Tecnam P2002-JF, Flight Manual, Page: 408 / 435

Page A14-34
Section 4 –Normal procedures
Checklists
3
rd
Edition, Rev. 0
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
CAUTION
Pilots shall adjust throttle friction in order to grant smooth and pre-
cise throttle control through both throttle systems (Hand Control -
rotation; Normal Throttles - push/pull) and at the same time it shall
be ensured that no inadvertent throttle increase may happen after
sudden a/c decelerations (e.g. during braking, landing, taxiing turns)
due to Rotax engine spring loaded throttle cable devices.
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 pressure build
up)
8. Electric fuel pump: OFF
9. Avionic Master switch (if installed) : ON, instruments check, then set in OFF
position
10. Flap control:
10.1 Switch selector: set to NORMAL
10.2 Control switch (standard): cycle fully extended and set UP
10.3 Switch selector: HAND CONTROL
10.4 Control switch (hand control): cycle fully extended 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
performance and take off rotation execution at the correct
V
R
IAS.
13. Nav. light & Strobe light: ON