MD Helicopters MD900 with PW206E, Flight Manual

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CSP–900RFM206E–1
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
Limitations
FAA Approved
Original
2–4
2–3. AIRSPEED LIMITATIONS
Observe gross weight depictions on chart.
V
NE
decreases at a rate of 4 kts/1000 FT above 5500 Feet H
D
ÏÏÏ
ÏÏÏ
ÏÏÏ
ÏÏÏ
ÏÏÏ
ÏÏÏ
20000
15000
10000
5000
0
40 50 60 70 80 90 100 110 120 150 130 140
DENSITY
AL
TITUDE − FEET
INDICATED AIRSPEED − KNOTS
−30 ° C
−36 ° C
F92–010
V
NE
: AUTOROTATION
OEI OPERATIONS
HYDRAULICS FAILURE
VSCS FAILURE
XMSN CHIP LIGHT
100 KIAS ENVELOPE
140 KIAS
ENVELOPE
<5100 LB
V
NE
: POWER ON
V
NE
: −25 ° C
5100 − 6250LB
: V
NE
DUE TO
TIP MACH
Figure 2–3. V
NE
Chart
2–4. WEIGHT LIMITATIONS
Maximum gross weight: 6250 pounds.
Minimum flying gross weight: Refer to Figure 2−4.
Cargo deck capacity: 1500 lb. not to exceed 115 lbs. per square foot.
Maximum weight in baggage compartment (sta. 234 to 257): 500 lb. not to exceed
115 lb per square foot.