Sikorsky CH-53E Super Stallion

ICAO aircraft code H53S
Manufacturer Sikorsky Helicopter
Country United States
New price USD 24.36 million (1992)

The Sikorsky CH-53E Super Stallion is a heavy-lift helicopter operated by the United States military.

Specifications

Full description

Similar aircraft

Sikorsky CH-53E Super Stallion specifications

General

ICAO aircraft code
H53S
Manufacturer
Sikorsky Helicopter
Manufactured
1981 - 2003
Country
United States
New purchase price
USD 24.36 million (1992)

Aircraft performance

Avionics:
Rockwell Collins Avionics
Engine:
3x 3 × General Electric T64-GE-416/ GE-416A / GE-419
Turboshaft
Power:
4,380 HP
Max Cruise Speed:
150 Kts
278 Km/h
Travel range:
540 Nm
1,000 Kilometers
Fuel Economy:
0.5 Nm / gallon
0.245 Km / liter
Service Ceiling:
18,500 feet
Rate of Climb:
2500 feet / minute
12.70meter / second

Weight & dimensions

Max Take Off Weight:
33,340 Kg
73,501 lbs
Max Payload:
14,515 Kg
32,000 lbs
Fuel Tank Capacity:
2,810 gallon
10,637 liter

Disclaimer: The information on this page may not be accurate or current. Never use it for flight planning or any other aircraft operation purposes. No warranty of fitness for any purpose is made or implied. Flight planning or any other aircraft operations should only be done using official technical information provided by the manufacture or official aviation authorities.

About the Sikorsky CH-53E Super Stallion

The Sikorsky CH-53E Super Stallion is a heavy-lift helicopter operated by the United States military. As the Sikorsky S-80, it was developed from the CH-53 Sea Stallion, mainly by adding a third engine, adding a seventh blade to the main rotor, and canting the tail rotor 20°. It was built by Sikorsky Aircraft for the United States Marine Corps. The less common MH-53E Sea Dragon fills the United States Navy’s need for long-range minesweeping or airborne mine countermeasures missions, and perform heavy-lift duties for the Navy. Under development is the Sikorsky CH-53K King Stallion, which has new engines, new composite rotor blades, and a wider aircraft cabin; this is to replace the CH-53E.

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