TECHNICAL DESCRIPTION, OPERATING, MAINTENANCE AND REPAIR MANUAL
Inspection after Event Event description
first
25 hr
every
50 hr
every
100hr
Carried
out by:
Inspected
by:
4.1.9 Lubricate according to the Lubrication
Chart
*
5. MAIN LANDING GEAR
5.1 Visually check of the leg for
delaminations, damages, attachment,
bolts security
* * *
5.2 Visually check laminated fairing
(mudguard) condition-repair found
damages and cracks
* * *
5.3 Check tyres for condition, cuts, uneven
or excessive wear and slippage-replace
if need be. Check pressure – inflate at
required pressure ( see Flight Manual )
* * *
5.4 Visually check condition of the pads-
steady and symmetry abrasion of the
pads-replace a pad if need be The same
is valid for the brake disc.
* *
5.5 Visually check disc for cracks,
permanent deformation – replace if need
be. Check condition of bearings, wheel
free rotation, play
* *
6.
LIFTING SURFACE
6.1 Wing
6.1.1
Wing disassembly, Check of the bushing,
root of beam and root rib
After 200 flight hours
or once a year
6.1.2 Visually check of the wing surface for
damages, delaminations, recesses
* * *
6.1.3 Check of the surface for finding out of
the delaminations of the sandwich.
Contact aeroplane manufacturer if are
found larger areas of the delaminations.
*
6.1.4 Check plays of wing suspensions . Move
the wing tip upward-downward,
frontward-rearward. Contact aeroplane
manufacturer if the motions are greater
than 5 mm
* *
6.1.5 Check pitotstatic tube attachment at the
right wing
* * *
6.2 Aileron
6.2.1 Visually check of the aileron surface for
damages, delaminations and paint
damages
* * *
6.2.2 Check free movement, aileron hinge and
plays
* * *
6.2.3 Check security of control rod ends * * *
6.2.4 Lubricate the bearings *
6.2.5 Check control-surface weight balance
attachment
* * *
6.3 Flap
6.3.1 Visually check of the flap surface for
damages, delaminations
* * *
Date: 20.10.2008, Rev3 WT-9 Dynamic Section 3 Page 3 - 8
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