MD Helicopters MD900 with PW206E, Flight Manual

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CSP–900RFM206E–1
Performance Data
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
5–49
5–10.HEIGHT VELOCITY DIAGRAM
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100
80
60
40
20
0
AL
TITUDE −
AGL
(FEET)
INDICATED AIRSPEED − KNOTS
0 5 10 15 20 25 30 35 40
SMOOTH HARD
SURFACE − WIND CALM
AVOID
AREA
CHART ‘‘A’’
ÉÉÉÉÉÉ
ÉÉÉÉÉÉ
ÉÉÉÉÉÉ
ÉÉÉÉÉÉ
ÉÉÉÉÉÉ
ÉÉÉÉÉÉ
ÉÉÉÉÉÉ
ÉÉÉÉÉÉ
ÉÉÉÉÉÉ
ÉÉÉÉÉÉ
ÉÉÉÉÉÉ
7000
6000
5000
4000
3000
2000
1000
0
5800 5900 6000 6100 6200
GROSS WEIGHT − LBS
DENSITY
AL
TITUDE − FEET
NOTE: IF THE COMBINATION OF
GROSS WEIGHT AND
DENSITY ALTITUDE FALL
IN THE SHADED REGION
OF CHART ‘‘B’’, THE
‘‘AVOID AREA’’ IN CHART
‘‘A’’ APPLIES.
CHART ‘‘B’’
F92–046A
Figure 5–41. Height Velocity Diagram
The clear area of Figure 5−41 Chart ‘‘B’’ represents density altitude/gross weight
combinations for which the height velocity diagram does not apply.
Safe landings and single engine fly−aways following an engine failure have been
demonstrated for the conditions stated below.
6000 LB gross weight at 7000 Ft H
D
and
6250 LB gross weight at 1400 Ft H
D
:
Safe landings following a vertical descent were demonstrated up to a 35 FT
skid height.
Safe run−on landings were demonstrated up to a 90 FT skid height.
Fly−aways were demonstrated down to a 100 FT skid height.