MD Helicopters MD900 Explorer, Flight Manual

Page: 163 / 564

CSP − 902RFM207E − 1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Performance Data
FAA Approved
Reissue 2
Revision 5
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 5-2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Table 5-1. FAA Noise Levels 5-2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Table 5-2. FAA Noise Levels 5-2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5-3. Density Altitude Chart 5-3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5-1. Density Altitude Chart 5-4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5-4. Airspeed Calibration 5-5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5-2. Airspeed Calibration Curve 5-6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5-5. Best Rate of Climb Speed 5-7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Figure 5-3. Best Rate of Climb Speed (VY) 5-8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5-6. Rate of Climb and Descent - OEI 5-9 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
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 5-10 . . . . . . . . . . . . . . . . .
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 5-11 . . . . . . . . . . . . . . . . .
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 5-12 . . . . . . . . . . . . . . . . .
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 5-13 . . . . . . . . . . . . . . . . .
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 5-14 . . . . . . . . . . . . . . . . .
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 5-15 . . . . . . . . . . . . . . . . .
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 5-16 . . . . . . . . . . . . . . . . .
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 5-17 . . . . . . . . . . . . . . . . .