Sikorsky Ch-53e (H53)
ICAO H53 Medium

Sikorsky Ch-53e

Tri Rotorcraft

The Sikorsky CH-53E Super Stallion is the U.S. Marine Corps' largest and most powerful helicopter, and the only three-engine heavy-lift rotorcraft in Western military service. Introduced in 1981, the Super Stallion was designed to carry external loads up to 36,000 pounds, roughly double the capacity of its CH-53D predecessor, making it essential for amphibious assault operations, combat logistics, and disaster relief. Its triple General Electric T64 turboshaft engines deliver over 13,000 horsepower combined, enabling the aircraft to operate effectively in hot-and-high conditions and maintain flight even with one engine failed. The CH-53E can sling-load artillery pieces, light armored vehicles, and even downed aircraft, and its seven-blade main rotor gives it exceptional lifting power at altitude. With a cruise speed around 150 knots and a never-exceed speed of 170 knots, the Super Stallion prioritizes payload over speed, routinely operating from amphibious assault ships and forward bases. Its titanium rotor head and reinforced airframe allow it to withstand the stresses of shipboard operations and harsh combat environments. The type has seen extensive service in every major U.S. conflict since the 1980s, from Desert Storm to Afghanistan and Iraq, and remains the backbone of Marine Corps heavy-lift aviation despite plans for eventual replacement by the CH-53K King Stallion. SkyMeter has tracked flights across airframes and operators, with unique routes observed.

ACTIVE AIRFRAMES
last 7 days
🏢
OPERATORS
unique airlines
📊
FLIGHTS
tracked
AVG DURATION
per flight
INCIDENT RATE
0.0%
0 flagged

Safety in context

The incident rate counts flights with ANY safety event detected by SkyMeter: go-arounds (a routine response, not a failure), unstable-approach gate flags (advisory thresholds), rejected takeoffs (the system working as designed), and runway events. It is NOT an accident rate or fatality rate. For accident statistics, refer to the NTSB Aviation Accident Database (USA) or the Aviation Safety Network. See methodology for what each event type measures.

Performance

Speed envelope & approach

Vref
Vref range
Vmo
Mmo
Approach category

Dimensions

Airframe geometry

Wingspan
Length
Tail height
Wheelbase
Gear width
Wake category
M

Weight & identification

Operating limits

MTOW
73,500 lb
MALW
Manufacturer model
CH-53E
FAA designator
Registered

Top operators

By fleet size · last 7 days

0

No operator data available.

Safety profile

Flagged flights · last 7 days

No safety data available.

Recent flights

Real flights of H53 · airborne ≥ 20 min

17
06/11/2026
4h 53m
No alerts
06/10/2026
42m
No alerts
06/10/2026
19m
No alerts
06/10/2026
5h 0m
No alerts
06/09/2026
1h 35m
No alerts
06/09/2026
30m
No alerts
06/08/2026
28m
No alerts
06/08/2026
4h 41m
No alerts
06/04/2026
39m
No alerts
06/04/2026
58m
No alerts
06/02/2026
45m
No alerts
05/28/2026
1h 43m
No alerts
05/28/2026
4h 38m
No alerts
05/21/2026
21m
No alerts
05/21/2026
4h 3m
No alerts
05/20/2026
1h 18m
No alerts
05/20/2026
20m
No alerts
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© SkyMeter · All flight data subject to ODbL attribution · Tracking window: 7 days (free tier)