CSP–520N–1
MD 520N (500N) ROTORCRAFT FLIGHT MANUAL
TM
Original
5–i
FAA Approved
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C
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N
V
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ERFORMANCE
D
ATA
TABLE OF CONTENTS
PARAGRAPH
PAGE
5−1. General
5−1
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5−2. Noise Characteristics
5−1
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5−3. Airspeed Calibration Curve
5−2
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Figure 5−1. Airspeed Calibration Curve
5−3
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5−4. Density Altitude Chart
5−4
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Figure 5−2. Density Altitude Chart
5−5
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5−5. Speed For Best Rate of Climb
5−6
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Figure 5−3. Speed for Best Rate Of Climb
5−7
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5−6. Height Velocity Diagram/Gross Weight Limits For Height velocity diagram
5−8
Figure 5−4. Height Velocity Diagram
5−9
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Figure 5−5. Gross Weight Limits For Height Velocity Diagram
5−10
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5−7. Hover Ceiling Vs Gross Weight
5−11
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Figure 5−6. Hover Ceiling VS Gross Weight, IGE, 3−Foot Skid Clearance,
Short Landing Gear, Standard Engine Inlet, Takeoff Power
5−12
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Figure 5−7. Hover Ceiling VS Gross Weight, IGE, 3−Foot Skid Clearance,
Extended Landing Gear, Standard Engine Air Inlet,
Takeoff Power
5−13
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Figure 5−8. Hover Ceiling VS9 Gross Weight, IGE, 6−Foot Skid Clearance,
Standard Engine Air Inlet, Takeoff Power
5−14
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Figure 5−9. Hover Ceiling VS Gross Weight, Out of Ground Effect,
Standard Engine Air Inlet, Takeoff Power
5−15
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Figure 5−10. Hover Ceiling VS Gross Weight, IGE, 3−Foot Skid
Clearance, Short Landing Gear, Engine Air Particle Separator
Inlet,Takeoff Power
5−16
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Figure 5−11. Hover Ceiling VS Gross Weight, IGE, 3−Foot Skid Clearance,
Extended Landing Gear, Engine Air Particle Separator Inlet,
Takeoff Power
5−17
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Figure 5−12. Hover Ceiling VS9 Gross Weight, IGE, 6−Foot Skid Clearance,
Engine Air Particle Separator Inlet, Takeoff Power
5−18
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