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The Siller Helicopters CH-54A (ICAO type S64) is an aircraft certificated in the Restricted Category Rotorcraft category. It has a maximum take-off weight of 21,300 kg. It offers a maximum range of 210 nm, a cruise speed of 91 knots, a service ceiling of 13,000 ft and seating for up to 2 across its variants.

Siller Helicopters CH-54A

Model overview

Fleet & certification

Built
4
Active
3
Certifying authorities
FAA
Variants

Per-variant specifications

VariantEngineMTOWRangeCruisePax
CH-54A
CH-54A
—21,300 kg210 nm91 kt2
Type certification

The FAA paperwork

TCDS H18NM · issued 1994-08-15

Category
Restricted Category Rotorcraft
MTOW
19,051 kg
Seats
2 crew · 5 passengers
Fuel
5,110 L
Approved fuelJP4JP5
Engine

(2) Pratt & Whitney JFTD12A-4A (T73-P-1)

Certification basis

FAR 21.25(a)(2) effective February 1, 1965, including Amendments 21-1 through 21-71.

Safety & ops history

Where to look next

Detailed safety & ops history coming soon — view this model's FAA Airworthiness Directives at FAA.gov.
CH-54A — frequently asked
What is the range of the Siller Helicopters CH-54A?

The Siller Helicopters CH-54A has a maximum range of 210 nautical miles across variants.

How many people can the Siller Helicopters CH-54A carry?

The Siller Helicopters CH-54A seats up to 2 across its variants.

What is the MTOW of the Siller Helicopters CH-54A?

The Siller Helicopters CH-54A's maximum take-off weight is 21,300 kg.

What is the ICAO type designator for the Siller Helicopters CH-54A?

The Siller Helicopters CH-54A's ICAO type designator is S64.

How many Siller Helicopters CH-54A aircraft are registered worldwide?

Sprinkle tracks 4 registered Siller Helicopters CH-54A airframes worldwide.

Registered CH-54A aircraft

Individual CH-54A airframes by tail number — registration history, operator and lineage.