More Capability, One Less Engine.

The Eagle Single is the work horse in the Bell Medium Lift helicopter market. This program, by virtue of a 9-passenger Supplemental Type Certificate approval process, converts the venerable Bell 212 helicopter from a twin engine to a single engine.

While maintaining the Type Certificate of the Bell 212, owners and operators alike enjoy the inherent benefits of the Bell 212, such as the 11,200 lb gross weight limitation, common Bell 212 part numbers, dual hydraulics, enhanced 212 airframe structure and the availability of the aftermarket accessories commonly found on today’s working machines.

As a by-product of the conversion, the Eagle Single has a resulting loss of weight from removing one engine, the original heavy avionics and associated wiring, producing a medium helicopter in the 5,900 lb empty weight range.

While performance of the helicopter alone has set a new standard, there are additional benefits from the program. Traditional cost of operation are reduced, allowing for more operating profits. Reliability is enhanced by incorporating modern-day avionics and upgrades to the instrument panel, fuel panel and collective head design. 

The Eagle Single has been designed to be the helicopter of choice in the medium lift market. An all-commercial helicopter ensuring lasting value, product support, part commonality, aftermarket accessories availability, and unmatched performance. Currently certified in Canada, USA, Australia, Chile, Peru and Indonesia.

 

Helicopter Specifications

ENGINE

Manufacturer

Model

Weight. lbs

Length, in

Width, in

Honeywell

T5317A or 17B

540

47.60

23.00

POWER RATING

Uninstalled, sea level,shp

1800

TRANSMISSION RATING

Takeoff, shp

Max Continuous, shp

1290

1130

20,000

7,800

6,800

1420

110

130

PERFORMANCE

Service Ceiling, Hp, ft

HIGE, ft, MGW, SL

HIGE, ft, ISA +20deg

ROC, fpm, 65 KIAS

Econ Cruise, S/L, kts

Vne, kts

FUEL CAPACITY

Standard tank

Aux or Ferry tank

215 gals

180 gals

AVG FUEL BURN

Gallons per hr (GPH)

GPH Per Seat

70-75

7.77-8.33

RANGE

Max Fuel, nm

Aux Fuel, No Res, nm

Endurance

336

624

3.07hrs Std Fuel, No Res

ROTOR SYSTEM

Main Rotor

Tail Rotor

Construction

2

2

Metal

PERFORMANCE
  • Giving you more, with one less engine

INCREASED PAYLOAD CAPACITY
  • 212 max gross weight allowance  

  • Lower empty weight

MAINTAINABILITY
  • Uses current 205 & 212 part numbers

  • Easier inspections

  • Lower direct operating cost

VALUE PRICED
  • Affordable alternative

  • Configured to your specifications

EAGLE Single Typical Configuration

(single engine Bell 212)

AVIONICS

Garmin GNS30 GPS/NAV/COM

King KY196A VHF Com NAT AMS-42 Audio Panel

Garmin GTX-330 Transponder Technisonic TFM550 FM Transceiver

DART Avionics Riser Console

ACCESSORIES

Dual Control

Bleed Air Heater

Cargo Hook

DART Cargo Mirror Kit

Co-Pilot External Cargo Hook Release

DART Bearpaws

DART Vertical Reference Door

DART Left Hand Seat STC

DART Shoulder Harness Kit

DART High Skid Gear

DART Cabin Door Roller Kit

DART Fuel Purge Canister

COMPONENT TIME REMAINING

Engine T53-17A or B

Fuel Control

Governor

Main Rotor Straps

Main Rotor Blades

Transmission

Servos

Tail Rotor Hub

Tail Rotor Blades

42 Degree Gearbox

90 Degree Gearbox

5000

2500

3000

1200

4000

6000

2500

2500

5000

5000

5000

EXTERNAL DIMENSIONS

Length, Fuselage, ft

Length, T/R Turning, ft

Length. Both Turning, ft

Width, Fuselage, ft

Width, Widest Point, ft

Width, Landing Gear, ft

Height, Top, Rotor Hub, ft

Height, Top, T/R Arc, ft

Height, Top, Tail Fin, ft

Gr Clearance, T/R Guard, ft

42.40

45.93

57.28

8.00

9.38

8.67

12.83

15.75

11.52

5.75

INTERNAL DIMENSIONS
Length, Max, ft

Width, Max, ft

Height, Max, ft

Volume, ft3

 

CABIN

7.67

8.00

4.33

220.00

BAGGAGE

7.09

1.74

2.26

28.00

EXTERNAL DIMENSIONS

Max Gross, lbs

Empty, lbs, Mission Typical

Useful load, lbs

External Load, lbs

Gross with Ext Load, lbs

11,200

5,990

5,210

5,000

11,200

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