Figure 7-42.  Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA + 10 C (Sheet 2 of 2)
Figure 7-43.  Maximum Cruise Power One-Engine Inoperative 1900 RPM, ISA +20C (Sheet 2 of 2)

TM-55-1510-219-10 Army Aviation Maintenance Engineering Manual Weight and Balance
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