AIR.ONE

Airbus Helicopters H225 vs Dassault Falcon 8x vs Sikorsky S 92

The Airbus H225 and Sikorsky S-92 are twin‑engine heavy helicopters designed for offshore, search‑and‑rescue, and utility transport, while the Dassault Falcon 8X is a long‑range, tri‑jet business aircraft optimized for high‑speed intercontinental travel. In range, the Falcon 8X is in a different class, typically capable of roughly 6,000+ nautical miles, enabling nonstop missions such as transoceanic or deep intercontinental routes. The H225 and S-92 have helicopter-class ranges, generally on the order of a few hundred nautical miles (often around 500 nm depending on payload and reserves), suited to regional point-to-point operations and offshore sectors rather than long-haul travel. For passenger capacity, both helicopters usually carry around 18–19 passengers in typical transport configurations (with layouts varying widely by operator and mission equipment), whereas the Falcon 8X is commonly configured for about 12–16 passengers in executive cabin layouts, with a certified maximum higher but rarely used in business-jet service.

SpecAIRBUS H225Dassault Falcon 8XSikorsky S-92
Summary
Cockpit222
DOC / nm$ 20.87$ 7.66$ 19.79
Min Crew222
Total Seats211721
Flight RulesIFR—IFR
ManufacturerAirbus HelicoptersDassault FalconSikorsky
Aircraft NameH2258XS-92
CertificationFAA / EASAFAA / EASAFAA / EASA
Max Range (nm)4546450439
DOC / nm / Seat$ 0.99$ 0.64$ 0.94
Max Cabin Seats281619
OEM VerificationUn-VerifiedVERIFIEDUn-Verified
Useful Load (lbs)11929369007417
Standard Cabin Seats191419
Direct Operating Cost$ 2,963$ 3,805$ 3,068
Flight Deck (Base Spec)EFISHoneywell Primus EASy IIEFIS
Max Cruise Speed (ktas)142516155
Base Aircraft Price (USD)$ 29,500,000$ 62,500,000 $30,650,000
Cabin
Cockpit232
Min Crew222
Total Seats211721
Max Cabin Seats281619
Standard Cabin Seats191419
Lavatory—2 Enclosed Flushing—
Crew Rest—No—
Jump Seat—Yes—
Galley Location—FWD—
Lavatory Location—FWD / AFT—
Cabin Pressure (psi)—10.2—
Galley / Refreshment—Galley—
SL Cabin Altitude (ft)—29200—
Max Cabin Altitude (ft)—3900—
Engine
FADECYesYesYes
ModelMakila 2A1PW307DCT7-8A
Fuel TypeJetFuel—JetFuel
TBO (hrs)3500On-Condition4000
Horsepower2100—2520
No. of Engines231
Fuel Capacity (gal)684—760
Flat Rating—ISA + 17—
Thrust (lbs)—6722—
Dimensions
Length (ft)63.480.2—
Overall Height (ft)16.326.117.8
Rotor Diameter (ft)53.2——
Cabin Volume (cu. ft)5471695775
Wingspan (ft)—86.3—
Cabin Width (ft)—7.7—
Cabin Height (ft)—6.2—
Cabin Length (ft)—42.7—
Cabin Width - Floor (ft)—6.3—
Cabin Length - Seating (ft)—29.2—
Baggage Volume Int. (cu. ft)—140—
Baggage Volume Ext. (cu. ft)——140