Aquila AT01, Руководство по обслуживанию

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MAINTENANCE MANUAL
AQUILA AT01
A
Page 25
05-20-00
16.09.19
Maintenance Checks
No. Inspection Items Inspection Finding / Initials
Fuselage Method Condition (Cont.)
27. Area around pedal control brackets - delamination, cracks. V
Cockpit Area and Baggage Compartment
28. Front cockpit floor - Check for delamination and cracks. V, T
Check bonding area to the fuselage structure for disbonding.
29. Front shear bulkhead - Check for delamination and cracks. V, T
Check bonding area to the fuselage structure for disbonding.
30. Front seat bulkhead - Check for delamination and cracks. V, T
Check bonding area to the fuselage structure for disbonding.
31. Seat elements and attachments - delamination, cracks. V, T
32. Rear seat bulkhead - Check for delamination and cracks. V, T
Check bonding area to the fuselage structure for disbonding.
33. Front landing gear bulkhead - Check for delamination and V, T
cracks. Check bonding area to the fuselage structure for
disbonding.
34. Rear landing gear bulkhead - Check for delamination and V, T
cracks. Check bonding area to the fuselage structure for
disbonding.
35. Baggage bulkhead - Check for delamination and cracks. V, T
Check bonding area to the fuselage structure for disbonding.
36. Lower lap belt attachments - Check for delamination and V
cracks. Check bonding area to the fuselage structure for
disbonding.
37. Lower lap belt fitting - Check for wear and corrosion. V
38. Upper lap belt attachments - Check for delamination and V, T
cracks at the baggage bulkhead.
39. Baggage compartment floor supports - Check for delamination V
and cracks. Check bonding area to the fuselage structure for
disbonding.
40. Gas spring supports - Check for delamination and cracks. V
Check bonding area to the fuselage structure for disbonding.
41. Composite tube stiffener and attachments - Check for V
delamination and cracks. Check bonding area to the fuselage
structure for disbonding.
42. Baggage compartment door, doorframe and supports - Check V
for delamination and cracks. Check bonding area to the
fuselage structure for disbonding.
43. Tailboom bulkheads - Check for delamination and cracks. V
Check bonding area to the fuselage structure for disbonding.