Aquila AT01, Maintenance Manual

Page: 38 / 50

MAINTENANCE MANUAL
AQUILA AT01
A
Page 20
05-20-00
16.09.19
Maintenance Checks
No. Inspection Items Inspection Finding / Initials
Right Method Condition Wing (Cont.)
Inner Flap Hinge Support Rib
6. Bonding area of rib to the wing shell - delamination, cracks. V, T
7. Condition of rib laminate, delamination, cracks. V, T
8. Bonding area at the main wing spar web. V
9. Areas around bushing - delamination, cracks. V
10. Condition of ball bearing, wear, corrosion. V
Wing Main Spar
11. Spar cap between root ribs - bonding to shear web, cracks. V
12. Shear web between root ribs - condition, cracks, delamination. V
13. Spar cap - inspection through openings in root rib and V
inspection opening in lower wing shell. Bonding to the wing
shell (cracks), condition of the main shear web (delamination).
Upper and Lower Wing Shell
14. Wing shell - delamination, cracks, scratches in shell surfaces, V, T
chipping of paint, UV damage.
15. Wing shell - core damage and dents in sandwich, disbond of V, T
shell laminate from core material.
16. Areas around inspection openings - delamination, cracks. V
17. Wing leading edge bonding area - disbonds, cracks. V, T
18. Area around tie-down fixation point - delamination, cracks. V, T
19. Area around NAV-light opening - delamination, cracks. V
20. Area around winglet root upper wing shell - cracks. V, T
21. Area around ring insert of the tank filler - cracks, disbonding. V, T
Trailing Edge Shear Web
22. Wing trailing edge, flap area - bonding lower to upper shell, V, T
disbond, cracks.
23. Wing trailing edge, flap area - laminate condition, cracks. V
24. Wing trailing edge, aileron area - bonding area shear web to V, T
wing shell, disbonds, cracks.
25. Wing trailing edge, aileron area - laminate condition, cracks. V
26. Bonding left an right of hinge levers for flap and aileron. V, T
27. Aileron hinge levers - delamination at bolt area, bolt corrosion. V