Bell 206L4 Product Specifications - Bell Helicopter
Bell 206L4 Product Specifications - Bell Helicopter
Bell 206L4 Product Specifications - Bell Helicopter
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Hovering Ceiling IGE - 2.5 ft Skid Height<br />
Rolls-Royce 250-C30P Engine at Takeoff Power<br />
High Altitude Tail Rotor<br />
Note: Takeoff and landing at gross weights above 4150 pounds/1882 kilograms is subject to density altitude limitation,<br />
see the FAA approved Rotorcraft Flight Manual Supplement BHT-<strong>206L4</strong>-FMS-19.<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. 18 <strong>Bell</strong> <strong>206L4</strong> <strong>Product</strong> Specification<br />
January 2012
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