BELL 206 — Performance
1 performance reference for the BELL 206.
Overview
BELL 206L-1 LONG RANGER II PERFORMANCE AND OPERATIONS HANDBOOK · 1999
This document is a Performance and Operations Handbook for the Bell 206L-1 Long Ranger II helicopter. It is intended for use by pilots and operators to understand the performance capabilities and operational limitations of the aircraft. The handbook includes critical information on operating limitations, performance data, weight and balance considerations, fuel and oil specifications, and various charts to assist in flight planning and operations. The data provided is derived from actual flight tests and is essential for ensuring safe and efficient flight operations.
- Maximum gross weight for internal operations: 4050 lbs (1837 kg).
- Maximum torque for takeoff: 100% for 5 minutes.
- Best rate of climb speed: 60 MPH (52 KTS) at maximum weight.
- Total fuel capacity: 376.3 liters (99.4 U.S. gallons), usable fuel: 372.4 liters (98.4 U.S. gallons).
- Maximum operating pressure altitude: 20,000 feet.
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