MD Helicopters MD900 with PW206E, Flight Manual

Page: 149 / 450

Performance Data
CSP–900RFM206E–1
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original 5–i
S
E C T I O N
V
P
ERFORMANCE
D
ATA
TABLE OF CONTENTS
PARAGRAPH PAGE
5−1. General 5−1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5−2. Noise Characteristics 5−1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5−3. Density Altitude Chart 5−2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5−1. Density Altitude Chart 5−3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5−4. Airspeed Calibration 5−4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5−2. Airspeed Calibration Curve 5−5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5−5. Best Rate of Climb Speed 5−6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5−3. Best Rate of Climb Speed (VY) 5−7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5−6. Rate of Climb and Descent − OEI 5−8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5−4. Single Engine Rate of Climb and Descent, From −36
°
C to 0
°
C
at VY, OEI MCP, and 3500 LB Gross Weight 5−9 . . . . . . . . . . . . . . . . .
Figure 5−5. Single Engine Rate of Climb and Descent, From −10
°
C to 50
°
C
at VY, OEI MCP, and 3500 LB Gross Weight 5−10 . . . . . . . . . . . . . . . . .
Figure 5−6. Single Engine Rate of Climb and Descent, From 0
°
C to −36
°
C
at VY, OEI MCP, and 4000 LB Gross Weight 5−11 . . . . . . . . . . . . . . . . .
Figure 5−7. Single Engine Rate of Climb and Descent, From −10
°
C to 50
°
C
at VY, OEI MCP, and 4000 LB Gross Weight 5−12 . . . . . . . . . . . . . . . . .
Figure 5−8. Single Engine Rate of Climb and Descent, From −36
°
C to 0
°
C
at VY, OEI MCP, and 4500 LB Gross Weight 5−13 . . . . . . . . . . . . . . . . .
Figure 5−9. Single Engine Rate of Climb and Descent, From −10
°
C to 50
°
C
at VY, OEI MCP, and 4500 LB Gross Weight 5−14 . . . . . . . . . . . . . . . . .
Figure 5−10. Single Engine Rate of Climb and Descent, From −36
°
C to 0
°
C
at VY, OEI MCP, and 5000 LB Gross Weight 5−15 . . . . . . . . . . . . . . . . .
Figure 5−11. Single Engine Rate of Climb and Descent, From −10
°
C to 50
°
C
at VY, OEI MCP, and 5000 LB Gross Weight 5−16 . . . . . . . . . . . . . . . . .
Figure 5−12. Single Engine Rate of Climb and Descent, From −36
°
C to −0
°
C
at VY, OEI MCP, and 5500 LB Gross Weight 5−17 . . . . . . . . . . . . . . . . .
Figure 5−13. Single Engine Rate of Climb and Descent, From −10
°
C to 50
°
C
at VY, OEI MCP, and 5500 LB Gross Weight 5−18 . . . . . . . . . . . . . . . . .
Figure 5−14. Single Engine Rate of Climb and Descent, at VY, OEI MCP,
and 5750 LB Gross Weight 5−19 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .