Tecnam P2006T - Page 137

Page 4 - 21
Section 4 – Normal procedures
4
th
Edition, Rev. 0
3.9. TAKEOFF AND CLIMB
1
Landing light
ON
2
LH and RH Electrical Fuel pump
BOTH ON
3
Carburettors heat
CHECK OFF
4
LH and RH Propeller Lever
FULL FORWARD
5
LH and RH Throttle Lever
FULL POWER
6
Engines instruments
Parameters within green arcs
7
Rotation speed
MTOW 1180kg
MTOW 1230 kg
Vr = 64 KIAS
Vr = 65 KIAS
8
Apply brakes to stop wheel spin-
ning
9
Landing gear control knob
UP: check green lights and TRANS
light turned OFF within about 20”
10
Landing and taxi light
OFF above 10000 ft
11
LH and RH Propeller Lever
Set max cont power at safe altitude
CAUTION
Max take off power must be limited to 5 minutes. Reduce Throttles MAP
power before retracting Propeller to 2200 RPM or below.
12
LH and RH Electrical Fuel pump
BOTH OFF
It is recommended to retract landing gear when a positive climb rate
is ensured at the applicable best speed (V
Y
or V
X
as necessary).
It has been demonstrated that best climb rate is always obtained with
flaps in UP position: refer to Section 5, “Take off rate of climb” and
“Enroute rate of climb” tables.
Noteworthily best climb gradient speed (V
X
) flaps UP is lower than
best climb speed (V
X
) flaps T/O up to 6000 ft (density altitude).
Refer to Section 5, “Best climb gradient speed” table.
NOTE