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THE MOST CURRENT DOCUMENT INFORMATION IS AVAILABLE
FROM YOUR BELL HELICOPTER TEXTRON REPRESENTATIVE.
PRODUCT DATA
JANUARY 2003
DESIGN SPECIFICATIONS
METRIC
ENGLISH
MAIN ROTOR
Number of Blades
4
4
Diameter
12.8 meters
42 feet
Chord
36.1 centimeters
14.2 inches
RPM (100%)
348
348
TAIL ROTOR
Number of Blades
2
2
Diameter
2.1 meters
6.9 feet
Chord
25.4 centimeters
10 inches
RPM (100%)
1881
1881
ENGINES-TWO ROLLS-ROYCE 250-C40B ( Engine Rated Shaft Horsepower )
Twin Engine Power (Each)
5 Minute
557 kW
747 SHP
Maximum Continuous
461 kW
618 SHP
Single Engine Power
30 Second
629 kW
844 SHP
2 Minute
605 kW
811 SHP
30 Minute
588 kW
789 SHP
TRANSMISSION RATINGS (@100%RPM)
5 Minute @ Main Rotor Mast
779 kW
1045 SHP
MCP @ Main Rotor Mast
738 kW
989 SHP
Single Engine @ Input
30 Second
629 kW
844 SHP
2 Minute
605 kW
811 SHP
Continuous
532 kW
714 SHP
Содержание BELL 430
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