Fluggerät

Eurocopter EC135 P2/T2

Type
Light twin-turbine multi-purpose helicopter (leichter zweimotoriger Mehrzweckhubschrauber)

Country (Land)
Germany (Deutschland)

Manufacturer (Hersteller)
Eurocopter Deutschland
Postfach 801140
81663 München
Germany

Phone: 0049-89/6000-0
Fax: 0049-89/6000-9033
Internet: www.eurocopter.com

Helicopters with the Pratt & Whitney engine are designated as P1 or P2 (with higher rated version), while the Turbomeca variant is the T1 or T2 (the latter with the Arrius 2B2)

General (Allgemeine Angaben)
Crew (Besatzung): 1 or 2
Passengers (Passagiere):
   - 5 to 7 in standard version
   - 4 or 5 in VIP layout
   - One litter and 3 seats for doctor and medical attendants
   - Two litters and 2 seats for doctor and attendant
External load capacity (Außenlast): 1260 kg

Power plant (Antrieb): 2 x Turboméca Arrius 2B2 or (oder) 2 x Pratt & Whitney Canada PW206B2
Maximum power per engine (max. Leistung): The PW 206B2 has a take-off power of 463 kW (621 shp), a maximum continuous power of 419 kW (560 shp) and a 2 min emergency rating of 580 kW (77 shp). With the Arrius 2B2, take-off power is 452 kW (606 shp), maximum continuous is 426 kW (571 shp) and the emergency rating for two minutes is 580 kW (777 shp).
Main transmission ratings are 616 kW for take off and 566 kW max. continuous or 513 kW (687 shp) from a single engine in case of an emergency (2 minute limit).
Fuel consumption
   - 232 l/h at fast cruise speed, or 237 l/h with Arrius 2B2
   - 205 l/h at economical cruise speed or 219 l/h with Arrius 2B2

Dimensions (Abmessungen)
Fuselage length (Rumpfänge): 10,20 m
Fuselage width (Rumpfbreite): 1,56 m
Width over stabiliser (Breite über alles): 2,65 m
Total length, rotors turning (Länge über alles): 12,16 m
Height (Höhe): 3,51 m
Rotor diameter (Hauptrotordurchmesser): 10,2 m
Main rotor disk area (Rotorkreisfläche): 81,7 sq m
Fenestron diameter (Durchmesser des Fenestron): 1,0 m
Tail rotor disk area (Fenestronkreisfläche): 2,84 sq m

Cabin length (Kabinenlänge): ca. 3,50 m
Cabin width (Kabinenbreite): 1,5 m
Cabin height (Kabinenhöhe): 1,26 m maximum, 1,15 m in the back
Cabin floor area (Kabinenfläche): 3,15 sq m plus 1,15 sq m for the pilot
Cabin volume (Kabinenvolumen): 3,8 cu m plus 1 cu m for the pilot
Baggage compartment volume (Gepäckraumvolumen): 1,1 cu m

Weights (Massen)
Empty weight (Leermasse): 1490 kg
Useful load (Zuladung): 1265 kg or less, depending on outfitting (EMS packages weight 83 to 152 kg)
Max. external load (max. Außenlast): 1260 kg
Max. fuel (max. Kraftstoff): 536 kg usable or 560 kg usable from production number 250
Max. fuel, long range tank (Langstreckentank): 722 kg
Max. take-off weight (Max. Startmasse): 2835 kg
Max. take-off weight with external load (Max. Startmasse mit Außenlasten): 2900 kg

Performance (Flugleistungen)
Max. speed (VNE) (max. Fluggeschwindigkeit): 259 km/h (140 kts)
Max. cruise speed (max. Reisegeschwindigkeit): 256 km/h (138 kts)
Economical cruise speed (wirtschaftliche Reisegeschw.): 229 km/h with PW engine or 239 km/h with Arrius 2B2
Service ceiling (Dienstgipfelhöhe): 3045 m (10000 ft)
Rate of climb (Steigrate): 7,6 m/s (1500 fpm)
Hover ceiling (Schwebeflughöhe)
    - IGE (im Bodeneffekt): 3045 m (10000 ft) at ISA or 2315 m at ISA + 20 deg C or 2255 m at ISA + 20 deg C with Arrius 2B2
    - OGE (ohne Bodeneffekt): 2190 m (7200 ft) at ISA, 1100 m at ISA + 20 deg C or 1005 m at ISA + 20 deg C with Arrius 2B2
Range (Reichweite):
   - 595 km (321 NM) at economical cruise speed, standard tank, with Arrius 2B2
   - 615 km (332 NM) at economical cruise speed, standard tank
   - 621 km (335 NM) at economical cruise speed, new 560 kg tank, with Arrius 2B2
   - 646 km (349 NM) at economical cruise speed, new 560 kg tank
   - 799 km (431 NM) with long range tanks, with Arrius 2B2
   - 805 km (434 NM) with long range tanks
Endurance at sea level (Einsatzdauer):
   - 3:15 hours with Arrius 2B2
   - 3:23 hours with new 560 kg tank, Arrius 2B2
   - 3:30 hours at 65 KIAS, no reserves
   - 3:39 hours at 65 KIAS, no reserves, with new 560 kg tank

03.03.2009

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