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Aircraft data

Bell 412

The helicopter is used for inter-hospital transfer of intensive care patients, for emergency rescue operations, to transport physicians and equipment, for day and night operations (VFR/IFR).

Photo: Uwe Mattuschka

PERFORMANCE

Manufacturer: Bell Helicopters, Textron, USA
Engines: Pratt & Whitney PT6T-3B
Max. power per engine: 1,025 shp
Cruising speed: 250 km/h (135 kts/h)
Max. operating altitude:: Approx. 6,000 m NN (19,685 ft)
Endurance: 700 km (378 NM)
Max. fuel load: 1,250 Liter (330 US gal)
Max. take-off weight: 5,400 kg (11,905 lb)
Required take-off/ landing area: Approx. 28 x 28 m (91.9 ft x 91.9 ft) (Performance group 1, elevated Helipad)
Dimensions: Length: 17,10 m (55.77 ft)
Height: 4,60 m (13.12 ft)
Width: 2,80 m (6.56 ft)
Rotor Ø: 14,00 m (45.93 ft)
Crew: 2 pilots, HEMS crew member (paramedic), emergency physician

EQUIPMENT

Mobile Equipment: Emergency bag, pediatric emergency bag, suction unit
Artificial ventilation: Emergency care respirator, intensive care respirator
Circulation: Defibrillator, infusion pump, High-Flow-infusion pump, syringe pumps, pace maker
Trauma management: Scoop stretcher, vacuum mattress, pneumatic splint, KED-System, anti-shock trousers, burn pac
Diagnostics: ECG, blood pressure (invasive/ noninvasive), pulse oximetry, capnometry, temperature
Liquid gas supply: Oxygen 6,400 liters (1,690 US gal), Pressurized air 1,200 liters (317 US gal), air pump
Special equipment: ECLA, PECLA, IABP, NO-ventilation
Options: Incubator, safety harness, winch, life raft