Our fleet includes Bell 427, Bell 407, Bell 212, Bell 206L, and Bell 206B helicopters operating in Manitoba.  Our Bell 407 helicopters offer better design, performance and lift capabilities than the 206B many other operators in Manitoba have available.

We’ve chosen these various model helicopters for their power, versatility, and the ability to get the job done in a safe and timely manner. We offer custom solutions for all your charter needs.

BELL 407 (4 Available)

Bell 407 C-FAUQ Helicopter

Crew: 1
Passengers: 6
Engine: 1 x Rols Royce 250-C47 turboshaft rated at 813 shp
Main rotor diameter: 35 ft length: 35 ft, height: 10.9 ft
Take-off weight: 6000 lbs
Avg empty weight: 2900 lbs
Max speed at sea level: 140 kn, Cruising speed at sea level: 130 kn
Service ceiling: 20,000 f
Range: 608km
Internal gross weight : 5250 lbs
External Gross weight 6000 lbs

BELL 206L (6 Available)

fleet fygb

Crew: 1
Passengers: 6
Engine 1x Rolls Royce 250 C30P rated @435 shp
Main rotor diameter: 37 ft length: 42 ft overall height 10 ft
Takeoff weight: 4250 lbs
Average empty weight: 2500 lbs
Max speed: 130 kn, Cruise speed: 115 kn
Service ceiling: 20,000 ft
Range: 340 km
Internal gross weight: 4150 lbs
External gross weight: 4250 lbs

BELL 206B (4 Available)

fleet fwgs

Crew: 1
Passengers: 4
Engine:1x  rated @  420 shp
Main rotor diameter:  33 ft length:  39 ft overall height  10.4 ft
Takeoff weight: 3200 lbs
Average empty weight: 1800 lbs
Max speed:  130 kn, Cruise speed: 110 kn
Service ceiling:  20000 ft Range:  450 kn
Internal gross weight: 3200 lbs
External gross weight 3350  lbs

BELL 427 (1 Available)

fleet fhed

  • Crew: 2
  • Capacity: 7 passengers / 2,960 lb (1,343 kg) internal load
  • Length: 37 ft 6 in (11.43 m)
  • Height: 10 ft 6 in (3.20 m) with standard skids[14]
  • Empty weight: 3,881 lb (1,760 kg)
  • Max takeoff weight: 6,550 lb (2,971 kg)
  • Powerplant: 2 × Pratt & Whitney Canada PW207D turboshaft engines, 710 shp (530 kW) each
  • Main rotor diameter: 37 ft 0 in (11.28 m)
  • Main rotor area: 1,075 sq ft (99.9 m2)
  • Blade section: – root: Boeing VR-7; tip: Narramore 8%[16]
  • Maximum speed: 140 kn (160 mph, 260 km/h)
  • Cruise speed: 138 kn (159 mph, 256 km/h)
  • Range: 394 nmi (453 mi, 730 km)
  • Service ceiling: 10,000 ft (3,000 m)
  • Rate of climb: 2,000 ft/min (10 m/s)


BELL 212 (1 Available)

  • Crew: 1 (two for IFR operation)
  • Capacity: 14 passengers
  • Length: 57 ft 1.68 in (17.4163 m)
  • Height: 12 ft 6.83 in (3.8311 m)
  • Empty weight: 6,529 lb (2,962 kg)
  • Max takeoff weight: 11,200 lb (5,080 kg)
  • Powerplant: 1 × Pratt & Whitney Canada PT6T-3 or -3B turboshaft engine, 1,800 shp (1,300 kW) (TwinPac)
  • Main rotor diameter: 48 ft 0 in (14.63 m)
  • Main rotor area: 1,809.5 sq ft (168.11 m2)
  • Blade Section: root: NACA 0010.8tip: NACA 0005.4 mod[21]
  • Cruise speed: 100 kn (120 mph, 190 km/h)
  • Never exceed speed: 120 kn (140 mph, 220 km/h)
  • Range: 237 nmi (273 mi, 439 km)
  • Service ceiling: 17,400 ft (5,300 m)
  • Rate of climb: 1,745 ft/min (8.86 m/s)
  • Disk loading: 6.19 lb/sq ft (30.2 kg/m2)