Tecnam P2002-JF, Flight Manual, Page: 164 / 435

Page A06-6
Section 9 – Supplements
Supplement no. A06 – AFM Supplement for CIS Countries Operators
3
rd
Edition, Rev. 0
4. Electric fuel pump: OFF
5. Throttle: full in until the engine stops running
6. Cabin vents: OPEN
7. Magnetos: OFF
8. Speed: 69 KIAS (maximum efficiency speed)
9. Do not restart the engine.
R
ECOVERY FROM
U
NINTENTIONAL
S
PIN
If unintentional spin occurs, the following recovery procedure should be used:
1. Throttle: idle (full out position)
2. Rudder: full, in the opposite direction of the spin
3. Stick: move and hold forward until spin is halted
As the spin is halted
4. Rudder: neutralize
5. Aeroplane attitude: make a smooth recovery by pulling the stick back
gently averting speeds in excess of V
NE
and maximum load factor
(n=+3.8)
O
THER
E
MERGENCIES
E
LECTRIC
P
OWER
S
YSTEM
M
ALFUNCTION
Causes for malfunctions are hard to establish but, in any case, problems of this
nature must be dealt with immediately. The following may occur:
Generator Light Illuminates
Generator light may illuminate for a faulty alternator or when voltage is above
16V, in this case the over-voltage sensor automatically shuts down the alterna-
tor.
In both cases proceed as follows:
1. Generator switch and master switch: OFF
2. Generator switch and master switch: ON
If the problem persist
3. Generator switch: OFF
4. Non vital electric equipments: OFF
5. Radio calls: reduce at the strictly necessary
The battery is capable of supply the electrical system enough time
to complete flight in emergency conditions, with normal flight
electric-loads including operation of flap and trim.
If the light turns off:
6. No further action is requested.
NOTE