Fly Synthesis STORCH CL Maintenance Manual page 10

(1) Ensure that the ignition key is REMOVED.
(2) Check: the electrolyte level in the battery.
Replace the spark plugs. For replacement procedure
(3) Check the propeller attaching bolts for proper torque.
(4) Check the- driven wheel self locking nut for proper torque.
(5) Check the driving
(6) Check for proper torque the self-locking nuts and securing the engine to its housing and to the engine
mount respectively.
Torque loads required: nuts: 8 Nm (337 lbs-in); nuts: 22 Nm (195 lbs-in).
(7) Check for proper torque the self-locking nuts securing the engine mount to the fuselage. Torque
load, required: 10 Nm (89 lbs-in).
(8) Check for proper torque the self-locking nuts securing the shock absorbers and to the engine mount .
Torque load required: 10 NT, (89 lbs-ini).
(9) Check for proper torque the bolts securing the-engine cowling to the cylinder heads.
Torque load required: 15 Nm (133 lbs.in).
(10) Carefully inspect the brake control cables for condition (e.g. wear, broken wires) and security of
attachments.
Check that cables conduits are not bended or damaged.
(11) Inspect the push-pull control cables (55), (116) and the trim control cable (103) for general
conditions and, in particular, for cleaning and security of attachments.
(12) Ref. I.F'.C. Fig. 3: check tightening of self-locking nuts (5) and (3) securing the wings to
the tubular framework.
(13) Ref. I.P.C. Fig. 3: check tightening of self locking nuts (42) securing the wing brace struts.
(14) Ref. I.F'.C. Fig. 3: check tightening of self-locking nuts (14), (25), (32) securing the aileron control
1inkages.
(15) Ref. I.P.C. Fig. 3.. check tightening of bolts (21), (28) attaching the aileron hinge supporting plates
(19), (20), (26), (27) to the wings.
(16) Ref. I.P.C. Fig. 7, sheet 4 of 4: check tightening of self-locking nuts (119) attaching
push-pull control cable to the rudder and (141), (145) securing the rudder hinge pins.
(17) Ref. I.P.C. Fig. 7, sheet 2 of 4: check tightening of self-locking nuts (58) attaching the push-pull
control cables to stabilator hinge support and nuts (72) securing the hinge pin (70).
The same check should be performed on nuts
(67) and nut (79) connecting the hydraulic damper (77) to the same support (67).
(18) Ref. I.P.C. Fig. 7, sheet 2 of 4: check tightening of
self-locking nuts (90), (95), (99), (102), relevant to the anti-tab tension/regulator device.
Check the operating rod (96) for abnormal play.
(19) Check: all fuel hose connections for security.
(20) For engines equipped with drive reduction gear only: check oil level in the gearbox.
AQ 002 Rev.00
Storch CL, HS, S
Maintenance Manual
(for Rotax 912 UL/S, 914 UL and
Jabiru 2200 version)
1.6 20-HOURS INSPECTION
consult the engine Operator's Manual - last issue.
When engine is cold torque the spark plugs to 27 Nm
(240 lbs-in).
Required torque load: 15 Nm (133 lbs-in).
Required torque load:
wheel attaching bolt for proper torque.
Required torque load: 60 Nm (532 Lbs-in).
Issued/Verify/Approval M. Garofolo
Identification:
Page:
Date:
Issued:
Verify:
Approval:
Revisions description:
Updated manual
60 Nm (532 lbs-in).
(66) attaching the stabilator to its hinge support
13/july/02
MM 002 Rev 01
10 of 26
20/april/2005
M. Fiorindo
R.Ciotti
R. Ciotti
the