Tecnam P2006T, Aircraft Flight Manual

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GARMIN G950 IFDS – SMP
FOR DIGITAL CONFIGURATION
Page SMP3-37
Ed.4, Rev.0
Section 3 – Emergency procedures
ONE ENGINE INOPERTIVE PROCEDURES
6.3 E
NGINE FAILURE DURING TAKEOFF RUN
BEFORE ROTATION: ABORT TAKE OFF
1.
Throttle Lever BOTH IDLE
2.
Rudder Keep heading control
3.
Brakes As required
When safely stopped:
4.
Failed Engine Ignition BOTH OFF
5.
Failed Engine Field
OFF
6.
LH and RH AUX FIELD switch
BOTH OFF
7.
Failed Engine Electrical fuel pump
OFF
IF THE DECISION IS TAKEN TO CONTINUE THE TAKEOFF:
WARNING
A take-off abort should always be preferred if a safe stop can be per-
formed on ground.
A suggested “GO-NO-GO” criteria is: abort take-off until LG is still
down and locked.
Once airborne accelerate to Blue Line Speed (V
YSE
) before command-
ing LG retraction.
Take-off planning should take into account that high density altitude
and aircraft mass may result in OEI negative climb rate.
V
YSE
with flap up shall be flown in order to achieve best possible rate
of climb after landing gear retraction and engine feathering.
1. Operating engine Throttle Lever FULL POWER
2. Operating engine Propeller Lever FULL FORWARD
3. Heading Keep control using rudder and
ailerons
4. Attitude Reduce as appropriate to keep
airspeed over 62 KIAS
5. Inoperative engine Propeller Lever FEATHER
6. Landing gear control lever UP
7. Airspeed V
XSE
/V
YSE
as required
8. Flaps 0°
9. LH and RH AUX FIELD switch BOTH OFF