Tecnam P2002 JF - Page 772

Page 205 2
nd
Edition - Rev 0
57-10
WINGS – MAINTENANCE PRACTICE
Step
no.
Task description
Additional info &
References
8.
Remove pins that join the small bar to the
pushrods then connect aileron control
Refer to Figure 4.
9.
Connect flap control by removing roller bear-
ings that link push-pull rod
Refer to Figure 3.
10.
Connect the fuel quantity sensor wiring and the
position lights wiring
11.
For the right wing, connect stall-warning sys-
tem wires
12.
Install the fuel tank outlet inspection panel,
Fasten and install the fuel hose from the tank’s
outlet. Only for the left wing, connect also the
fuel return line.
13.
Install all wing-fuselage fairings
14.
Install the wing’s composite root-leading edge
NOTE
On the wing to fuselage main fittings, there is a gap of about 1mm between the wing’s
main spar lugs and the carrythrough. This gap may be present either on the front side
of the carrythrough or on the back side according to the wing to fuselage incidence set-
ting (regulated in Factory). Fill this gap using the shim 96-1-108-1 according to the
gap position.