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I.C.P. Srl

 

Savannah™ VG 

- XL VG 

 AIRPLANE 

MAINTENANCEMANUAL 

 

01-12-51-122

 

Page 11 

 

Issue 1/Revision 04 

ICP Srl

 – S.P.16 km 15,150-14022 Castelnuovo Don Bosco (AT) 

August 2011 

Phone +39-0119927503  

  Fax +39-0119927266 

 

replace fuel filter if necessary. 

35 

Check and lubricate throttle and mixture cables and linkages; if 
required, adjust engine idle and idle carburation  

 

 

36 

Check the air hoses and air filters condition 

 

 

37 

Lubrication system: check for condition all pipes and clamps; 
check for the proper oil level, refill if required 

 

 

38 

Cooling system: check for condition all pipes and clamps, coolant 
level and coolant level in the coolant recovery reservoir, check all 
cooling system components are properly secured  

 

 

39 

Engine electrical system, ignition system: check for general 
condition, properly fastened electrical connections, no damaged 
wires, no connections oxidation, etc.; check the ignition harnesses 
be properly connected to the spark plugs 

 

 

40 

Spark plugs cleaning; re-gap or replace as required 

 

 

41 

By using a suitable tester (differential pressure gauge) check the 
engine compression 

 

 

42 

Check the engine silent-blocks, the engine and engine mount  
attachments 

 

 

43 

Check the exhaust system for cracks, loose fasteners, springs in 
place and oxidation 

 

 

44 

Thoroughly clean both the engine and its accessories 

 

 
 

 
45 

Check for condition of the air-box support spring  

 

 

 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

Summary of Contents for Savannah VG

Page 1: ...9 0119927503 Fax 39 0119927266 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 ...

Page 2: ...m 15 150 14022 Castelnuovo Don Bosco AT August 2011 Phone 39 0119927503 Fax 39 0119927266 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 ...

Page 3: ...CHEDULE 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...

Page 4: ...re 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 fligh...

Page 5: ...one 39 0119927503 Fax 39 0119927266 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 ...

Page 6: ...sue 1 Revision 04 ICP Srl S P 16 km 15 150 14022 Castelnuovo Don Bosco AT August 2011 Phone 39 0119927503 Fax 39 0119927266 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 ...

Page 7: ...h 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 aircraf...

Page 8: ... 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 ...

Page 9: ...itted 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 Ch...

Page 10: ...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...

Page 11: ...lamps coolant level and coolant level in the coolant recovery reservoir check all cooling system components are properly secured 39 Engine electrical system ignition system check for general condition properly fastened electrical connections no damaged wires no connections oxidation etc check the ignition harnesses be properly connected to the spark plugs 40 Spark plugs cleaning re gap or replace ...

Page 12: ...TE The 50 hours inspection requires that a 25 hours inspection is carried out plus the checks below stated N DESCRIPTION MECH CER ST 1 Check out all the movable surfaces deflection angles make reference to the attached drawing 2 Check the nose landing gear wheel and vertical tailplane alignment 3 Check the brakes operating effectiveness clean or replace the pads as required 4 Change oil filter 5 C...

Page 13: ...condition 5 Check the movable surfaces travel stops 6 Check the flaperon attachment fittings 7 Wings and wing struts thoroughly check the wing skin for loose rivets corrosion panels deformation and damage inspect the wing leading and trailing edges check all the bolts and safety locks 8 Empennages thoroughly the empennages skin for loose rivets corrosion panels deformation and damage inspect the e...

Page 14: ... AT August 2011 Phone 39 0119927503 Fax 39 0119927266 NOTE in the event of a hit on the wing leading edge it has to be understood they don t reduce the wing structural resistance until they become more than 15 mm long over each 1 m wing span they could slightly affect the in flight aircraft s trimming periodically check for a crack that could arise ...

Page 15: ...0 hours 18 months inspection requires that a 100 hours inspection 25 hours plus the 50 hours adding checks plus the 100 hours adding checks is carried out plus the checks below stated N DESCRIPTION MECH CER ST 1 Check the fuel pipes replace the fuel filter and the gascolator valve gasket 2 Drain and refill the coolant fluid in the cooling system 3 Replace the spark plugs 4 Remove clean and reinsta...

Page 16: ...ility N DESCRIPTION MECH CER ST 1 Replace all tubes of fuel system 2 Replace all tubes of lubrication system 3 Replace all tubes of cooling system 4 Replace the rubber sleeves 5 Replace propeller s bolts and nuts 6 Replace accelerator s cables 7 Replace engine s silent blocks and nuts and bolts 8 Replace rubber band and inferior guides 9 Replace the bearings of three wheels and anterior wheel pin ...

Page 17: ...ation API SG or JASO MA Castrol GPS Cooling liquid Castrol Long Life Coolant Attention use EVANS NPG if showed on the label on the liquid bottle Brake liquid MINERAR BASIS OIL FOR HIDRAULIC USE DO NOT USE SINTETIC OIL TYPE DOT4 Plug NGK DCPR7E Rotax 912 UL NGK DCPR8E Rotax 912 ULS The content of the present manual is the sole property of I C P srl and cannot be reproduced by third parties in any f...

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