AQ 002 Rev.00 Issued/Verify/Approval M. Garofolo 13/july/02
Identification: MM 002 Rev 01
Page: 9 of 26
Date: 20/april/2005
Issued: M. Fiorindo
Verify: R.Ciotti
Approval: R. Ciotti
Revisions description:
Updated manual
Storch CL, HS, S
Maintenance Manual
(for Rotax 912 UL/S, 914 UL and
Jabiru 2200 version)
1.5 10-HOURS INSPECTION
(1)
Ensure that the ignition key is REMOVED.
(2)
Check the manifold attaching bolts and the cylinder head nuts (only air-cooled engines) for proper
torque. Above check should be performed after the first 10 flight hours only.
For sequence and torque loads refer to engine Operator's Manual - last issue.
(3)
Inspect the air and fuel filters for clogging.
(4)
Inspect the rewind starter rope for conditions (this interval is applicable to aircraft equipped with
engine manual starting only).
Worn or -Frayed ropes are not acceptable. For replacement procedure, refer to engine Operator's Manual - last
issue.
(5)
For aircraft equipped with drive belt reduction unit, check: belt tension as follows:
(a)
Apply a force of 10 Kg (22 lbs) in the middle of each belt.
(b)
Measure the deflection on each belt which should result 7 mm approx. (0.270 in). If
necessary adjust the belt tension as detailed the subsequent items (c), (d), (e) and
(f).
(c)
Remove the spinner (if installed) and the propeller.
(d)
Using a socket wrench unloose the self-locking nut; for this operation apply an
opposite torque on the proper housing located in the eccentric. To increase the belt
tension turn the eccentric clockwise.
(e)
Torque the self-locking nut to 60 Nm (5:1,2 Lbs.in).
(f)
Reinstall the propeller. Torque the attaching bolts to 15 Nm (133 lbs.in).
(6)
Remove and check the spark plugs for condition. For evaluation criteria consult the engine
Operator's Manual. Spark Plug torque load: 27 Nm (240 lbs-in). Using a suitable solvent ,
clean the ignition cables terminals.
(7)
Carefully inspect the whole exhaust system (manifold, muffler, elbow) for cracks; verify the
serviceability of retaining -springs and rubber buffers.
(8)
Using a suitable, neutral, aqueous, free of solvents and abrasives detergent, clean the wings
and empennage.
In performing this operation take care that
some
detergent does not penetrate inside the
airframe: this to avoid contaminations and corrosions in not inspection able places.
