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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. 

Summary of Contents for STORCH CL

Page 1: ...JABIRU 2200 ENGINES 01 20 apr 05 Updated manual M Fiorindo R Ciotti R Ciotti Num Date Description REVISION Preparation Verify Approvation The FlySynthesis s r l it reserves him to terms of law the exc...

Page 2: ...indo 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 Log of revisions All revisions to this M...

Page 3: ...912 UL S 914 UL and Jabiru 2200 version Log of effective pages Page Date 1 Aprile 2005 2 Aprile 2005 3 Aprile 2005 4 Aprile 2005 5 Aprile 2005 6 Aprile 2005 7 Aprile 2005 8 Aprile 2005 9 Aprile 2005 1...

Page 4: ...PRE FLIGHT INSPECTION 7 1 4 DAILY INSPECTION 7 1 5 10 HOURS INSPECTION 9 1 6 20 HOURS INSPECTION 10 1 7 50 HOURS INSPECTION 11 1 8 100 HOURS INSPECTION 13 1 9 150 HOURS INSPECTION 14 1 10 200 HOURS IN...

Page 5: ...testing repair lubrication torque loads and reassembly the operator should refer to the Operator s Manual and Spare Parts List last issues published by engine manufacturer 1 2 MAINTENANCE SCHEDULE Th...

Page 6: ...intenance Table Flight hours totalised New and General Inspection 10h Inspection 20h Inspection 50h Inspection 100h Inspection 150h Inspection Q P O 200h Inspection Q P O 300h Inspection Q P O New X 1...

Page 7: ...ity of attachment 5 Remove the floating chamber from the carburettor and inspect for cleanliness and absence of water 6 Verify the air filter for security of attachment 7 Inspect the ignition cable te...

Page 8: ...es relevant to rotary valve gear lubrication and oil injection systems for Security leaks and chafing 22 Verify the integrity of safety locking wires of gearbox drain and oil level plugs 23 BY pushing...

Page 9: ...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 Re...

Page 10: ...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 Ins...

Page 11: ...oper tension and interference with other equipments Clean and lubricate as necessary On the carburettor verify the RPM and CHOKE operating levers for freedom of movement 6 Check the carburettor for cl...

Page 12: ...upper screw Use 140 cc of oil specified in the paragraph 2 LUBRICATION 13 Check the shock strut piston for abnormal play both transversal and longitudinal play should be 2 3 mm max 078 in 120 in max C...

Page 13: ...equired after 2 years from last filling Apply whichever occurs first For relevant procedure refer to the engine Operator s Manual last issue 9 Check and adjust the preload of knuckle joint spring wash...

Page 14: ...zation Replace if necessary 3 Remove the cylinder heads and cylinders assemblies than proceed as follows Examine the barrel and cylinder heads f or condition and carbon deposits Decarbonise as necessa...

Page 15: ...and replace if necessary 4 ea 3 Check all flexible control cables and replace if necessary 5 ea 4 Check the ailerons hydraulic dampers old models 6 ea 5 Overhaul the stabi1ator hydraulic damper old m...

Page 16: ...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...

Page 17: ...4 7 4 8 use lubricants sparingly providing a preventive cleaning In Table 4 are also Listed the sealing products used sealants should be applied after each removal of concerned parts and or whenever d...

Page 18: ...X X X X X X X X X X X X X X X X X X X 6 Inspect spark plugs for conditions and clean ignition cable terminal X X X X X X X X X X X X X X X X X X X X X X X X X X X X X 7 Check exhaust system for cracks...

Page 19: ...ng nuts X X X X X X X X X X X X X X 14 Torque shock absorber self locking nuts X X X X X X X X X X X X X X 15 Torque cylinder head cowling retaining bolts X X X X X X X X X X X X X X 16 Check oil leve...

Page 20: ...250 260 270 280 290 300 21 Check carburettor for cleanliness and proper adjustment X X X X X 22 Replace exhaust muffler retaining spring X X 23 Replace exhaust muffler buffers X X 24 Replace cartridg...

Page 21: ...70 180 190 200 210 220 230 240 250 260 270 280 290 300 31 Check needle and jet of the carburettor X 32 Check cylinders cylinder heads pistons ring grooves and crank shaft for condition X 33 Check cyli...

Page 22: ...4 ________ x x 3 Check spark plug electrode gap adjust if necessary 0 7 0 8mm 0 028 0 031in x 4 Replace spark plugs type NGK 12 DCPR7E x x 5 Drain oil while engine is warm x x x 6 Check engine and re...

Page 23: ...X X X X X X X X X X X X X X X X X X X X X X 2 Inspect brake control cables for conditions and security X X X X X X X X X X X X X X 3 Inspect push pull control cables for conditions and security X X X...

Page 24: ...locking nuts relevant to the following conditions push pull control cables to stabilator hinge support stabilator hinge pin hydraulic damper to hinge support X X X X X X X X X X X X X X 10 Check self...

Page 25: ...trol stick articulations for security and smooth movement Clean and lubricate as necessary X X X X X 14 Check stabilator supporting plates self locking nuts for tightening X X X X X 15 Check rudder pe...

Page 26: ...210 220 230 240 250 260 270 280 290 300 20 Clean and lubricate the main landing gear leg housing X X X X X 21 Check safety belts self locking nuts for tightening X X 22 Check main landing gear brake l...

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