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Bell 206L4 Product Specifications - Bell Helicopter

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Fuel Flow vs. Airspeed<br />

Pressure Altitude = 4, 000 FT<br />

OAT = 7°C (ISA)<br />

The data set forth on this document are general in nature and may vary with conditions.<br />

For performance data and operating limitations for any specific flight mission, reference must be made to the approved Flight Manual<br />

© 2012 <strong>Bell</strong> <strong>Helicopter</strong> Textron Inc. 26 <strong>Bell</strong> <strong>206L4</strong> <strong>Product</strong> Specification<br />

January 2012

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