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Tecnam P2002 JF - Page 128

Tecnam P2002 JF
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2
nd
Edition - Rev 0
Page 3
05-60
UNSCHEDULED MAINTENACE
ITEM
INSPECTION
INSPECTION
INTERVAL
Landing gear attach
points. (Not required for
severe turbulence.)
Buckling, cracks, overstress, wing
skin buckling and side brace for
damage and condition. Inspect land-
ing gear attachment bolts (magnetic
particle method).
Each occurrence, before
further flight.
Wings
Wing attachment bolts for slippage,
damage and overstress. Upper and
lower wing skins for wrinkles,
cracks, popped or loose rivets.
Remove access plates and inspect
for internal damage to ribs, stringers
and sparwebs; fuel tanks for damage
and leaks
Each occurrence, before
further flight.
Engine and propeller
Engine mounts for distortions and
damage to elastomeric parts. Propel-
ler for evidence of ground strike (i.e.
hard or overweight landing).
Each occurrence, before
further flight.
Fuselage
Canopy alignment, windows and at-
tachment for overstress cracks or
damage. Stringers, bulkheads, keel
beams for buckling, cracks or dam-
age. Avionics, instruments and ac-
cessories installation for security
and operation.
Each occurrence, before
further flight.
Empennages
Skin for buckling wrinkles, loose or
missing rivets. Stabilator and rud-
der for security of attachment and
overstress of bolts. Ribs, stringers
for buckling, cracks and damage.
Each occurrence, before
further flight.

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