AQ 002 Rev.00 Issued/Verify/Approval M. Garofolo 13/july/02
Identification: MM 002 Rev 01
Page: 16 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)
1.12 ANNUAL INSPECTION
(1)
Ensure that the ignition key is REMOVED.
(2)
Using a suitable torque wrench check the cylinder head securing nuts for proper torque. Torque load
required: 22 Nm (195 lbs.in).
(3)
Carefully examine all rivets for security of attachment. Rivets loosened should be replaced.
(4)
Bolts and self-locking nuts relevant to the installations listed below should be checked for
tightening:
-
Light controls and associated supporting devices;
-
connections engine - airframe;
-
engine controls and associated supporting devices;
-
landing gear.
(5)
Verify the nose landing gear for proper operation of hydraulic shock absorber.
(6)
Using a 10 X magnifying glass carefully inspect for cracks all welding relevant to:
- tubular framework interconnecting the wings;
- tubular framework supporting the main landing gear;
- nose gear drag struts (2 ea.);
- wheel axles (2 ea.);
- aileron torque tubes (2 ea.);
- pedals assemblies;
- stabilator hinge support;
- exhaust system components (manifold - elbow muffler);
- engine mount.
(7)
Front and rear wing fittings: using a vernier slide gauge check the hole diameters by taking two
measures at right angle each other (one vertically and the other horizontally).
Ovalization allowed: 0,5 mm MAX (.02 in MAX).
(8)
Carefully examine the wing fitting attaching bolts (4 c-,a.) for damage, distortion and corrosion.
Indentations on bolt working area are not acceptable.
(9)
Wing brace strut end fittings:
using a vernier slide gauge check the hole diameters by taking two measures at right angle each
other (one along the fitting centre line and the other at right angle).
Ovalization allowed: 0,4 mm
MAX (.(D16 in MAX).
(10)
Wing brackets for brace struts:
with the same method used in the previous item (9) check the hole diameters.
Ovalization allowed: 0,4 mm MAX (.016 in MAX).
