MAINTENANCE MANUAL
AQUILA AT01
Aviation by Excellence AG
05-50-00
Page 01
Maintenance Checks
UNSCHEDULED MAINTENANCE CHECKS
1.
A.
Special checks are to be carried out only in circumstances, outside routine inspections, where
event have occurred that may have caused damage to the aircraft or an impairment of
airworthiness possibly during the operation of the aircraft.
Furthermore, the 25-hour inspection necessary for a newly delivered aircraft and its engine, as
well as for overhauled engines and after extensive airframe repairs, falls under the special checks
since it must only be carried out once after the first 25 hours of operation of the aircraft.
2.
A.
25-Hour Inspection
After the first 25 hours of operation of a newly delivered aircraft and its engine, after an airframe
overhaul, and after extensive airframe repairs an inspection within the specifications of a 100-hour
inspection is to be completed (Refer to 05-20-00).
After the first 25 hours of operation of newly supplied or overhauled engines an inspection of the
engine and propeller must be performed. Refer to ROTAX Aircraft Engines Maintenance Manual
for ROTAX Engines Type 912 Series pertaining this inspection.
B.
Hard Landing
After an excessively hard landing or other unusual loads of the landing gear a thorough inspection
of the affected components and their attachment is required. Even if no obvious defects are
detectable, a visual inspection must be carried out. Perform the following:
(1) Prepare aircraft for visual checks as follows:
(a) Remove engine cowling (refer to 71-10-00).
(b) Remove landing gear fairings.
(c)
Inside cabin and baggage compartment, remove required carpets and floorboards to
gain access to the landing gear mounting brackets (Refer to 25-21-009.
(2) Inspect main landing gear.
(a) Check wheel fairings for damages such as cracks, dents and delamination.
(b) Inspect fairing mounts for cracks, distortion or other damage.
(c)
Inspect fuselage structure visually at such points and areas where the main landing gear
is attached. Check for stress marks, distortion, dis-bonding, and delamination. Inspect
main landing gear strut brackets for distortion, cracks and security of attachment. Check
condition of the polyamide inserts. Check bolts for correct torque.
(d) Check main gear struts for deformation and cracks. Inspect wheel axles for security of
attachment to struts and for any damage.
(e) Inspect tires for integrity and proper location of the red slide marks.
(f)
Inspect brake fluid carrying lines at the main landing gear for condition, leakage, and
security of attachment.
General
Special Checks
30.04.08
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