
years in service
12
years in production
6
countries operating
ⓘ The producing country still actively operates it.
04 / Variants
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.
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 Heavy Lift Helicopters entry →