Figure 7-13. Wind Components

Figure 7-12. Takeoff Weight - Flaps 40%, To Achieve Positive One-Engine Climb at Lift-Off Flaps 40%

Figure 7-14. Takeoff Distance - Flaps 0%

TM-55-1510-221-10 Army Model RC-12D Aircraft Manual
Page Navigation
246

TM 55-1510-221-10 WIND COMPONENTS Demonstrated Crosswind is 17 kts EXAMPLE: WIND SPEED ANGLE BETWEEN WIND DIRECTION AND FLIGHT PATH HEADWIND COMPONENT CROSSWIND COMPONENT Figure 7-13. Wind Components 7-18 Change 4 20 KTS 50% 13 KTS 15 KTS

Privacy Statement
Press Release
Contact