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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THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.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: Includes 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 Hovering Ceiling ISA m 5243 4632 4023 3475 3078
ISA+20C m 4084 3383 2743 2103 1707
OGE Hovering Ceiling ISA m 4450 3840 3246 2682 1890
ISA+20C m 3322 2652 1981 1311 914
Service 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 Range Cruise Speed (average) km/h 241 241 243 243 243
Range 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 Continuous Power kW 518 461
OEI (30 seconds) kW 701 629
OEI (2 minute) 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 Minutes kW 605
Takeoff Power (5 Minutes) kW 779
Continuous 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
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