Increased Internal
Gross Weight Operations
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
CSP–900RFM206E–1
FAA Approved
Original
11–i/(11–ii blank)
S
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C
T
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XI
I
NCREASED
I
NTERNAL
G
ROSS
W
EIGHT
O
PERATIONS
TABLE OF CONTENTS
PARAGRAPH
PAGE
11−1. General
11−1
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11−2. Environmental Operating Conditions
11−2
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Figure 11−1. Ambient Temperature Envelope
11−2
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Figure 11−2. Controllability Envelope and Critical Azimuth for
Crosswind Operations
11−2
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11−3. Airspeed Limits
11−3
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Figure 11−3. VNE Placard
11−3
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11−4. Weight Limitations
11−3
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Figure 11−4. Longitudinal Center of Gravity Envelope
11−3
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11−5. Performance Data
11−4
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Figure 11−5. Height Velocity Diagram
11−4
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Figure 11−6. Single Engine Rate of Climb and Descent, at VY, OEI MCP,
6500 LBS Gross Weight
11−5
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Figure 11−7. Twin Engine Rate of Climb, at VY, MCP,
6500 Pounds Gross Weight
11−6
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Figure 11−8. Maximum Internal Gross Weight, IGE, 3.5 Foot Skid Height,
Standard Engine Inlet, Takeoff Power
11−7
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Figure 11−9. Maximum Internal Gross Weight, OGE,
Standard Engine Inlet, Takeoff Power
11−8
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Figure 11−10. Maximum Internal Gross Weight, IGE, 3.5 Foot Skid Height,
IPS Inlet, Takeoff Power
11−9
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Figure 11−11. Maximum Internal Gross Weight, OGE, IPS Inlet,
Takeoff Power
11−10
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Summary of Contents for MD900 with PW206E
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