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AEROMOT AMT 200S SUPER XIMANGO S Maintenance Manual

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AMT 200S
MAINTENANCE
MANUAL
200-25

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Summary of Contents for AEROMOT AMT 200S SUPER XIMANGO S

  • Page 1 AMT 200S MAINTENANCE MANUAL 200-25...
  • Page 2 MAINTENANCE MANUAL AMT 200S SECTION:1 SECTION 1 - DESCRIPTIONS, SYSTEMS, RIGGINGS AND PLACARDS 1. Motorglider Characteristics Basic Dimensions Wing span 57.32 ft (17.47 m) Wing span with winglets (optional) 57.97 ft (17.67 m) Wing span (wings folded) 33.30 ft (10.15 m) Length 26.50 ft (8.08 m) Maximum height...
  • Page 3 MAINTENANCE MANUAL AMT 200S SECTION:1 Vertical Empennage Vertical empennage surface (area) 22.93 Sqft (2.13m Rudder surface (area) 7.42 Sqft (0.69m Landing Gear Conventional: Two main gears with a tail wheel coupled at the rudder. For ground operation the tail wheel disengages automaticaly when the minimum curve radius is reached. Main landing gear shock absorber: Pressure 130 psi ( 9,14 kg/cm ) >0°C Pressure 145 psi (10,19 kg/cm...
  • Page 4 MAINTENANCE MANUAL AMT 200S SECTION:1 Propeller Hoffmann - model HO-V62R-1/170FA 2 blades, wood core covered with fiber glass Three pitch positions: Minimum pitch, cruise pitch and feathered pitch Change from minimum pitch to cruise pitch - 3800 RPM Change from cruise pitch to minimum pitch - 2200 RPM 1.10 Cockpit - Two places - side by side...
  • Page 5 MAINTENANCE MANUAL AMT 200S SECTION:1 1.12 Air Pressure Ports Dynamic air pressure port Static air pressure port Total energy Page 1.4 MM - 200-25 August 10, 2004 - Rev. 8...
  • Page 6 MAINTENANCE MANUAL AMT 200S SECTION:1 1.13 Vent holes and drains Page 1.5 August 10, 2004 - Rev. 8 MM - 200-25...

  • Page 7: Battery Diagram

    MAINTENANCE MANUAL AMT 200S SECTION:1 2. Electrical Diagram PP1A4 ENGINE RELAY PP17A22 BLACK PP18A22 ENGINE GROUND BATTERY PP1D10 PP3A4N PP1B10 SHUNT PP2A4N PP3B10N MAIN AIRCRAFT END PP4A10 MAIN BUS BUS BAR GROUND PP6A20 MAIN/SOARING PP1C10 MASTER SOARING SOARING PP5A10 SOARING BUS PP8A20N PP7A20 BATTERY DIAGRAM...
  • Page 8 MAINTENANCE MANUAL AMT 200S SECTION:1 STARTER RELAY PP1A4 BLACK PP17A22 PP18A22 BAT TERY MAIN BUS BAR GROUND PP1B10 PP3A4N PP1D10 PP4A10 MAIN PP2A4N SHUNT OIL PRESSURE SWITCH PP14A16 HOUR METER FUSE FIREWALL LINE MASTER E7A22 E6A22 SWITCH PP8A20N PP6A20 PP15A16N E8A22 PP1C10 MAIN BUS...
  • Page 9 MAINTENANCE MANUAL AMT 200S SECTION:1 STARTER LA NDING GEAR BAT TERY ALARM PP1A4 KK1A4 KK5A 22 KK3 A20 KK2A20 MAI N BUS BAR STARTER STARTER KK6A 20N JK3A 18 JK1A1 8 IGNIT ION A MAGNET O A JK2A18 IGNIT ION B JK4A 18 MAGNET O B STARTER AND MAGNETO DIAGRAM...
  • Page 10 MAINTENANCE MANUAL AMT 200S SECTION:1 PP9A10 MAIN BUS ALTERNATOR ALTERNATOR PP10A10 PP13A20 FUSE LINE ALTERNATOR 22.000 uf 22.000 uf PP12A20N ALTERNATOR DIAGRAM (Motorglider s/n 200.128 and on) T&B F1A22 F2A22 TURN BANK F3A22N PILOT T&B F10A22 F11A22 TURN BANK F12A22N COPILOT MAIN BUS BAR F3A22...
  • Page 11 MAINTENANCE MANUAL AMT 200S SECTION:1 T&B F1A22 F2A22 TURN BANK (OPTIONAL) F3A22N PILOT T&B F10A22 F11A22 TURN BANK (OPTIONAL) F12A22N COPILOT F3A22 F4A22 DIREC. GYRO (OPTIONAL) F6A22N PILOT F14A22 F13A22 DIREC GYRO MAIN BUS BAR (OPTIONAL) F15A22N COPILOT F8A22 F7A22 INDICATOR (OPTIONAL) F8A22N...
  • Page 12 MAINTENANCE MANUAL AMT 200S SECTION:1 LEFT GEAR LEFT WING MICRO SWITCH CONNECTOR GW3A22 GW3C22 GW2D22N GW2A22N GW5B22 RIGHT GEAR RIGHT WING MICRO SWITCH CONNECTOR GW1C22 GW1A22 GW2E22N GW5C22 AIR BRAKE MICRO SWITCH GW2B22N GW1B22 GW2C22N GW6A22 GEAR UP MICRO SWITCH GW4A22 GW5A22 GW5D22...
  • Page 13 MAINTENANCE MANUAL AMT 200S SECTION:1 LEFT GEAR LEFT WING MICRO SWITCH CONNECTOR GW3C22 GW3A22 GW2D22N GW2A22N GW5B22 RIGHT GEAR RIGHT WING MICRO SWITCH CONNECTOR GW1C22 GW1A22 GW2E22N GW5C22 AIR BRAKE M ICRO SWITC H GW2B22N GW1B22 GW2C22N GW6A22 GEAR UP M ICRO SWITC H GW4A22 GW5A22...
  • Page 14 MAINTENANCE MANUAL AMT 200S SECTION:1 E2A22 OIL TEMP. SENDER E3A22 OIL PRESSURE OIL TEMP./ SENDER PRESSURE E8A22N E1A22 INDICATOR MAIN E4A22N BATTERY OIL TEMPERATURE / PRESSURE DIAGRAM - Standard configuration OIL TEMPERATURE / PRESSURE AND RPM INDICATION Optional Configuration F1A22 TURN AND BANK (OPTIONAL) F3A22 INTERCOM (OPTIONAL)
  • Page 15 MAINTENANCE MANUAL AMT 200S SECTION:1 Q2A18 Q1A18 Q3A18N FUEL PUMP FUEL PUMP LEFT AUX. POWER PM2A20N PM1A20 AUX. POWER RIGHT AUX. POWER PM2B20N PM2B20 AVIONICS DIAGRAM - Standard configuration Q4A22 FUEL INDICATOR D 15 Q4C22 YELLOW Q5A22 Q5B22 SENDER BLACK Q7B22N Q7E22N FUEL...
  • Page 16 MAINTENANCE MANUAL AMT 200S SECTION:1 3. Ground Connecting Straps STRAP IPC REFERENCE PAGE ITEM IPC FIGURE 05 2.16 2-3-43-66 IPC FIGURE 13 2.44/2.45/2.46/2.47/2.48 18-26-44-90 IPC FIGURE 15 2.58 19-26 IPC FIGURE 16 2.62 3-26-33-60 IPC FIGURE 18 2.68 11-27 IPC FIGURE 20 2.74 Ground Connecting Straps Table Page 1.15...
  • Page 17 MAINTENANCE MANUAL AMT 200S SECTION:1 4. Fuel System Each wing has one aluminum fuel tank located between the leading edge and the main gear wheel well. The tanks are independent and the fuel level is indicated by a fuel quantity transmitter. There is a three-position selector valve to select the tank in use and cut off the fuel.
  • Page 18 MAINTENANCE MANUAL AMT 200S SECTION:1 FIREWALL FUEL RETURNING LINE TO FUEL TANKS CARBURETOR VENT AND DRAIN TUBE Fuel System Page 1.17 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 19 MAINTENANCE MANUAL AMT 200S SECTION:1 5. Brake System Find below the basic components of the brake system. Fluid reservoir Master cylinders Tubes Fittings Flexible tubes Brake cylinder Bleeder valve Only use approved brake fluids: Aeroshell Fluid 41 or Esso HD 400. Measure brake lining thickness (minimum 0.100 inches).
  • Page 20 MAINTENANCE MANUAL AMT 200S SECTION:1 Brake System Page 1.19 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 21 MAINTENANCE MANUAL AMT 200S SECTION:1 6. Aileron Controls Find below basic components of the Aileron Control System Control Stick Aileron rod n° 1 Aileron rod n° 2 Aileron rod n° 3 Aileron rod n° 4 Aileron link rod Inboard and outboard ailerons Bellcrank n°...
  • Page 22 MAINTENANCE MANUAL AMT 200S SECTION:1 6.2.5 Record the neutral position in a table as the example below AILERON (LH) AILERON (RH) ß α (+ 1°) (+ 1°) Neutral Down 6.2.6 Release the control stick by removing tool P/N 27100 D/E-A-28 F1. 6.2.7 Move the control stick to full left and measure the travel on the two ailerons.
  • Page 23 MAINTENANCE MANUAL AMT 200S SECTION:1 6.2.10 If the travel limits measured do not agree with the specified parameters, continue the rigging procedure. 6.2.11 Move the control stick to full left; adjust the up-position of the left aileron by regulating the up-stop screw P/N TH-5x25-RT (ref. IPC fig. 13 D item 51) on left wing and measure the travel on the two ailerons.
  • Page 24 MAINTENANCE MANUAL AMT 200S SECTION:1 Aileron Controls Page 1.23 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 25 MAINTENANCE MANUAL AMT 200S SECTION:1 7. Elevator Control System Find below basic components of elevator control system. Control stick Rod n° 1 Rod n° 2 Rod n° 3 Rod n° 4 Bellcrank n° 1 Bellcrank n° 2 Bellcrank n° 3 Bellcrank n°...
  • Page 26 MAINTENANCE MANUAL AMT 200S SECTION:1 Elevator Control Page 1.25 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 27 MAINTENANCE MANUAL AMT 200S SECTION:1 8. Rudder Control System Find below the basic components of the Rudder Control System Rudder pedals Control cables Rudder bellcrank Rudder Rigging 8.2.1 Inspect the travel to the left and right sides by adjusting the limiting stop screws on each side of the bellcrank arm.
  • Page 28 MAINTENANCE MANUAL AMT 200S SECTION:1 Rudder Control Page 1.27 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 29 MAINTENANCE MANUAL AMT 200S SECTION:1 9 Elevator Trim Control System Basic components of the Trim Control System: Trim control wheel assembly Trim tab wheel indicator Cartridge spring Elevator control rod Cable assembly support Cable Rigging 9.2.1 Verify the elevator travel (up and down) and adjust as necessary. See item 6. 9.2.2 Install tool n°...
  • Page 30 MAINTENANCE MANUAL AMT 200S SECTION:1 Trim Control System Page 1.29 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 31 MAINTENANCE MANUAL AMT 200S SECTION:1 10. Airbrake Control System 10.1 Basic components Airbrake control lever Airbrake control link rod Airbrake angular transmission gear box Airbrake push rod Airbrake torque tube (rod) Airbrake housing 10.2 Rigging Extended: Inspect the correct airbrake extension by adjusting the stop screw at the base of the control lever below the center console.
  • Page 32 MAINTENANCE MANUAL AMT 200S SECTION:1 Airbrake Control System Figure 2 Page 1.31 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 33 MAINTENANCE MANUAL AMT 200S SECTION:1 Figure 2 Airbrake control lever Center console Airbrake control link rod Stop screw Airbrake micro switch 6.38 ± 0.31 in Figure 3 Page 1.32 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 34 MAINTENANCE MANUAL AMT 200S SECTION:1 This page intentionally left blank Page 1.33 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 35 MAINTENANCE MANUAL AMT 200S SECTION:1 11. Main Landing Gear Control System 11.1 Basic components Landing gear control lever Landing gear control rod Landing gear torque tube Landing gear gear box Link rod Control arm Landing gear assy Page 1.34 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 36 MAINTENANCE MANUAL AMT 200S SECTION:1 Main Landing Gear Control System Page 1.35 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 37 MAINTENANCE MANUAL AMT 200S SECTION:1 11.2 Main Landing Gear Rigging 11.2.1 Put the aircraft on jacks 11.2.2 Landing Gear Up-Lock Rigging (See Figure below) Retract the landing gear Adjust the length of the link rod (1) on the rod ends until you obtain an effective landing gear uplock Extend and retract the landing gear several times.
  • Page 38 MAINTENANCE MANUAL AMT 200S SECTION:1 11.3 Landing Gear Down-Lock Rigging (See Figure below) Press the landing gear to the opposite direction of its retraction Adjust the stop screw (6) of the control arm (3) until it aligns with the rod (5) WARNING: MAINTAIN THE LANDING GEAR EXTENDED BY MEANS OF THE FORK BECAUSE THE COMPENSATION SPRING CAN INADVERTENTLY CLOSE THE GEAR.
  • Page 39 MAINTENANCE MANUAL AMT 200S SECTION:1 11.4 Landing Gear Control Lever Rigging - (See figure below) 11.4.1 Do the rigging procedure with the landing gear retracted. Adjust the length of the control link rod (2) so it does not pass the upper dead center as it is shown in the figure below, forming at maximum an angle of 175°...
  • Page 40 MAINTENANCE MANUAL AMT 200S SECTION:1 11.5 Adjusting of Landing Gear and Airbrake Warning Devices (See Figure in the Preceeding Page) Note: Before performing the adjustment, check the correct attachment of the airbrake micro switch. 11.5.1 Retracted landing gear- warning micro switch rigging (a) Extend the airbrakes (b) In the landing gear up and locked position, approach the micro switch to the landing gear control lever until the warning is activated.
  • Page 41 MAINTENANCE MANUAL AMT 200S SECTION:1 11.6.1.3 The lever must show positive sign of locking in the down position (backwards). 11.6.1.4 Make sure that each upper articulated strut does not let the landing gears retract 11.6.1.5 Make sure that all rod lock nuts are tightened and locked. 11.6.2 The warning must sound in the following situations: 11.6.2.1...
  • Page 42 MAINTENANCE MANUAL AMT 200S SECTION:1 ln order to identify the main subassemblies of the motorglider AMT-200S Super Ximango, refer to the table below: Page 1.41 November 23, 2004 - Rev. 9 MM - 200-25...
  • Page 43 MAINTENANCE MANUAL AMT 200S SECTION:1 This page intentionally left blank Page 1.42 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 44 MAINTENANCE MANUAL AMT 200S SECTION: 1 Placards 25-B 30-B 21-A Standard version Optional - Factory Incorporated Only Page 1.43 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 45 MAINTENANCE MANUAL AMT 200S SECTION: 1 Optional - Factory Incorporated Only 30-B 32-B 21-A 45-B Optional - Factory Incorporated Only Page 1.44 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 46 MAINTENANCE MANUAL AMT 200S SECTION: 1 25-E 30-B 32-C Optional - Factory Incorporated Only 25-G 30-B 32-E Optional - Factory Incorporated Only Page 1.45 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 47 MAINTENANCE MANUAL AMT 200S SECTION: 1 30-B 43-A AIR FRAME TIME 21-A 44-A 44-A ENGIN E TIME 32-E 48-A Optional - Factory Incorporated Only 30-B 43-A 21-A 32-E 48-A Optional - Factory Incorporated Only Page 1.46 October 10, 2005 - Rev. 10 MM - 200-25...
  • Page 48 MAINTENANCE MANUAL AMT 200S SECTION: 1 25-I 30-B 32-F Optional - Factory Incorporated Only 2 5 - J 3 0 - B 43-A 3 2 - G 44-A 44-A Optional - Factory Incorporated Only Page 1.47 October 10, 2005 - Rev. 10 MM - 200-25...
  • Page 49 MAINTENANCE MANUAL AMT 200S SECTION: 1 25-K 30-B 32-H 21-A Optional - Factory Incorporated Only 25-L 43-A 30-C 44-A 44-A 48-D 32-I 1 33 Optional - Factory Incorporated Only Page 1.48 July 17, 2007 - Rev. 11 MM - 200-25...

  • Page 50: Section 5 - Maintenance Checks

    MAINTENANCE MANUAL AMT 200S SECTION: 5 SECTION 5 - MAINTENANCE CHECKS 1. External Visual Inspection Inspect the aircraft before every flight to prevent failures or even accidents. 1.1 External Inspection Cabin - Extend the airbrakes. - Make sure that the ignition switch OFF. NOTE We recommend that you do the inspection clockwise from the trailing edge of the left wing root.
  • Page 51 MAINTENANCE MANUAL AMT 200S SECTION: 5 - Make sure that engine cooling openings are clear. - Examine oil level. - Drain fuel filter. For more information, refer to engine and propeller manuals. (4) Right Wing - Do the same procedure used for the left wing except for the pitot tube. (5) Fuselage - Examine the fuselage for the condition.
  • Page 52 MAINTENANCE MANUAL AMT 200S SECTION: 5 - Examine pedals for condition. - Examine rudder cables for condition. - Examine panel instruments for general condition. - Make sure that the airbrakes retract and extend symmetrically and lock correctly. 2. Maintenance Inspection Guideline The inspection procedures are shown on Scheduled Inspection tables.
  • Page 53 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY OPERATIONAL ITEM INSPECTION year NOTE: Before checking oil level, turn propeller over several times to ensure that crankcase oil has been returned to the oil tank.This process finishes when air is returning back to the oil tank and can be noticed by a murmur from the open oil tank.
  • Page 54 Check air brakes for RETRACTED, EXTENDED and intermediate positions. Make sure that the two air brakes move symmetrically. NOTE: If the air brakes do not move symmetrically, contact AEROMOT for more instructions. Page 5.5 August 10, 2004 - Rev. 8 MM - 200-25...
  • Page 55 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY CONTROL CABIN ITEM year Check cables and connections located under control column fairing. Make sure there are spare fuses available. Check the spar attaching pin for deformation, cracks , corrosion and plays. Perform instrument calibration test for the altimeter, speed indicator and vertical speed indicator .
  • Page 56 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY FUSELAGE ITEM year Remove baggage compartment inspection panel. Inspect rear fuselage for condition. Also check the items, as follows: - antennas - cables - rudder control - elevator control rods - bellcranks - ground cables Install baggage compartment inspection panel.
  • Page 57 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY WINGS ITEM year Check wing surface for condition, deformation, corrosion, wear and cracks. Check lights for condition and cracks. Remove access panels on the outboard wings Inspect the pitot tube for condition and security. Make sure it is clear.
  • Page 58 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY WINGS ITEM year Inspect wing fairings for cracks, corrosion and deformation. Operate air brakes. While extending the air brakes, inspect Inspect fuel tank cap gasket for deterioration. Make sure that fuel tank cap vent is clear. Check fuel lines for leaks and wear.
  • Page 59 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY STABILIZER (HORIZ. AND VERT.) ITEM year Remove access panel on vertical stabilizer Inspect surfaces for deformation, wear and cracks. Check elevator vent holes for condition and bstruction. Check flight control travel limits and deflections. Check lights for condition, security and cracks.
  • Page 60 NOTE: If the landing gear legs do not retract symmetrically, there is a malfunction on the angular gear box and you must contact AEROMOT for more instruction. Remove the central console and make sure that the landing gear control handle fits correctly in the EXTENDED and RETRACTED positions.
  • Page 61 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY LANDING GEAR ITEM year Inspect wheels for cracks using a 10x glass. NOTE: In case of hard landing or 500 flight hours, inspect wheels with penetrant. Inspect brake linings and discs for wear, distortion and deformation.
  • Page 62 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY PROPELLER ITEM year Remove spinner Inspect spinner and plate for cracks, deformation and attaching hole wear. Inspect propeller attaching nuts. Torque the nuts to 390-410 in.lb. and apply the torque seal. Use a magnifying glass to check propeller blades for vibration spots, wear and cracks.
  • Page 63 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY POWER PLANT ITEM year Remove engine cowling. Inspect frame 1 and firewall for deformation, cracks, corrosion and security. Check battery gravity and electrolyte level. Clean battery terminals and check electrical wires. Remove battery. Check battery box for acid leakage.
  • Page 64 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY POWER PLANT ITEM year Inspect the expansion tank for damage and abnormalities. Verify coolant level, fill as necessary. Check radiator cap. Inspect rubber plate on expansion tank base for secure fit. Inspect and clean the low level sensor of expansion tank Inspect the overflow bottle for damage and abnormalities.Verify coolant level, replenish as necessary.
  • Page 65 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY POWER PLANT ITEM year Renew gasket ring of drain screw on oil tank.Fit drain screw and tighten to 25 Nm (220 in.lbs.). Refill oil tank with approx. 3 litres of oil. For oil quality refer to Operator's Manual and Service Information ROTAX SI-912-016 / SI-914-019.
  • Page 66 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY POWER PLANT ITEM year Check the exhaust system for corrosion, burns, cracks, leaks and security. Remove the exhaust tube thermal insulator and inspect it for cracks, leaks and distortion. Repair or replace it, as necessary.
  • Page 67 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY ENGINE TEST RUN ITEM year Start the engine and run to operating temperature. Check ignition circuits at 4000 rpm engine speed. Check carburetor preheating. After engine test run, re-tighten the oil filter by hand. Page 5.18 August 10, 2004 - Rev.
  • Page 68 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY LEVELING AND WEIGHING ITEM year 1. Perform weight and balance procedure at the end of the inspection, if necessary. NOTE: If aircraft basic weight is changed due to repair or paint, perform weight and balance procedure after the inspection.
  • Page 69 MAINTENANCE MANUAL AMT 200S SECTION: 5 FIRST EVERY GENERAL ITEM year Make sure that the airplane is clean. Check the aircraft is in accordance with Federal Regulation Authority specifications. Check that all applicable Service Bulletins and Airworthiness Directives have been properly applied. Check that Flight Manual is on board.
  • Page 70 MAINTENANCE MANUAL AMT 200S SECTION: 5 3. Recommended Lubricants Only use the lubricants and fluids approved. In case you use non-approved lubricants, the manufacturer is not responsible for the consequences. 3.1 Main Gear Calibrate the oleo-pneumatic shock struts to 130 psi (9.14 kg/ cm ) at ambient temperatures above 32ºF or 145 psi (10.19 kg/ cm ) at temperatures below 32ºF.
  • Page 71 MAINTENANCE MANUAL AMT 200S SECTION: 5 CLIMATIC MULTI-GRADE OILS ºC ºF CONDITIONS TROPICAL TEMPERATE ARCTIC Lubrication chart ATTENTION: THE AMBIENT GROUND AIR TEMPERATURES LISTED IN THE CHART ABOVE ARE MEANT ONLY AS A GUIDE SPECIFIED BY THE ENGINE MANUFACTURER AND AN INDICATION THAT A HIGHER VISCOSITY OIL SHOULD BE CONSIDERED WHEN THE OIL INLET TEMPERATURE APPROACHES THE MAXIMUM DURING OPERATION.
  • Page 72 MAINTENANCE MANUAL AMT 200S SECTION: 5 4. Recommended Calibration Pressure Main Gear Tires Recommended pressure : 45 ± 1.5 psi (3.2 ± 0.1 Kg/ cm Tail Gear Tire Recommended pressure : 36.2 ± 1,5 psi (2.5 ± 0,1kg/cm 5. Battery The battery GILL G-35 has the following characteristics : 12 V / 35 AH In case you need to recharge the battery, clean the terminals first.
  • Page 73 MAINTENANCE MANUAL AMT 200S SECTION: 5 Corrosion In case you find signs of corrosion, follow procedures from Section 4. Deterioration Replace rubber and plastic components when superficial cracks start. Composite Material Surface Damage Only repair superficial damage (nicks, scratches, etc.). For larger repairs, contact the manufacturer or an authorized workshop to repair the damaged areas.

  • Page 74: Section 6 - General

    MAINTENANCE MANUAL AMT 200S SECTION: 6 SECTION 6 - GENERAL 1. Special Tools Each aircraft is delivered with a special screw driver for the cowling d-zus and a special tool for removing and installing the horizontal stabilizer bolt. 2. Leveling the Motorglider The reference to level the aircraft is obtained with a 19.68 x 0.96 in (500 x 24,5 mm) block or wedge, supported on the extreme rear side of the canopy rail.
  • Page 75 MAINTENANCE MANUAL AMT 200S SECTION: 6 4. Jacking CAUTION BEFORE YOU PUT THE AIRCRAFT ON JACKS, TIE ONE COUNTERWEIGHT TO THE TAIL TO PREVENT THE AIRCRAFT FROM OVERTURNING. Use the jack points located on the lower wing surface near the landing gear to put the aircraft on jacks.