Eurocopter AS 350 83 Flight Manual page 88

FLIGHT MANUAL
.SECTION 5
~EGULATORY PERFORMANCE DATA
1 INTRODUCTION
The following perfomlance curves apply to the basic version of the
aircraft. Refer to the supplements when optional equipment is fitted.
2 SUBSTANTIATED WIND ENVELOPE
2.1 Wind envelope for spinnina and stopoino the rotors
.
Spinning or stopping of rotors has been substantiated for winds of
40 kts from any direction and for 50-kt headwinds.
-2.2 Wind envelope in hover
Hovering with wind from any direction has been substantiated over the
entire flight envelope up to winds of 17 kts, although this is not to
be taken as a limit. For example hover at sea level at maximum weight,
for all c.g. locations, has been substantiated at 30 knots.
3 AIRSPEED CALIBRATION
0 50 100 150 200 250 (km/h)
150 , ,. ..., , E
,g
(k1) 250
co
~ 200
100
.150
50 100
0
0
..
0
a 50
g
>'
2
0 50 100 (kt) 150 0
CAS
.
DGAC Approved: 350 B3 5. 1
I A I B I C I F I 97-40 Page 1