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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THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.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 LBS
Standard Configuration Weight (Note 1) 5358
Normal Gross Weight 9300
External Gross Weight 9300
Standard Configuration Useful Load (Normal Gross Wt - Standard Configuration Wt) 3942
Maximum External Load [Cargo Hook Limit] 2800
Note 1: Includes thirty-five pounds 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 Lbs 7500 8000 8500 9000 9300
IGE Hovering Ceiling ISA ft 17,200 15,200 13,200 11,400 10,100
ISA+20C ft 13,400 11,000 9000 6900 5600
OGE Hovering Ceiling ISA ft 14,600 12,600 10,650 8800 6200
ISA+20C ft 10,900 8700 6500 4300 3000
Service Ceiling (MCP) - AEO ISA ft 20,000 20,000 18,650 17,000 16,180
(30-minute) - OEI ISA ft 14,15012,450 10,700 9200 8300
(continuous) - OEI ISA ft 13,590 11,840 10,190 8630 7740
Cruise @ Sea Level ISA
Maximum Continuous Speed ktas 147 146 145 144 143
Long Range Cruise Speed (average) ktas 133 134 134 135 135
Range at LRC, No Reserve nm 286 283 280 277 275
Category A Takeoff and Landing Ceiling (Note 2)
Ground Level or Elevated Helipad
ISA ft 8000 6000 3600 1200 (Note 2)
ISA+20C ft 5300 3100 900 8730 lbs(Note 2)
@SL
Endurance, @ Loiter 65 kts ISA hr 2.8
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) SHP 808 747
Maximum Continuous Power SHP 695 618
OEI (30 seconds) SHP 940 844
OEI (2 minute) SHP 880 811
OEI (30 minute) SHP 835 789
OEI (Continuous) SHP 808 747
TRANSMISSION RATING: OEI (@ Input) AEO (@ Mast)
30 Second SHP 844
2 Minutes SHP 811
Takeoff Power (5 Minutes) RHP 1045
Continuous SHP 714 RHP 989
FUEL CAPACITY (USABLE):
Wheel Landing Gear 187.5 US Gallons
Auxiliary(Optional) 48 US Gallons
SPECIFICATION SUMMARY (ENGLISH) - WHEEL 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.
Engine Rated
Shaft Horse-
power
Uninstalled
Thermodynamic
Shaft Horsepower
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