Flight
and
operational
manual
TL
3000
SIRIUS
Page
38
5.2.5
Climb
Optimal
climb
speed
(km/h)
Rate
of
climb
(m/s)
120
4,82
NOTE:
The
climb
stated
in
the
table
above
is
valid
in
the
sea
level
and
International
Standard
Atmosphere
conditions
and
for
the
specified
runway
type.
5.2.6
Cruising
flight
Regime
Economical
cruise
Maximum
permanen
Maximum
Take
‐
off
Time
limitation
unlimited
unlimited
5
minutes
max.
Engine
rotations
4500
5500
5800
Flight
altitude
(ft)
IAS
(km/h)
IAS
(km/h)
IAS
(km/h)
2000
178
22
227
4000
181
22
228
5000
180
22
229
5.2.7
Endurance
Regime
Maximum
permanent
Economical
cruising
Engine
rotations
(rpm)
5500
4500
IAS
(km/h)
221
178
Airspeed
CAS
(km/h)
214
172
Consumption
(litres
per
hour)
19
11
Range
(km)
1400
2000
NOTE:
The
consumption
and
range
values
are
valid
for
the
aircraft
maximum
take
‐
off
weight
and
flight
altitude
of
2000
ft
ISA.
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