MAINTENANCE MANUAL
AQUILA AT01-100
AMaintenance Checks
1. Spinner - Remove from aircraft and check for delamination 61-10-00 X
and cracks.
2. Spinner plate - Check for cracks and fit. X
3. Blade root and hub area - Examine for oil and grease leaks. X
4. Propeller blades - Check blade play (up to X
3 mm [1/8 in.] allowed).
35. Carburetors - Check the free movement of the carburetor R* 12-20-00 X 1 year
actuation (throttle lever and starting carburetor). Check that sec. 10.5
the Bowden cable allows full travel of the throttle lever from
stop to stop. Check Bowden cables for bulging with control
lever in the full throttle position. Adjust throttle control if 76-00-00
necessary. Lubricate carburetor throttle shaft. 12-22-00
36. Carburetor sockets and drip tray - Inspect the carburetor for Rotax Heavy MM, 200h1)
damage and abnormalities, check for cracks, wear and good 73-00-00
condition. Take note of any changes caused by temperature.
37. Airbox assy - Check for damage, security of attachment and X 1 year
condition. Inspect connected air hoses for condition and
leakage. Check that the flaps can be moved through their
full arc of travel for hot and filtered ram air.
38. Air filter - Inspect and clean. Renew if necessary. Clean air R* 12-20-00 X 1 year
filter casing. Check the drain hole at the bottom of casing sec. 2
for obstructions or blockage.
39. Other external engine accessories - Inspect screws and nuts X 1 year
of all other external engine parts and accessories for tight fit.
Inspect safety wiring if applicable, replace as necessary.
40. Engine mounts (manufactured by ROTAX and AQUILA) - R* 12-20-00 X 1 year
Check mounts for deformation, cracks, corrosion, sec. 3.1
security and damage from heat. Check mounting bolts for SB-912-028,
condition and correct torque value. latest Rev.
At engine (4 bolts M10): 40 Nm SB-AT01-022,
At shock mounts (4 bolts M10): 25 Nm latest Rev.
At firewall (4 bolts M10): 30 Nm
Inspect shock mounts for deterioration.
41. Engine test run - Attach cowling and perform an engine 17-10-00 X 50h2)
test run as described above in “Pre-Inspection/Engine Ground 05-20-00 1 year
Test”. 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.
Check oil level, replenish as necessary. R* 12-10-00
sec. 4.1
Page 7
05-20-00
No. Engine (Cont.) Reference Interval Initials
100h other
No. Propeller Reference Interval Initials
100h other
1) See SB-912-030 - latest edition.
2) If more than 30% of operation hours have been flown with leaded fuel e.g.: AVGAS 100LL (SI-912-016)
Temporary Revision 2, 14.08.14
