259
THIS IS AN UNCONTROLLED DOCUMENT.
THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.
THE MOST CURRENT DOCUMENT INFORMATION IS AVAILABLE
FROM YOUR BELL HELICOPTER TEXTRON REPRESENTATIVE.
PRODUCT DATA
JANUARY 2003
WEIGHTS
KG
Standard Configuration Weight (Note 1)
2415
Normal Gross Weight
4218
External Gross Weight
4218
Standard Configuration Useful Load (Normal Gross Wt - Standard Configuration Wt)
1803
Maximum External Load [Cargo Hook Limit]
1270
Note 1: Inc ludes sixteen kilograms of engine oil. Ballast is not included in standard configuration weight (ballast is function of
installed equipment).
PERFORMANCE SUMMARY: (INTERNATIONAL STANDARD DAY EXCEPT AS NOTED)
• • • REFER TO DEMONSTRATED TAKEOFF & LANDING AND MAXIMUM OPERATING ALTITUDE NOTES ON THE PERFORMANCE CHARTS • •
•
TAKEOFF, GROSS WEIGHT
Kg
3400
3625
3850
4080
4218
IGE Ho vering Ceiling
ISA
m
5243
4632
4023
3475
3078
ISA+20C
m
4084
3383
2743
2103
1707
OGE Ho vering Ceiling
ISA
m
4450
3840
3246
2682
1890
ISA+20C
m
3322
2652
1981
1311
914
Ser vice Ceiling (MCP) - AEO
ISA
m
6096
6096
5685
5212
4932
(30-minute) - OEI
ISA m
4313
3795
3261
2804
2530
(continuos) - OEI
ISA
m
4142
3609
3106
2630
2359
Cruise @ Sea Level ISA
Maximum Continuous Speed
km/h
265
263
261
259
258
Long Rang e Cruise Speed (average)
km/h
241
241
243
243
243
Rang e at LRC, No Reserve
km
680
675
667
658
654
Category A Takeoff and Landing Ceiling (Note 2)
Ground Level or Elevated Helipad
ISA
m
2438
1829
1097
366
(Note 2)
ISA+20C
m
1615
945
274 3960 Kg (Note 2)
@SL
Endurance, @ Loiter 120 km/h
ISA
hr
3.8
Note 2: Maximum approved weight for Category A operations is 9000 pounds(4082 Kg).
ENGINE RATINGS:
Rolls-Royce 250-C40B with Full Authority Digital Electronic Control
Takeoff Power (5 Minutes)
kW
603
557
Maximum Contin uous Power
kW
518
461
OEI (30 seconds)
kW
701
629
OEI (2 min ute)
kW
656
605
OEI (30 minute)
kW
623
588
OEI (Continuous)
kW
603
557
TRANSMISSION RATING:
OEI (@ Input)
AEO (@ Mast)
30 Second
kW
629
2 Min utes
kW
605
Takeoff Power (5 Minutes)
kW
779
Contin uous
kW
532
kW
738
FUEL CAPACITY (USABLE):
Skid Landing Gear
935 Liters
Auxiliary(Optional)
182 Liters
SPECIFICATION SUMMARY (METRIC) - SKID GEAR
(Serial No. 49088 & Subsequent)
THE DATA SET FORTH ON THIS DOCUMENT ARE GENERAL IN NATURE AND MAY VARY WITH CONDITIONS. FOR PERFORMANCE DATA AND OPERATING LIMITATIONS FOR
ANY SPECIFIC FLIGHT MISSION, REFERENCE MUST BE MADE TO THE APPROVED FLIGHT MANUAL.
Uninstalled
Thermodynamic
Kilowatts
Engine Rated
Kilowatts
Содержание BELL 430
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