Tecnam P2002-JF, Flight Manual, Page: 69 / 435

Section 4 – Normal procedures
Checklists
3
rd
Edition, Rev. 0
Page 4 - 7
C
HECKLISTS
3.3. B
EFORE
E
NGINE
S
TARTING
(A
FTER
P
REFLIGHT
I
NSPECTION
)
1. Seat position and safety belts adjustment
2. Flight controls: operate until their stop checking for movement
smoothness, free of play and friction.
3. Parking brake: engage and brake pedal press/brake lever pull
4. Throttle friction: adjust
5. Circuit Breakers: check all IN
6. Master switch: ON, Check generator light ON and Voltage (at least
10.5 V)
7. Electric fuel pump: ON, (check for audible pump noise and fuel pres-
sure build up)
8. Electric fuel pump: OFF
9. Avionic Master switch (if installed) : ON, instruments check, then set in
OFF position
10. Flap control: cycle fully extended and then set T/O
11. Pitch Trim: cycle fully up and down, from both left and right controls,
check for trim disconnect switch operation.
12. Pitch trim: set neutral
WARNING
Pitch trim other than in neutral position would affect take off per-
formance and take off rotation execution at the correct V
R
IAS.
13. Nav. light & Strobe light: ON
14. Fuel quantity: compare the fuel televels read with fuel quantity visually
checked into the tanks (see Pre-flight inspection – External inspection)
In absence of RH seat occupant: fasten seat belts around the seat
so as to prevent any interference with the aeroplane flight control
operation and with rapid egress in an emergency.
15. Canopy: Closed and locked
CAUTION
Avionic Master switch (if installed) must be set OFF during the en-
gine’s start-up to prevent avionic equipment damage.
NOTE