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THIS MANUAL SHALL BE IN THE HELICOPTER DURING ALL OPERATIONS COPYRIGHT NOTICE COPYRIGHT 2009 BELL ® HELICOPTER TEXTRON INC. AND BELL BHT-206B3 HELICOPTER TEXTRON CANADA LTD. ALL RIGHTS RESERVED Notice The instructions set forth in this manual, Ballast as required to maintain
weight empty CG within limits. Refer to Center of gravity vs Weight Empty chart in BHT-206B3-MM-1. LONGITUDINAL CENTER OF GRAVITY LIMITS Center of gravity limits are from station 106.0 (2692.4 mm) to 114.2 (2900.7 mm); however, the aft limits are variable depending upon gross weight. Refer to Center of Gravity vs Gross Weight chart (Figure 1-1) and BHT-206B3-MD-1.POWER PLANT LIMITATIONS Rolls Royce Model 250-C20B Engine or 250-C20J Engine. The 250-C20B engine limitations contained herein are applicable to the 250-C20J engine. POWER TURBINE (N2) OPERATING RPM LIMITS
weight empty CG within limits. Refer to Center of gravity vs Weight Empty chart in BHT-206B3-MM-1. LONGITUDINAL CENTER OF GRAVITY LIMITS Center of gravity limits are from station 106.0 (2692.4 mm) to 114.2 (2900.7 mm); however, the aft limits are variable depending upon gross weight. Refer to Center of Gravity vs Gross Weight chart (Figure 1-1) and BHT-206B3-MD-1.POWER PLANT LIMITATIONS Rolls Royce Model 250-C20B Engine or 250-C20J Engine. The 250-C20B engine limitations contained herein are applicable to the 250-C20J engine. POWER TURBINE (N2) OPERATING RPM LIMITS
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