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MD Helicopters

Explorer MD900

tags: ALL

aircraft

Manufacturer:

MD Helicopters

Country:

USA

Commercial designation:

Explorer

Technical designation:

MD900

Version, Variant:

Type:

Notar

Currently produced:

Y

Typical missions:

ALL

Flight conditions:

First flight:

0

Landing system:

skids

Blades number:

5

Tail blades number:

13

weight

Weight class:

3

MTOW with external loads:

3130 kg

6902 lbs

MTOW with only internal loading:

2948 kg

6500 lbs

Empty weight:

1485.5 kg

3276 lbs

External payload:

1599 kg

3526 lbs

Internal payload:

1417.5 kg

3126 lbs

Standard fuel tank:

593 kg

1308 lbs

with optionnal external fuel tank:

685 kg

1510 lbs

performance

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

244.5 km/h

132 kt

Vne:

248 km/h

134 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

585.8 km

316 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

03:24:00 h:min

Rate of climb @ SL:

0 m/s

0 ft/min

Rate of climb @ SL @MTOW:

10.6 m/s

2086 ft/min

IGE max hovering altitude, MTOW:

3195 m

10480 ft

IGE max hovering altitude, empty:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, MTOW:

2820 m

9250 ft

IGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

OGE max hovering altitude, MTOW:

2634 m

8640 ft

OGE max hovering altitude, empty:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, MTOW:

2244 m

7360 ft

OGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

Service ceiling ISA, MTOW:

4200 m

13776 ft

Max operating altitude, empty weight:

4200 m

13776 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

power

APU in HC:

Engine manufacturer:

Pratt & Whitney

Model:

PW207E

Engines quantity:

2

Powerplant category:

turbine

Main rotor rotation speed:

392 rpm

Fuel consumption @ SL @ max continuous speed:

0 kg/kW/h

0 lbs/hp/h

Minimum consumption speed @ SL:

0 km/h

0 kt

Fuel consumption @ eco cruise speed @SL:

0 kg/h

0 lbs/h

Fuel consumption @ min consumption speed @ SL:

0 kg/h

0 lbs/h

Engines nominal power:

820 kW

1114 hp

Transmission shaft max continuous power:

746 kW

1014 hp

Transmission shaft max power:

820 kW

1114 hp

Takeoff power 5 min:

926 kW

1258 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

522 kW

709 hp

OEI max continuous power :

463 kW

629 hp

OEI max continuous transmission power:

463 kW

629 hp

OEI 30 sec transmission power:

0 kW

0 hp

OEI 2 min transmission power:

504 kW

685 hp

dimensions

Overall length:

11.84 m

39 ft

Rotor diameter:

10.31 m

34 ft

Tail rotor diameter:

0.56 m

2 ft

Fuselage length:

9.86 m

32 ft

Overall height:

3.32 m

11 ft

Main rotor blades chord:

0.25 m

1 ft

Tail rotor blades chord:

0.1 m

0 ft

Mast tilt angle:

0 °

noise

Noise at flyover, level:

83 dB EPNL

Noise at flyover, limit:

93 dB EPNL

Noise at takeoff, level:

85 dB EPNL

Noise at takeoff, limit:

94 dB EPNL

Noise at landing, level:

89 dB EPNL

Noise at landing, limit:

95 dB EPNL

seating

Crew:

1

Max pax number:

7

use

Average price:

3e+06 $

tags:

remarks: