ICP Savannah VG User manual

I.C.P. Srl
Savannah™ VG - XL VG AIRPLANE
MAINTENANCEMANUAL
01-12-51-122
Page 1
Issue 1/Revision 04
ICP Srl –S.P.16 km 15,150-14022 Castelnuovo Don Bosco (AT)
August 2011
Phone [phone] •Fax [phone]
MAINTENANCE MANUAL
Savannah™VG / XL VG
Copyright I.C.P. 2002
Savannah™ is registered trademark solely owned by ICP srl and their use in any form is strictly
forbidden.
The content of the present manual is the sole property of I.C.P. srl and cannot be reproduced by
third parties in any form whatsoever without ICP’s previous written authorization.

I.C.P. Srl
Savannah™ VG - XL VG AIRPLANE
MAINTENANCEMANUAL
01-12-51-122
Page 2
Issue 1/Revision 04
ICP Srl –S.P.16 km 15,150-14022 Castelnuovo Don Bosco (AT)
August 2011
Phone [phone] •Fax [phone]
LOG OF REVISIONS
Revision
Number
Revised
Pages
Description of Revision
Date
00
All
First version
06/06
01
All
Effective also for XL
11/08
02
11
Point 34, general change.
5/2/2009
03
16
1000h/1500h
27/2/2009
TABLE OF CONTENTS

I.C.P. Srl
Savannah™ VG - XL VG AIRPLANE
MAINTENANCEMANUAL
01-12-51-122
Page 3
Issue 1/Revision 04
ICP Srl –S.P.16 km 15,150-14022 Castelnuovo Don Bosco (AT)
August 2011
Phone [phone] •Fax [phone]
SECTION 1
INSPECTION SCHEDULE AND REPORTS
Paragraph
Page
1.1
Inspection schedule
4
1.2
Maintenance historic report
5
1.3
Inspection reports
6
1.3.1
Daily/pre-flight inspection
8
1.3.2
25 hours inspection
9
1.3.3
50 hours inspection
12
1.3.4
100 hours inspection
13
1.3.5
200 hours inspection
15
1.3.6
600 hours inspection
16
1.3.7
1000 hours inspection (Aircraft overhaul)
16
1.3.8
1500 hours inspection (Engine overhaul)
16
1.3.9
Consumer material
17

I.C.P. Srl
Savannah™ VG - XL VG AIRPLANE
MAINTENANCEMANUAL
01-12-51-122
Page 4
Issue 1/Revision 04
ICP Srl –S.P.16 km 15,150-14022 Castelnuovo Don Bosco (AT)
August 2011
Phone [phone] •Fax [phone]
1.1 INSPECTION SCHEDULE
The aircraft’s maintenance schedule is as indicated in the table below:
Daily/Pre-flight inspection
before the first flight each day
25 hours inspection/3 months
every 25 hours flight time/ 3 months
50 hours inspection
every 50 hours flight time
100 hours/12 months inspection
every 100 hours flight time/12 months calendar
time
200 hours/18 months inspection
every 200 hours flight time/18 months calendar
time
600 hours
every 600 hours flight time
1000 hours flight time/72 months
every 1000 hours flight time/72 months calendar
time
1500 hours inspection (Engine overhaul)
every 1.500 hours flight time
1.2 MAINTENANCE HISTORIC REPORT

I.C.P. Srl
Savannah™ VG - XL VG AIRPLANE
MAINTENANCEMANUAL
01-12-51-122
Page 5
Issue 1/Revision 04
ICP Srl –S.P.16 km 15,150-14022 Castelnuovo Don Bosco (AT)
August 2011
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Sc. flight time
Sc. cal. time
Total time
Date
Location
Mechanic
25
3 m
50
75
100
12 m
125
150
175
200
18 m
225
250
275
300
24 m
325
350
375
400
30 m
425
450
475
500
36 m
525
550
575
600
42 m
625
650
675
700
48 m
725
750
775
800
54 m
825
850
875
900
60 m
925
950
975
1.000
64 m
1.025
1.050
1.075
1.100
68 m
1.125
1.150
1.175
1.200
72 m

I.C.P. Srl
Savannah™ VG - XL VG AIRPLANE
MAINTENANCEMANUAL
01-12-51-122
Page 6
Issue 1/Revision 04
ICP Srl –S.P.16 km 15,150-14022 Castelnuovo Don Bosco (AT)
August 2011
Phone [phone] •Fax [phone]
Sc. flight time
Sc. cal. time
Total time
Date
Location
Mechanic
1225
1250
1275
1300
78m
1325
1350
1375
1400
84m
1425
1450
1475
1500
90m
1.3 INSPECTION REPORTS

I.C.P. Srl
Savannah™ VG - XL VG AIRPLANE
MAINTENANCEMANUAL
01-12-51-122
Page 7
Issue 1/Revision 04
ICP Srl –S.P.16 km 15,150-14022 Castelnuovo Don Bosco (AT)
August 2011
Phone [phone] •Fax [phone]
NOTE:
Below are indicated the exact meaning of all the terms used in the inspection reports in order to
avoid any possible misunderstanding.
Visual inspection
Inspection to be performed without using any instrument or testing device,
by expert and trained eye only.
Functional inspection
Inspection to be performed by supplying the component to be inspected
with the proper energy, in order to check its correct operativeness, without
removing the component from the aircraft.
Test
It’s a verification of a component, without disembarking it from the
aircraft, to be performed by using a tester or other suitable instrumentation,
to check its proper operation.
Check
It’s a verification, typically to be performed by the pilot, without removing
anything from the aircraft, to determine whether there is a correct cause-
effect relation produced by engaging the device to be checked.
Bench test
It’s a verification of a component, disembarked from the aircraft, to be
performed by connecting it to a testing bench or other laboratory suitable
instrumentation, to check its proper operation and measure some significant
parameters values.

I.C.P. Srl
Savannah™ VG - XL VG AIRPLANE
MAINTENANCEMANUAL
01-12-51-122
Page 8
Issue 1/Revision 04
ICP Srl –S.P.16 km 15,150-14022 Castelnuovo Don Bosco (AT)
August 2011
Phone [phone] •Fax [phone]
1.3.1 DAILY/PRE-FLIGHT INSPECTION
N.
DESCRIPTION
MECH.
CER. ST.
1
Without moving the aircraft, drain the airplane fuel system
2
Check all the airplane surfaces to assure there’s no noticeable
defects or any accumulation of slush, snow or other detrimental
material.
3
Remove all the mooring ropes and the gust lock devices.
4
Check there aren’t any defects in the windshield or windows.
5
Check the landing gear for no defects, no damaged tires, and tires
for proper inflation.
6
Check all the fairings and inspection panels for general condition,
safety and no loosen or missing fastener.
IMPORTANT: Your airplane is made with aeronautic alluminium (6061 T6) with good
anticorrosion characteristics, but however simple cleaning procedures are always necessary. It is
important to avoid water stagnation making appropriate drying. Don’t use pressure jet of water to
avoid infiltration into not accesible point.
The original finishing will remain for a long period, if periodically the airplane is washed with a
wet sponge and a car detersive. Rinse always with a lot of water.
Periodically, use a good not abrasive car wax.
If the airplain lies in an saltish ambient, (near the sea) it must be washed frequently with fresh
water; repeat treatment with a good not abrasive car wax.
IMPORTANT: due to continuous emission of Service Bullettins and Service Informations by Rotax,
I.C.P. Srl does not intend to transmit anymore those informations to Rotax engines owners. Those
informations are available on web site www.rotax-aircraft-engines.com in section
"Documentation": we also suggest to contact the official Rotax dealer in your country.
I.C.P. Srl does not take any responsability of eventual damage to persons and things due to lack of
application of Rotax prescriptions.

I.C.P. Srl
Savannah™ VG - XL VG AIRPLANE
MAINTENANCEMANUAL
01-12-51-122
Page 9
Issue 1/Revision 04
ICP Srl –S.P.16 km 15,150-14022 Castelnuovo Don Bosco (AT)
August 2011
Phone [phone] •Fax [phone]
1.3.2 25 HOURS/ 3 MONTHS INSPECTION
N.
DESCRIPTION
MECH.
CER. ST.
1
Remove all the engine fairings
2
Open the inspection panel on the bottom of the fuselage
3
Check the general conditions of the whole airframe
4
Check the propeller for dents and cracks; check the blades leading
edge protection for condition;
NOTE: if some vibrations are noted the prop should be balanced
5
Check for presence and integrity of the safety nuts or the safety
wire on the propeller’s hub
6
Check the battery for proper liquid level, drain pipe condition,
corrosion due to acid spills and for electrodes condition
7
Check the flight controls for freedom of movement, excessive
play; all screws and nuts must be in place, properly tightened and
fitted with their safety devices
8
Check the flight controls cables, their end fittings and the
nicopresses; to check out for broken wires in cable, touch it along
by hand and by a soft fabric piece; if required, replace the cable
with an original spare
9
Check the pulleys and the teflon guides
10
Lubricate all the moving parts
11
Check all the components for freedom of movement and
excessive play
12
Check the flight controls cables tension; the proper tension is 18-
24 lbs (9-12 kg); greater tension induce too high load on the
aircraft’s structure and make the flight controls too hard to
operate, lower tension induce a very imprecise and not ready
response; at the worst, some flutter at the moving surfaces may
arise; the too low tension cables ARE VERY DANGEROUS
12e
Check throttle lever on firewall and in particular the welding on
the 4 levers
13
Check the radiator is fully accessible by the cooling air and the
duct isn’t obstructed by grass, leaves or other debris; check for
coolant leaks, all the hoses and clamps are in place and properly
secured
14
Parachute: if installed, check for security, bridles condition, that

I.C.P. Srl
Savannah™ VG - XL VG AIRPLANE
MAINTENANCEMANUAL
01-12-51-122
Page 10
Issue 1/Revision 04
ICP Srl –S.P.16 km 15,150-14022 Castelnuovo Don Bosco (AT)
August 2011
Phone [phone] •Fax [phone]
the hook is locked, the control cable for condition
15
Check the electric wires for condition, routing and security; check
the anti-collision lights control box for condition, if installed
16
Check the flaperon and elevator springs for security; adjust if
required
17
Visually inspect the fuselage interior; close the inspection panel at
the fuselage bottom
18
Check the landing gear for general condition; check the wheel
fairings if installed, the tires for wear and proper pressure
19
Check and, if required, adjust the brake control
20
Check the nose gear elastic chord and the sliding strut for excess
of play, clean and lubricate properly
21
Check the pedal rods and rod-ends; clean and lubricate properly
NB
WARNING: following a hard landing, particularly if happened in
a crosswind situation, check the wheel fork alignment.
22
Check all the bolts, nuts and attachment connections of the wings:
all the safety locking devices should be in place and not broken
23
Check the flaperon hinges: they should be show freedom of
movement and no play and be fitted with the safety locks
24
Clean all the flaperon hinges and lubricate
25
Check all the empennages hinges for freedom of movement and
no play, clean and lubricate; Check the cable end attachment
fittings for condition, freedom of movement, no play, cleanliness
and lubrication
26
Inspect for condition and security the four (4) horizontal tailplane
to fuselage attachment connections
27
Check all the inspection panels for condition and security, their
hinges and fasteners; clean and lubricate properly
28
Inside the cabin check for general condition, open the control
stick repair, check all hinges, screws, nuts, safety locks, for
freedom of movement, excessive play
29
Lubricate the control stick mechanism (3 spots)
30
Close the control stick repair; make sure to fix it.
31
Visually inspect the cabin electrical system, the brake system’s
pipes and cables, the cabin switches, breakers, all controls
32
Lubricate the brake system cables and the rudder pedals
33
Clean all inside the cabin
NB
NOTE: to properly maintain the engine it’s strongly
recommended to follow the engine manufacturer instructions
and all Rotax service informations
34
Fuel system: visually inspect pipes, clamps, fuel filter, electric
pump and mechanical pump; clean and inspect float chambers and