F.
Disconnect the fuel quantity sensor wiring and, if present, the position lights wir-
ing.
G.
Disconnect flap control (see fig. C-4) by removing roller bearings (6) that link
push-pull rods (6) to flap control plate.
H.
Remove the luggage compartment floor to get the access to the aileron control
circuit.
I.
Disconnect aileron control (see fig. C-5) by removing pins (4) that connect the
small bar (3) to the pushrods (5).
J.
While supporting the wing, release at first the rear spar pin and then the two main
spar’s pins.
K.
Replace pins in their original location and cap fuel lines.
Reverse above procedure for reinstallation paying close attention to tighten main
spar bolts to the recommended value (NAS 6608-28 torque 100 Nm).
F
IGURE
C-3
W
ING FITTING PINS
To Next Page
Loading...
