Flight
and
operational
manual
TL
3000
SIRIUS
Page
36
5.1
Introduction
Section
5
provides
the
airspeed
indication
system
calibration
data,
stall
speed,
performances
and
other
information.
The
data
contained
in
this
section
have
been
calculated
from
the
results
of
aircraft
and
power
plant
flight
tests
conducted
in
a
good
technical
status
and
using
usual
piloting
techniques.
If
not
specified
otherwise,
the
performances
presented
in
this
section
are
valid
for
the
aircraft
maximum
take
‐
off
weight
and
calculated
for
the
conditions
of
the
International
Standard
Atmosphere
(ISA).
5.2
Specified
values
5.2.1
Airspeed
indication
system
error
correction
IAS
(km/h)
Cruising
configuration
(flaps
closed)
Take
‐
off
configuration
(flaps
to 10.5°)
Landing
configuration
(flaps
to
45°)
CAS
(km/h)
50
58
55
60
67
66
70
76
76
80
85
86
86
90
93
95
97
100
102
105
107
110
110
114
117
120
119
124
127
130
128
134
140
136
144
150
146
160
155
170
164
180
174
190
183
200
193
210
203
220
213
230
223
240
234
250
244
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