AIR.ONE

Bell 407gxi vs Cessna 206 Turbo Stationair

The Bell 407GXi is a single‑engine turbine helicopter, while the Cessna Turbo Stationair (commonly the 206H Turbo) is a single‑engine turbocharged piston fixed‑wing airplane. In category terms, the Bell excels where vertical lift and hover matter—point‑to‑point access to confined sites, rooftop pads, unimproved clearings, and low‑speed observation—whereas the Stationair is oriented to runway‑based travel with efficient cruise and straightforward cross‑country utility. For range, the Turbo Stationair generally offers the longer legs in typical operations, often around 600–800 nautical miles depending on load, reserves, and conditions. The Bell 407GXi’s practical range is usually shorter, commonly on the order of roughly 300–400 nautical miles, varying with fuel configuration and mission profile. Passenger capacity is broadly similar but used differently. The Bell 407GXi typically carries one pilot plus up to five passengers (six total seats) with flexible cabin access. The Turbo Stationair commonly seats one pilot plus up to five passengers (six total), and can also be configured to emphasize cargo and utility loading.

SpecBell 407GXiCessna Turbo Stationair
Summary
Cockpit22
DOC / nm$ 4.43$ 1.08
Min Crew1—
Total Seats66
Flight RulesVFRVFR
ManufacturerBellCessna
Aircraft Name407GXi206 Turbo Stationair
CertificationFAA / EASAFAA / EASA
Max Range (nm)337703
DOC / nm / Seat$ 0.74$ 0.18
Max Cabin Seats5—
OEM VerificationVERIFIEDUn-Verified
Useful Load (lbs)2300—
Standard Cabin Seats54
Direct Operating Cost$ 589$ 174
Flight Deck (Base Spec)Garmin G1000H NXIGarmin G1000 NXi
Max Cruise Speed (ktas)133161
Base Aircraft Price (USD)$3,225,000 $745,000
Cabin
Cockpit22
Min Crew1—
Total Seats66
Max Cabin Seats5—
Standard Cabin Seats54
Engine
FADECYesNo
ModelM250-C47E/4TIO-540-AJ1A
Fuel TypeJetFuelAvGas
TBO (hrs)35002000
Horsepower862350
No. of Engines11
Fuel Burn (gph)46—
Fuel Capacity (gal)127.887
TBO (yrs)—12
Fuel Delivery—Fuel Injected
Dimensions
Width (ft)25.4—
Length (ft)41.428.3
Cabin Width (ft)53.6
Cabin Height (ft)3.94.2
Overall Height (ft)10.29.4
Rotor Diameter (ft)35—
Cabin Volume (cu. ft)125—
Baggage Volume Ext. (cu. ft)16—
Wingspan (ft)—36
Cabin Length (ft)—12.1
Baggage Volume Int. (cu. ft)—11