MD Helicopters MD900 with PW206E, Flight Manual

Page: 150 / 450

Performance Data
CSP–900RFM206E–1
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
5–ii
PARAGRAPH PAGE
Figure 5−15. Single Engine Rate of Climb and Descent, at VY,
OEI MCP, and 6000 LB Gross Weight 5−20 . . . . . . . . . . . . . . . . . . . . . . .
Figure 5−16. Single Engine Rate of Climb and Descent, at VY,
OEI MCP, and 6250 LB Gross Weight 5−21 . . . . . . . . . . . . . . . . . . . . . . .
5−7. Rate of Climb − AEO 5−22 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5−17. Rate of Climb − AEO, at VY, MCP, 3500 Pounds Gross Weight 5−23 .
Figure 5−18. Rate of Climb − AEO, at VY, MCP, 4000 Pounds Gross Weight 5−24 .
Figure 5−19. Rate of Climb − AEO, at VY, MCP, 4500 Pounds Gross Weight 5−25 .
Figure 5−20. Rate of Climb − AEO, at VY, MCP, 5000 Pounds Gross Weight 5−26 .
Figure 5−21. Rate of Climb − AEO, at VY, MCP, 5500 Pounds Gross Weight 5−27 .
Figure 5−22. Rate of Climb − AEO, at VY, MCP, 6000 Pounds Gross Weight 5−28 .
Figure 5−23. Rate of Climb − AEO, at VY, MCP, 6250 Pounds Gross Weight 5−29 .
Figure 5−24. Rate of Climb − AEO, at VY, TOP, 3500 Pounds Gross Weight 5−30 . .
Figure 5−25. Rate of Climb − AEO, at VY, TOP, 4000 Pounds Gross Weight 5−31 . .
Figure 5−26. Rate of Climb − AEO, at VY, TOP, 4500 Pounds Gross Weight 5−32 . .
Figure 5−27. Rate of Climb − AEO, at VY, TOP, 5000 Pounds Gross Weight 5−33 . .
Figure 5−28. Rate of Climb − AEO, at VY, TOP, 5500 Pounds Gross Weight 5−34 . .
Figure 5−29. Rate of Climb − AEO, at VY, TOP, 6000 Pounds Gross Weight 5−35 . .
Figure 5−30. Rate of Climb − AEO, at VY, TOP, 6250 Pounds Gross Weight 5−36 . .
5−8. Hover Ceiling, AEO 5−37 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5−31. Hover Ceiling, IGE, 3.5 Foot Skid Height,
Standard Engine Inlet, Takeoff Power, Cabin Heat Off 5−38 . . . . . . .
Figure 5−32. Hover Ceiling, IGE, 3.5 Foot Skid Height,
Standard Engine Inlet, Takeoff Power, Cabin Heat On 5−39 . . . . . . .
Figure 5−33. Hover Ceiling, OGE, Standard Engine Inlet,
Takeoff Power, Cabin Heat Off 5−40 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5−34. Hover Ceiling, OGE, Takeoff Power, Standard Engine Inlet,
Cabin Heat On 5−41 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5−35. Hover Ceiling, IGE, 3.5 Foot Skid Height, IPS Installed,
Takeoff Power, Cabin Heat Off 5−42 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5−36. Hover Ceiling, IGE, 3.5 Foot Skid Height, IPS Installed,
Takeoff Power, Cabin Heat On 5−43 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5−37. Hover Ceiling, OGE, IPS Installed, Takeoff Power,
Cabin Heat Off 5−44 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5−38. Hover Ceiling, OGE, IPS Installed, Takeoff Power,
Cabin Heat On 5−45 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5−9. Hover Ceiling, OEI 5−46 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5−39. Hover Ceiling, OGE, Standard Inlet, 2.5 Minute OEI Power 5−47 . . .