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AQ 002 Rev.00                                  Issued/Verify/Approval  M. Garofolo        13/july/02

 

Identification:                MM 002 Rev 01
Page:                                           5 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. ROUTINE MAINTENANCE 

1.1  GENERAL 

No other factors are quite important for the 

safety 

and reliability of, the aircraft and its components as a 

regular and diligent attention to the routine maintenance steps carried out within the recommended 
intervals. 
The same applies for a prompt corrective action , introduced for all minor troubles found during the 
aircraft in-service life. 
This chapter contains the maintenance instructions and checks to be performed on the air-frame, 
equipments and engine

.

 

For detailed instructions applicable to the engine and its components (e.g. disassembly, cleaning, 
inspection, 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 

The maintenance schedule for STORCH is based upon 10 inspections to be accomplished within the 
following limits. 
 

PRE--FLIGHT INSPECTION: to be accomplished before each flight. 
DAILY INSPECTION: to be accomplished daily, before beginning the flight

 

activity. 

10-HOURS INSPECTION: to be accomplished after 10 flight hours. 
20-HOURS INSPECTION: to be accomplished after 20 flight hours. 
50-HOURS INSPECTION: to be accomplished after 50 flight hours. 
100-HOURS INSPECTION: to be accomplished after 100 flight hours

.

 

150-HOURS INSPECTION: to be accomplished a after 150 flight hours. 
200-HOURS INSPECTION: to be accomplished after 200 flight hours. 
300-HOURS INSPECTION: to be accomplished after 200 flight hours. 

ANNUAL INSPECTION: to be accomplished once a year independently of flight hours totalised. 

GENERAL OVERHAUL: to be accomplished an airframe and engine at the manufacturer’s facilities after- 
150 flight hours. 

Содержание STORCH CL

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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