Home
Download PDF
Order CD-ROM
Order in Print
Figure 7A-15. Takeoff Weight to Achieve Positive One-Engine-Inoperative Climb at Lift-Off, Flaps UP
Figure 7A-17. Minimum Takeoff Power at 2000 RPM With Ice Vanes Retracted (65 Knots)
TM-1-1510-218-10 Army C12C Aircraft Army C12D Aircraft Army C12T Aircraft Manual
Page Navigation
698
699
700
701
702
703
704
705
706
707
708
TM 1-1510-218-10
7A-20
Figure 7A-16. Takeoff Weight to Achieve Positive One-Engine-Inoperative Climb
at Lift-Off, Flaps APPROACH