Tecnam P2002 JF - Wing Inspection

Page 211 2
nd
Edition - Rev 0
57-10
WINGS – MAINTENANCE PRACTICE
7. WING INSPECTION
Procedure
Step no.
Task description
Additional info &
References
1.
Engage parking brake
2.
Inspect wings skin along rivets line and
in particular:
 FWD spar upper and lower rivet line;
 AFT spar upper and lower rivet line;
 leading edge rivet line in correspondence
of wing taper;
check for cracks, deformation or rivets
loosening
No cracks , defor-
mation and rivet loos-
ing are allowed.
Refer to Figures 9. and
10.
3.
Check for FWD/AFT spar: lack of
cracks, corrosions and deformations
4.
Examine that wing and fuselage
FWD/AFT attachment points are free
from damages, corrosion or defor-
mations.
No deformation permit-
ted.
No corrosion permitted.
5.
Examine the main bolt assemblies. Look
especially for corrosion and deformation.
Replace bolts if required
Refer to figure 5.
6.
Examine FWD/AFT upper and lower
connection plates
Figure 5.
7.
Examine FWD/AFT upper and lower
connection insoles
Figure 5.