Aquila ATO1, Maintenance Manual

Page: 29 / 198

MAINTENANCE MANUAL
AQUILA AT01
Aviation by Excellence AG
1. Spinner - Remove from aircraft and check for delaminations 61-10-00 X
and cracks.
2. Spinner Plate - Check for cracks and fixing. X
3. Blade Root and Hub Area - Examine for oil and grease leaks. X
4. Propeller Blades - Check blade shake. (allowed up to X
3 mm [1/8 in.]
Bowden cables and levers for damage. The cables must allow
an easy movement of levers through their full range of travel.
Check for security of routing. Check for free movement of
carburator actuation (throttle and starting carburator).
37. Carburator Sockets and Trip Tray - Inspect for damage and Rotax Heavy MM, 600h
abnormalities, check for cracks, wear and condition as well P/N 899603,
as signs of abnormal temperature exposure. 73-00-00, Sec. 3.4.3
38. Airbox Assy - Check for damage, security of attachment and X
condition. Inspect connected air hoses for condition and
leakage. Check the flaps for hot and filtered ram air can be
moved in their full arc of travel.
39. Air Filter - Inspect and clean. Renew if necessary. Clean air R* 12-00-00 X
filter housing. Check the drain hole at the bottom of housing sec. 2.4
for obstructions or blockage.
40. Other Engine External Accessories - Inspect screws and nuts X
of all other external engine parts and accessories for tight fit.
Inspect safety wiring if applicable, replace as necessary.
41. Engine Mounts (manufactured by ROTAX and AQUILA R* 12-00-00
GmbH) - Check mounts for deformation, cracks, corrosion, Sec. 2.3 X
security and damage from heat. Check mounting bolts for SB-912-028, latest
condition and correct torque value. Rev.
At engine (4 bolts M10): 35 Nm
At shock mounts (4 bolts M10): 25 Nm
At firewall (4 bolts M10):
30 Nm
Inspect shock mounts for deterioration.
42. Engine Test Run - Install cowling and perform an engine 17-10-00 X
test run as described above under No. 3. 05-20-00
After engine test run, re-tighten oil filter by hand and
examine engine and engine compartment for signs of leakage.
Compare results with first engine test run.
Page 07
05-20-00
Maintenance Checks
No. Engine (Cont.) Reference Interval Initials
100 h Add.
30.04.08
No. Propeller Reference Interval Initials
100 h Add.