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Maintenance Manual DG-808C 

Issued: May 2012 

TN 800/41 

4.3

 

4.4

 

Removal and installation of the undercarriage (main wheel) 

4.4.1

 

General 

Warning:

 A gas strut is installed outside the landing gear box to compensate the 

mass of the landing gear. The landing gear may retract by itself when unlocked 
by the force of the gas strut, especially when the glider is not in the normal 
position. So when working at the landing gear, make sure that inadvertent 
retraction of the landing gear is prevented. 

 

Removal of the gas strut in the landing gear control system:

 Use a screw 

clamp to pre-stress the gas strut sufficiently so that the bolts can be removed. 

4.4.2

 

Removal 

see diagram 15 and 16

 

1. Disassemble and remove the wheel axle. 
2. Remove the wheel brake cable at the brake lever by loosening the attachment 

nipple. 

3. Remove the wheel insuring that the hub locking pin comes free out of the left 

hand front fork.  

4. Rear fork: From inside the undercarriage box remove the three bolts  

M6 (SW 10) that secure parts 6FW3 and 8FW42. After removing the baggage 
compartment floors disassemble pushrod 8FW47 from bellcrank 8FW42. 
Disassemble the gas strut from bellcrank 8FW42.  

5. Front fork: After removing the baggage compartment floors, the axle can be 

unscrewed and the whole thing removed through a 20 mm (.79 in.) dia. hole 
already drilled through the left hand fuselage side. 

4.4.3

 

Installation 

Reverse the above procedures - a new brake cable should be provided - see sect. 
1.5.2 for brake adjustment procedures. 

Note:

 The holes for disassembling des landing gear axles should be closed with 

a sticker. 
 

Содержание DG-800A

Страница 1: ...lugzeugbau de Spare part and material sales Tel 07251 3020 270 lager dg flugzeugbau de http www dg flugzeugbau de M A I N T E N A N C E M A N U A L F O R T H E M O T O R G L I D E R DG 808C Type DG 80...

Страница 2: ...l revision September 2007 3 0 6 8 1 diagram 10 TN800 35 Extension retraction unit rear fork of spindle drive April 2009 4 0 3 0 12 1 3 1 5 1 6 1 8 1 10 1 11 1 14 1 16 1 24 1 27 1 29 1 30 2 1 2 2 2 6 2...

Страница 3: ...Maintenance Manual DG 808C Issued June 2005 0 2 This page was intentionally left blank...

Страница 4: ...0 3 0 4 0 5 0 6 0 7 June 2005 Sept 2007 May 2012 0 8 May 2012 0 9 May 2012 0 10 Sept 2007 May 2012 0 11 May 2012 July 2017 0 12 Sept 2007 May 2012 July 2017 1 1 1 June 2005 1 2 May 2012 1 3 May 2012...

Страница 5: ...12 July 2017 2 3 2 4 2 5 May 2012 2 6 May 2012 2 7 Sept 2007 3 3 1 June 2005 May 2012 3 2 3 3 Sept 2007 May 2012 3 4 May 2012 3 5 Sept 2007 May 2012 3 6 May 2012 3 7 May 2012 July 2017 3 8 May 2012 3...

Страница 6: ...y 2012 4 23 May 2012 4 24 4 25 May 2012 4 26 May 2012 4 27 May 2012 4 28 May 2012 4 29 May 2012 4 30 May 2012 4 31 May 2012 4 32 4 33 July 2017 4 34 4 35 4 36 4 37 4 38 5 5 1 June 2005 May 2012 5 2 Ma...

Страница 7: ...2005 May 2012 valid up to ser No 8 372 11c June 1999 11d April 07 May 2012 valid from ser No 8 373 on 12 June 2005 May 2012 13 Febr 1999 May 2012 13a May 2012 14 Nov 2004 May 2012 14a June 2005 May 20...

Страница 8: ...2 1 3 Rudder control 1 5 1 4 Aileron and wing flap control 1 6 1 5 Airbrake control wheelbrake 1 8 1 6 Undercarriage 1 9 1 7 Tow hooks 1 10 1 8 Water ballast system 1 11 1 9 Massbalance and weights o...

Страница 9: ...system 4 1 4 2 Replacement of control circuit cables 4 2 4 3 Adjustment and servicing of the control circuit 4 2 4 4 Removal and installation of the undercarriage main wheel 4 3 4 4 1 General 4 3 4 4...

Страница 10: ...ation and removal of the extension retraction unit 4 36 4 22 Calibration of the fuel display in the DEI NT 4 37 4 23 Further DEI NT settings 4 37 5 Weight and balance 5 1 6 Instrumentation and accesso...

Страница 11: ...on holes Enclosures 6EP27M Installation Dr ger oxygen system 8EP38 Installation plan ELT ACK 8EP210 wing fuel tank system fuselage side with electromagnetic valves 8M110 Drawing assembly upper drive b...

Страница 12: ...hours Therefore inspections according to section 2 4 of this manual have to be executed at 3000 h 6000 h 9000 h and every 1000 hours following thereafter 0 4 3 Life time of equipment and components U...

Страница 13: ...ipment and components Follow the instructions of the respective manufacturer a Operating Manual for Safety Tow Releases Series Europa G 88 Safety Tow Release latest approved version And if installed O...

Страница 14: ...2 in at wing taper change y 4 5 m Angles of Incidence 1 measured at wing flap setting 5 Horizontal tailplane Angles of Incidence 3 5 chord lines fuselage centre line corresponding to boom slope 1000 3...

Страница 15: ...measured at 134 mm 5 3 in from hinge axis which is directly at the edge of the cut out for the rudder Measurement Hold a measuring stick with one end on the floor Deflect the elevator to neutral posit...

Страница 16: ...its trailing edge Any free play can be reduced by screwing in the adjustment screw on the automatic connector funnel 1 2 5 Trim The automatic trim mechanism should be adjusted according to the sketch...

Страница 17: ...en cable In the event of a replacement Bowden cable being installed it should be emphasised that the cable must pass between the two parallel arms of the Control column mechanism as shown in the sketc...

Страница 18: ...t is 1 5 mm 0 06 inch 1 3 5 Sealing the rudder The rudder is sealed on both sides On the outside with Mylar combi tape and inside the fin with V sealing tapes These sealings are not to be removed If d...

Страница 19: ...fixed part at the wing root with 0 1 mm 0 0 04 in 1 4 3 Stops The aileron stops are located behind the removable left hand side panel The stops can be adjusted at the nuts on the pushrod with two 4 mm...

Страница 20: ...fixed part at the wing root and 4 1 mm 0 16 in against the 18 m wing tip To adjust the flaperons you must first remove the fairings from the control surface horns Then unscrew the horns Allen key wre...

Страница 21: ...ment is at the turnbuckle between main brake cylinder and airbrake control shaft d Adjustment interconnection with wing flap control The airbrake control has to be adjusted so that with the airbrakes...

Страница 22: ...e at the mounting of the rubber buffer A torsion spring is installed to keep the handle in the locked position 1 6 1 3 Free play Free play between lever 8FW42 and the upper strut 8FW40 1 is not allowe...

Страница 23: ...be replaced if it is worn down to a thickness of 4 3 mm 0 17 in 1 7 Tow hooks 1 7 1 Tow release circuit see diagram 5 1 7 2 Adjustment There should be 5 2 mm 2 in 0 08 in space between the tow release...

Страница 24: ...is not successful the valve ball seat should be greased see sect 4 1 b Servicing see section 4 1 1 8 3 Fin tank only version DG 808C Competition The fin ballast tank is constructed as integral tank a...

Страница 25: ...wing parting Flaperon inboard 5 14 3 50 10 37 8 66 0 850 0 710 wing 11 33 7 72 9 00 7 52 1 874 1 566 Flaperon 0 57 0 45 0 693 0 55 0 105 0 083 wing tip 1 26 0 99 0 60 0 48 0 231 0 183 Caution Before a...

Страница 26: ...d attach a distance washer inside diameter 10 5 mm 41 in 0 25 mm 0 01 in thick with a suitable metal adhesive e g Stabilit Express Note the total thickness of the washers at the root rib with a waterp...

Страница 27: ...e electric power from the generator Coolant Commercially available anti freeze for car engines recommended BASF Glysantin G48 Protect Plus concentrate and distilled water With coolant pump type Webast...

Страница 28: ...eccentric propeller shaft see sect 4 12a As an Option a BBSA friction centrifugal clutch may be installed to reduce the drive belt loads when starting the engine The clutch is maintenance free and con...

Страница 29: ...g rubber cord may reduce the wear of the levers and the connecting rod 1 11 10 Tightening torques and locking a All bolts on the engine which are not secured by selflocking nuts should be tightened ac...

Страница 30: ...12 4 Adjusting the powerplant retaining cable Extend the engine via the ignition switch until the extension is switched off by the position switch It should be possible in this position to pull out th...

Страница 31: ...tank can be flushed after removing the drainer The vent outlet of the fuselage tank is at the bottom of the fuselage 1 13 2 2 Wing fuel bags Option In addition fuel bags may be installed in the wings...

Страница 32: ...tes even with the main switch off Via a press button located in the instrument panel the first pump can be switched off with the engine running to check the function of the second pump The excess fuel...

Страница 33: ...an the carburettor you should execute items 1 to 3 Switch on the ignition to clean the carburettor by the electric fuel pump If the carburettor is clean a jet of fuel will spurt out In addition the op...

Страница 34: ...hen screw them out to the noted positions The membrane is to be positioned between the rubber and the metal cover plate Use Loctite 243 to secure the screws of the carburettor cover All measures shoul...

Страница 35: ...n pulses according to the temperature With a hot engine nothing will be injected The DEI NT displays a syringe on the centre display as long as fuel is being injected setting of the primer see section...

Страница 36: ...ies 6V 10 or 12 Ah with screwed terminals The batteries are wired in series and parallel to supply 12V 20 or 24Ah The two 12V packs wired parallel are protected by fuses against discharging each other...

Страница 37: ...d damage disconnect the power plug first when removing the control unit Plug in the power plug after the other plugs when installing the unit Caution When you plug in the connector plugs carefully fix...

Страница 38: ...protection via a re settable fuse in the control unit 1 14 8 12 V Socket The socket is located in the fuselage main bulkhead behind the pilots left shoulder It is used for battery charging main switch...

Страница 39: ...ng The wire gauges are given in the wiring plan 8E250 at the end of the wire No inm or in AWG Shielded wires may be identified by circles at their ends Specification AWG mm MIL W_22759 16 6 WS 6 13 MI...

Страница 40: ...at the connector plug of the lamp 4 Resettable fuses are installed in the DEI NT unit for the following circuits Tankoscillator 0 2A Alarm outlet 2 fuses 0 2A Change over switch when extending the po...

Страница 41: ...stance of 1 8mm 071 in It is absolutely essential to secure the switch with the 4 counter nuts as damage to the switch will stop the RPM measurement and the retraction extension control With a defecti...

Страница 42: ...coolant pump the automatic extension of the engine and the control of the starter motor will be activated b the RPM indicator controls a relay which prevents the starter motor working whilst the engi...

Страница 43: ...2012 TN800 41 1 30 1 15 Pitot and static system 1 15 1 Layout See diagram 6 1 15 2 Maintenance No special maintenance needed 1 16 Ventilation and drain holes 1 16 1 Layout See diagram 171 1 16 2 Main...

Страница 44: ...f the wings see section 1 10 Check the canopy emergency releases according to section 7 16 of the flight manual Only version Classic Check the tension of the lines of the waterbag attachment see secti...

Страница 45: ...nose has touched the ground the nose tow hook Option is to be cleaned and to be checked for correct functioning Hole of the PC port After a landing where the fuselage nose has touched the ground clea...

Страница 46: ...the structure Any white areas around the bushes Outer skins Crushing cracks delaminations Note Hairline cracks from the edges of the airbrake housing are harmless Hairline cracks on the wing leading...

Страница 47: ...cks in the fin top rib fin sparend with tailplane attachment especially around the bushes Rudder mounts Increased free play White areas in the glass fibre bent rudder hinge pin supports Fuselage skin...

Страница 48: ...Undercarriage Check to insure if properly aligned No bent forks Proper extension and retraction Any dirt in the forward fork pivot Any white areas or cracks in the wheel box Remove the baggage area fl...

Страница 49: ...sults of this inspection are positive or if any defects found have been duly repaired the service time of the glider is extended to 9000 hours second step When the glider has reached a service time of...

Страница 50: ...ber 2007 TN800 34 2 7 2 5 Inspection procedure for the controls Check of flaperon and airbrake controls at the wing roots Remove the plastic cap in the rear wing root rib Insert a mirror with approx 3...

Страница 51: ...half year Schwabbel procedure The best method is with an electric power buffer as we do in the factory Also an electric drill may be used Speed approximately 2000 RPM Two packages of special cloth dis...

Страница 52: ...ce protected and must be covered with grease all the time see section 3 3 The other metal parts especially the control stick and all handles should be preserved with metal polishes occasionally 3 2 Ma...

Страница 53: ...undercarriage box Clean and grease all control surfaces hinges Clean and grease the control hook ups for flaperon airbrake and elevator control Clean and grease all pins and bushes of the wing and tai...

Страница 54: ...pair procedures can then be determined Minor damage such as small cracks and holes in the skin surfaces as specified in the repair manual may be self repaired or by a certified repair station Addition...

Страница 55: ...be executed at least 1 year after the last 25 hour inspection preferably with the annual inspection Checklists for this maintenance work are in the enclosures of this manual Please complete the checkl...

Страница 56: ...ain its original size and can be installed without the above mentioned trick 6 Primer a Check the filter of the primer valve The filter is installed in the fuel distributor in which the primer valve i...

Страница 57: ...nting Check the coolant hoses To check the water pump switch on the ignition You should hear a buzz 12 Cylinder and pistons Remove the exhaust manifold For the lower bolts a shortened wrench is needed...

Страница 58: ...ck the spring pressure at the coupling of exhaust manifold to muffler To accomplish this measure the distance between the brackets for the spring couplings at the muffler pipe and at the movable part...

Страница 59: ...drive belt tension according to section 4 12 item g Check the 6 rollers 8M171 which guide the drive belt for tight fit to their mounting brackets and for easy turning If there is any significant fric...

Страница 60: ...reakers 30 Reinstall the engine bay doors Check all the hinges on the engine compartment doors for proper fit and any cracks tears etc Check if hinge pins are secured properly Ground test run Warning...

Страница 61: ...rcraft engine maintenance workshop approved by the manufacturer and by the authorities 2 Replace all the nuts and bolts on the engine 3 Replace the drive belt 4 Replace the bearings of the upper drive...

Страница 62: ...at the parting of the tank has to be taken out and to be installed in the new tank Clean and test the check valve for proper function prior to reinstallation When you turn the valve so that the sprin...

Страница 63: ...to aircraft inspection and repair FAA AC 43 13 1 B or later issues Caution Control cables according to MIL W 83420 I A was MIL W 1511A or ISO 2020 was LN 9374 should be used Note For the electric prop...

Страница 64: ...emble and remove the wheel axle 2 Remove the wheel brake cable at the brake lever by loosening the attachment nipple 3 Remove the wheel insuring that the hub locking pin comes free out of the left han...

Страница 65: ...the landing gear fix left wheel door in the fully open position set the airbrake control in the retracted position remove the baggage compartment floor and rear cover Remove the reservoir mounting pla...

Страница 66: ...lcohol don t use fuel or solvents 3 Check brake pressure extend the airbrakes there must be a strong pressure when the wheel brake engages check several times the wheel brake must engage at the same p...

Страница 67: ...10 mm 3 8 in 2 mm 1 12 in thick with double sided tape at the rear end of the hinge see sketch Put on the canopy and try to lock the canopy to the hinge If this is not possible remove a small amount o...

Страница 68: ...at the flaperons Then screw away the horns Allen key wrench 4 mm 0 16 in 3 Remove the selflocking nut and the washer at the inboard flaperon hinge Socket key wrench 8 mm 0 32 in move the flaperon from...

Страница 69: ...the outboard flaperon drive and curved seals from the outboard flaperon drive up to the outboard end 4 7 2 Wing lower surface turbulators a Version with combi tape Sealing and turbulator are combined...

Страница 70: ...surface with 38 mm Teflon glass fabric tape a Removing the flaperons To remove the flaperons you have to remove the internal sealing first Peel off carefully so that the tape does not tear and no rema...

Страница 71: ...e accordingly with the next sections Then deflect the aileron several times in both directions If there is still a noise which sounds like the fabric sticking to the aileron and getting loose again yo...

Страница 72: ...Don t glue the film tape to the leading edge of the seal The scarfed leading edge of the seals must be pressed to the stabilizer surface by a PVC tape Prior to removing the sealing mark the leading e...

Страница 73: ...o be in line A max tolerance of 0 5 mm 0 02 in in up and down and fore and aft direction is allowed Fix the holders to the bench when in line Install the flaperon again and measure the load at the tra...

Страница 74: ...reinstallation you have to clean the thread of the bolt and the inside thread from any remains of Loctite For this procedure use Acetone If necessary re cut the inside thread Before you apply the Loc...

Страница 75: ...perlon cords at their attachment at the root rib Attach an extension line 3 mm diameter 1 8 in 5 m long to the red line Remove the fuel tank by pulling on the perlon cord marked red and black on the f...

Страница 76: ...bly applying a 22 mm open end spanner at the fork 8M119 until the next mounting hole in the flange of axis 8M115 appears Therefore press the pulley in upward direction at its front end Rotation in clo...

Страница 77: ...to secure all screws and bolts except for the propeller mounting bolts Caution When reassembling the drive belt covers be careful to use the correct screws Screws which are too long will damage the be...

Страница 78: ...e belt surface and the outer side of the propellermount at the same station from the left hand side through the opposite thread with the probe of a vernier caliper First measure with no load on W57 an...

Страница 79: ...ngs from the pulley you have to produce 2 pieces of round material each 100 mm 4 in long and with 47 mm 1 85 in and with 53 mm 2 09 in diameter 10 Press out the outer rings together with the Nilos rin...

Страница 80: ...ctite 243 Fix the first nut with a hook spanner so that the adjustment doesn t change and tighten the second nut as far as possible Check again the rotation of the pulley No free play is allowable 9 P...

Страница 81: ...two holes diameter 8 mm 32 in 80 mm 3 15 in apart Bolt this plate to gas strut and propellermount and retract the engine to extend the gas strut far enough to place the halfshells Remove the plate d...

Страница 82: ...ad and pull it out of the access hole An absorber element is installed on the adjustment screw Check if the washer at the rear end of the absorber is in place and fixed and if the absorber element is...

Страница 83: ...the radiator upper end Insert the test adapter W59 drawing see enclosure to this MM into the hose and secure with a hose clamp Install a PVC hose instrument line on the other end of the adapter and p...

Страница 84: ...handling Fill in coolant until the radiator is completely filled 3 Switch on the ignition to run the coolant pump Look into the radiator you must see the coolant bubbling If this is not the case there...

Страница 85: ...olts secured with Loctite with a hot air gun to enable easy removal Respect the notes for engine conservation see engine manual prior to removal of the engine To lift out the powerplant from the engin...

Страница 86: ...move hose clamp which fixes the electric wiring of the starter at the engine block Remove the pole insulating cap from the positive terminal then remove the electric wiring from the starter motor with...

Страница 87: ...move some further Ty raps 11 Separation of the extension retraction unit from the propeller mount a Disconnection of gas strut from the powerplant s section 4 14 b Spindle drive Retract powerplant unt...

Страница 88: ...N 912 10 9 1 sharp knife 1 roll insulating tape 1 bucket 1 Remove the drive belt fairings from the propeller mount by unscrewing the 16 bolts with a 3 mm Allen key wrench 2 Remove the drive belt accor...

Страница 89: ...section 4 16 2 Use a bucket to catch the coolant approx 2 litres 10 Remove the spark plug connectors from all spark plugs 11 Remove coolant outlet on top of the engine from the cylinder heads using a...

Страница 90: ...rhaul 17 Spark plugs Unscrew spark plugs with an 21 mm 13 16 socket wrench Seal the cylinder holes with tape 18 Exhaust manifold The exhaust manifold can be removed by unscrewing the four bolts at the...

Страница 91: ...the proximity switch and check its adjustment according to sect 1 14 15 and correct if necessary 5 Reconnect spindle drive and gas strut 6 Rig the wings to the fuselage and secure the glider Start th...

Страница 92: ...ing using small pliers Unhook the spring Pull the spring pins out of the hinge pins Remove the hinge pins Retract the engine until just before the engine doors close Move the left engine door far enou...

Страница 93: ...which runs through the hole b Twist both ends of the wire clockwise up to the other bolthead Slide the upper wire through the hole in the bolthead and bend the other wire around the head Twist with ma...

Страница 94: ...r with each other when the ignition switch is in on position For checking gain access to the connector plugs at the ignition electronic boxes by removing Ty raps and heatshrink tubing Check the resist...

Страница 95: ...neto housing with a gauge The gap must be 0 45 0 55 mm 0 018in 0 022in wide c Checking the generator coil Disconnect the engine main plug and measure the resistance between wires 491 and 501 It should...

Страница 96: ...n be discovered the control unit must be replaced b If the generator is overcharging the batteries Check all terminals at the control unit If no defect can be discovered the control unit must be repla...

Страница 97: ...s First don t tighten the bolt which connects the spindle drive to its front mounting block Extend the powerplant to the position see sketch Then tighten the bolt The reason for this procedure is to m...

Страница 98: ...TANK CALIB ration Calibration of the fuel gauge with empty tank Push the selector knob N will be displayed rotate the selector knob Y will be displayed Push the selector knob to execute the calibratio...

Страница 99: ...Activation or deactivation of the warning message Adjustment similar to Prop Brake Note You may deactivate this warning in case no watertanks are installed When deactivated the OAT screen will still b...

Страница 100: ...xt page Caution The distances a and b may change with different masses due to deflection of the landing gear Note The total mass M may be determined by weighing and adding W1 and W2 or by weighing and...

Страница 101: ...as Standard Category must have the weight and balance carried out by a licensed Airframe Mechanic Empty weight C G range is determined by reference to the diagram in sect 6 8 7 of the flight manual If...

Страница 102: ...icated in the flight manual section 2 3 Altimeter Manufacturer Type Certification No Winter 4 FGH 10 diam 80mm TS 10 220 46 1 000 10 000m Ident No 4110 1 000 20 000ft Ident No 4320 Winter 4 FGH 20 dia...

Страница 103: ...03JTSO Becker AR 3201 1 10 911 76 AR 2008 25 A 10 911 48 AR 4201 JTSO 2C37 D ED 23A AR 6201 EASA 210 1249 Filser Funkwerk ATR 720 A 10 911 74 ATR 720 C 10 911 83 ATR 600 LBA 0 10 911 106JTSO ATR 500 L...

Страница 104: ...ents and other equipment may be installed if they do not in themselves or by their effect upon the sailplane constitute a hazard to safe operation TN DG G 07 must be regarded Caution If additional ins...

Страница 105: ...he bearings of the upper drive belt pulley F Two steel rods dia 4 mm 5 32 in appr 70 mm 3 in long aileron control stops G Spring balance max reading 50 N 11 lbs H Nicopress tool 64 CGMP I Hose connect...

Страница 106: ...the wing tanks Hose with outside diameter 25 mm 1 in appr 2 m 6 56 ft long P To fill the fintank Z27 Funnel with clear PVC hose inner diameter 12 mm 47 in 1 7 m 5 ft long and hose connector GS12 Q Tes...

Страница 107: ...k plug connector PVL 401222 5k alternative to Bosch 60500127 Nut for spring coupling M 8 for exhaust muffler 60500128 Spring for spring coupling M 8 60502500 Starter motor DENSO 128 000 1671 12 V 6050...

Страница 108: ...Sealing ring for drainer CAV 110 for automotive fuel 60507561 Electric fuel pump Facet 40106 60507558 Refuelling pump KAVAN 12 V up to ser no 8 372 60507562 Refuelling pump Facet 60106 from ser no 8 3...

Страница 109: ...1908KA Master switch 60510370 Press button SECME 07 17801 21 for starter up to ser no 8 344 60510372 Press button DJET 07 17502 21 for starter from ser no 8 345 also used as push to talk switch 60510...

Страница 110: ...d 10m roll dimple turbulator tape 70000229 Tesafilm 4104 white 19 mm wide 66 m roll PVC tape 3 Flaperons sliding surface and internal sealing 30003136 Teflon glass fabric 0 08 x 38 mm 33 m roll selfad...

Страница 111: ...ll find a similar list in your aircraft logs Parts of the min equipment are to be chosen from sect 6 of the maintenance manual Subject type mass kg arms mm date of installation date of removal Airspee...

Страница 112: ...ce manual h 25 50 75 100 125 150 175 200 225 250 275 300 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 executed by place date engine hrs signature Eac...

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Страница 120: ...euvering V A 190 103 Rough air 190 103 Max flap extended speed 8 5 190 103 Landing gear operating 190 103 Maximum speed V NE 270 146 Max flap extended speed L 150 81 Powerplant extended 190 103 Powerp...

Страница 121: ...km h kts Winch launch 150 81 Aero tow 190 103 Manoeuvering V A 190 103 Rough air 190 103 Max flap extended speed 8 5 190 103 Landing gear operating 190 103 Maximum speed V NE 270 146 Max flap extende...

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Страница 146: ...Anschluss ext Benzin 47 46 external fuelpump connector Trennstelle ca 47cm vom Benzinpumpenanschlu 201 0 4 L 30cm 202 0 4 L 30cm Fl geltankumschalter c b a wing tank selector switch 0 4 L 52cm 0 4 L...

Страница 147: ......

Страница 148: ...s 1 Zweitanzeige Benzinpumpe Tankpumpe Tankpumpenstecker Hauptschalter Servo1 2 Servo1 1 Batteriespannung Ladestecker Hauptstromschiene Batterie 2x40 SpindMot 1 20 SpindMot 2 20 Anlasser GND 40 GEN 1...

Страница 149: ...DEI Z Kreis 1 Zweitanzeige Benzinpumpe Tankpumpe Tankpumpenstecker Hauptschalter Servo1 2 Servo1 1 Batteriespannung Ladestecker Hauptstromschiene Batterie 2x40 SpindMot 1 20 SpindMot 2 20 Anlasser GND...

Страница 150: ...QJ GLDJUDP RQWURO 5HFWLILHU 5HJXODWRU 5HIXHO 3XPS RQWURO 1 A B 35 3A 1 QWHUIDFH 1 LQWHUIDFH 3RZHU VXSSO PTC XVHODJH 7DQN 7DQN DSDFLWRU 7DQNRV LOODWRU 3URSHOOHU UDNH 6HULDO 3RUW DFNXS XHO 3XPS 0 2A DWH...

Страница 151: ...JXODWRU 5HIXHO 3XPS RQWURO 1 35 3A 1 QWHUIDFH 1 LQWHUIDFH 3RZHU VXSSO E R R Q R I I PTC XVHODJH 7DQN 7DQN DSDFLWRU 7DQNRV LOODWRU 3URSHOOHU UDNH 6HULDO 3RUW DFNXS XHO 3XPS 0 2A DWHU 3XPS 7 3UREHV XPSV...

Страница 152: ...on COM1 f select config and configure the serial data 9600 baud 8 data bits parity no 1 stop bit flow control XON XOFF or none g save changes File Save h select transfer capture text i enter a new fil...

Страница 153: ...are from left to right Flight data date TT MM JJ takeoff time HH MM landing time HH MM flight duration HH MM engine operating time HH MM Max engine speed of this flight RPM Operating time engine speed...

Страница 154: ...warning acknowledge Y N EGT sensor failure warning acknowledge Y N OAT sensor failure warning acknowledge Y N Communication failure with control unit acknowledge Y N Proximity switch failure acknowled...

Страница 155: ...es for aerial installation and wire feed through installation of the aerial To drill the holes for the aerial installation it is necessary to position the drilling template supplied with the aerial le...

Страница 156: ...y compartment From there on the cable has to be pushed through underneath the seat towards the compartment where the C G tow release is mounted Underneath the oxygen bottle tube a recess in the front...

Страница 157: ...er with separate control unit the control unit may be installed in the right hand cockpit side panel Connect the HF Connector to the transponder Power supply takes place through wires 14 and 04 includ...

Страница 158: ......

Страница 159: ...den Triebwerken SOLO 2 625 01 und SOLO 2 625 02 daher die betroffenen Teile zu kontrollieren und je nach Zustand auszutauschen Um den Zustand der Rutschkupplung bei allen Triebwerken der Baureihe SOL...

Страница 160: ...ng zum Hersteller gesendet werden Alle 50 h 2 625 01 2 625 02 Ausbau der Rutschkupplung zur Grund berholung beim Hersteller Actions Inspection of the slip clutch and replacement of the cover plate wit...

Страница 161: ...on einer sachkundigen Person durchgef hrt werden und ist im Bordbuch des Luftfahrzeuges einzutragen Ein evtl Ein oder Ausbau der Kupplung oder von Teilen der Kupplung muss von einem LTB durchgef hrt w...

Страница 162: ...el 49 7031 301210 Fax 49 7031 301136 Anschlagscheiben werden an unsere Vertretungen in Australien S dafrika und Argentinien gesendet Andere L nder werden von Deutschland aus beliefert Orders fort the...

Страница 163: ...intenance Manual DG 800B DG 808C and DG 500MB section 1 11 4 If the drive belt jumped the problem may be easily corrected with an approx 30mm wide by 100mm long piece of Mylar tape If the distance is...

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