Tecnam P2006T, Aircraft Flight Manual

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Page G7-12
Section 9 – Supplements
Supplement no. G7 – AFM Supplement for CIS countries operators
3
rd
Edition, Rev. 0
L
ANDING EMERGENCIES
L
ANDING WITHOUT ENGINE POWER
Landing on the Airfield
CAUTION
Both engines failure condition requires both propellers feath-
ered and aircraft attitude set to maximum efficiency until the
selection of the field, on which to perform an emergency land-
ing, is made.
1.
Airspeed (VY+4kts) 84 KIAS (1180kg)
82
KIAS (1080kg)
79 KIAS (980kg)
2.
Flaps
Only 0°
3.
Landing gear control lever
DOWN
CAUTION
To shorten the landing gear extension time, evaluate the possi-
bility to use the emergency extension control. In this way the
time required to complete the extension is shorter by about 8
sec.
4.
Select landing field (check for obstacles and wind)
5.
Safety belts
FASTEN
Before touch down
6.
Fuel Selector
BOTH OFF
7.
Electrical fuel pump
BOTH OFF
8.
Ignitions
ALL OFF
9.
MASTER SWITCHES
ALL OFF
WARNING
Emergency Landing outside of airfield shall be performed with land-
ing gear retracted and starting flaps extension in FULL configura-
tion at 50 ft of altitude. To reach the maximum gliding distance at the
optimal airspeed above mentioned, and to reduce the loss of altitude
during a 180° turn, turn with 30° bank angle.
The distance covered in correspondence of the optimal speed V
Y
is
about 4000 meters by 1000ft of altitude.
The loss of altitude, when a 180° turn is performed with bank angle
of 30°, is about 200ft in correspondence of V
Y
.
NOTE
NOTE