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Airbus Helicopters H225 vs Leonardo Aw189 vs Piper M600 Sls vs Sikorsky S 92

The Airbus H225 and Sikorsky S‑92 are large, twin‑engine heavy helicopters built for offshore transport and SAR, typically carrying around 18–19 passengers in an airline-style layout (higher in dense seating). Their real-world mission radius varies strongly with payload and reserves, but they generally offer long helicopter legs, roughly on the order of 400–600 nm. The Leonardo AW189 is a smaller, “super‑medium” twin helicopter, commonly configured for about 16–18 passengers, with a similar class-leading offshore focus but usually somewhat less cabin volume and lift than H225/S‑92. Its typical operating range is broadly comparable but often a bit shorter depending on fit, roughly around 400–500 nm. The Piper M600 SLS is a single‑engine turboprop airplane, not a helicopter. It carries up to six occupants (one pilot plus five passengers) and trades vertical capability for much greater cruise efficiency and range, typically around 1,000+ nm, making it better for point‑to‑point travel between runways rather than offshore deck operations.

SpecAIRBUS H225AGUSTA / LEONARDO AW189Piper M600 SLSSikorsky S-92
Summary
Cockpit2222
DOC / nm$ 20.87$ 15.57$ 2.19$ 19.79
Min Crew2112
Total Seats2121621
Flight RulesIFRIFRIFRIFR
ManufacturerAirbus HelicoptersLeonardoPiperSikorsky
Aircraft NameH225AW189M600S-92
CertificationFAA / EASAFAA / EASAFAA / EASAFAA / EASA
Max Range (nm)4546511406439
DOC / nm / Seat$ 0.99$ 0.74$ 0.55$ 0.94
Max Cabin Seats2819—19
OEM VerificationUn-VerifiedUn-VerifiedVERIFIEDUn-Verified
Useful Load (lbs)11929—22007417
Standard Cabin Seats1919419
Direct Operating Cost$ 2,963$ 2,413$ 603$ 3,068
Flight Deck (Base Spec)EFISEFISGarmin G3000EFIS
Max Cruise Speed (ktas)142155274155
Base Aircraft Price (USD)$ 29,500,000$2,413,000$3,081,400 $30,650,000
Cabin
Cockpit2222
Min Crew2112
Total Seats2121521
Max Cabin Seats2819—19
Standard Cabin Seats1919419
Lavatory——No—
Galley Location——MID—
Cabin Pressure (psi)——5.6—
Galley / Refreshment——Refreshment Centre—
SL Cabin Altitude (ft)——12600—
Max Cabin Altitude (ft)——8644—
Engine
FADECYesYesNoYes
ModelMakila 2A1CT7-2E1PT6A-42ACT7-8A
Fuel TypeJetFuelJetFuel—JetFuel
TBO (hrs)3500400036004000
Horsepower210019836002520
No. of Engines2211
Fuel Capacity (gal)684—260760
Flat Rating——ISA + 55—
Dimensions
Length (ft)63.457.829.7—
Overall Height (ft)16.316.611.317.8
Rotor Diameter (ft)53.248——
Cabin Volume (cu. ft)547395165775
Baggage Volume Ext. (cu. ft)—85—140
Wingspan (ft)——43.2—
Cabin Width (ft)——4.1—
Cabin Height (ft)——4—
Cabin Length (ft)——12.3—
Baggage Volume Int. (cu. ft)——20—