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Inspection after rigging cont.
6.
Left wing
a)
Check the aileron for excessive free play;
b)
Check the aileron drive if loose;
c)
Check airbrake, airbrake box and control rod for wear and free play. It
must be possible to retract the airbrake, even if it is pressed backwards
in direction of flight. If there is any water in the airbrake box, this has
to be removed;
d)
Check the wing shells for dents, delaminations and cracks, especially
close to the wing spars;
e)
Check leading and trailing edges for damage;
f)
Check aileron seals, see section 4.5 MM.
7.
Tail skid
a)
Check for good glued joint to fuselage, check if the skid is mounted in
the correct direction, the cable deflector and the corresponding cut out
in the skid plate must be at the front end;
b)
Check if drain hole in front of tail skid are open;
8.
Rear end of the fuselage
a)
Check the lower rudder hinge and the connection of the rudder cables
for wear, free play and correct securing;
b)
Check the bulkhead and fin trailing edge shear web for cracks and
delamination;
9.
Fin - horizontal tail
a)
Check the upper rudder hinge for wear and free play;
b)
Check the elevator for free play and correct control hook up;
c)
Check the securing of the of the tailplane (spring or ratched according
to TN51);
d)
Check the horizontal tail for free play;
e)
Check leading and trailing edges for damage;
f)
Check ports for total/Pitot pressure (if installed) and TE-probe for free
passage;
g)
Check the TE probe for correct insertion and fix it with tape;
h)
Check elevator seals, see MM section 4.5.
10. Right wing see item 6.
11. Fuselage nose
Check the ports for the static pressure and the pitot pressure for cleanliness.
Issued May 2011
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Flight Manual LS1-f
4.7
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