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#2080

Sikorsky CH-53E Super Stallion

🇺🇸 United States ·first flew 1974· heavy-lift cargo helicopter

Sikorsky CH-53E Super Stallion, photo 1 of 10
1/10 U.S. Navy photo by Mass Communication Specialist Seaman Sarah E. Bitter· Public domain

what is it?

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.

How to recognise it: 3 turboshaft engines · 24.1 m main rotor

base stats

  • speed 315 km/htop speed
  • range 1,000 kmwithout refuelling
  • seats 55passengers
  • size 33.3 tmax take-off weight
  • built 234made in total

Bars compare against all aircraft: 3,500 km/h, 20,000 km, 850 seats; size and number built on a log scale up to 640 t (An-225) and 45,000 built (Cessna 172).

fun facts

  • First flew 52 years ago, in 1974.
  • Top speed is 2.4× a car on the Dutch motorway (130 km/h).
  • Rotor of 24.1 m: about 5 cars parked nose to tail.
  • Fully loaded it can weigh as much as 6 African elephants (~6 t each).
  • Range of 1,000 km: 6× Amsterdam to Brussels.

turboshaft: A turbine that turns a shaft, usually a helicopter rotor.

spec sheet

first flight
1974
introduced
1981
status
still flying
number built
234
role
heavy-lift cargo helicopter
origin
🇺🇸 United States
makers
Sikorsky Aircraft Corporation
engines
3× General Electric T64-GE-416 / GE-416A / GE-419 / T64
crew
5
passengers
55
length
30.2 m
rotor diameter
24.1 m
height
8.5 m
max take-off weight
33.3 t
top speed
315 km/h
cruise speed
278 km/h
range
1,000 km
ceiling
5,639 m

Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.

Sources: Wikidata Q856317, Wikipedia: Sikorsky CH-53E Super Stallion (CC BY-SA 4.0).Updated 2026-10-24.

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