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Super Ximango AMT 200S, Руководство по эксплуатации самолета

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Содержание AMT 200S

Страница 1: ...AMT200S FLIGHTMANUAL 200 24 PR AMW N S 200 175 N175XS...

Страница 2: ...THE FEDERALAVIATION ADMINISTRATiON THIS MANUAL ISAPPLICABLE TO SUPERXIMANGO MOTORGLIDER AMT 200 S MODEL AMT 200S SERIAL NUMBER 200 175 REGISTRATION PR AMW MANUFACTURER AEROMOT INDUSTRIA MECANICO META...

Страница 3: ...2 12 2 13 2 14 I Introduction 2 1 lndicatedAirspeeds 2 1 Airspeed lndicatorMarkings 2 1 Power Plant Fuel and oillirilitations 2 2 Power Plarit Im trumentMarkings 2 3 Weight Limitations 2 4 Center of...

Страница 4: ...Temperature 3 5 3 8 6 5 High Cylinder Head Temperature 3 6 3 8 6 6 Abnormal Raise ofEngine Speed RPM 3 6 3 8 6 7 Low ethylene glycol level Indication 3 6 SECTION 4 NORMAL PROCEDURES 4 1 Introduction 4...

Страница 5: ...SECTION 6 WEIGHT AND BALANCE 6 1 Introduction 6 l 6 2 Center of Gravity C G Determination 6 1 6 2 1 Weighing 6 1 6 2 2 Arithmetical calculation 6 2 6 2 3 Calculation Table 6 4 6 3 C G Envelope 6 5 6 4...

Страница 6: ...Schedubed Maintenance 8 1 Prior to firstflight of the d 8 1 Ground Handl ing 8 1 8 1 SECTION 7 DESCRIPTION 7 9 Air pressure ports 7 10 Instrument F anel 7 6 7 11 Electrical Circuit 7 7 7 14 SECTION 8...

Страница 7: ...007 October 22 2004 Octbber 22 2004 July 17 2007 July 17 2007 July17 2007 January 29 2001 May 14 2002 October 01 2002 October 22 2004 November2 3 2004 October 10 2005 October 10 2005 March 24 2006 Jul...

Страница 8: ...22 2004 October 22 2004 July 17 2007 October 22 2004 October 22 2004 October 22 2004 October 22 2004 October 22 2004 October 22 2004 October 22 2004 October 22 2004 June 26 2000 October 22 2004 Octobe...

Страница 9: ...ion Placards 14 16 18 36 37 38 and 39 Placards added 40 41 and 42 RevisionOutsid Placard 9 Outside Placards added 12 13 and 14 In flight engine start revised Instrumentpanel drawing added Added of opt...

Страница 10: ...10 Revision Inside Placard 15 2 12 PlaCards added 25B and 25C 2 13 Placard added 30A and 32A I 2 19 Placard ad ded 15 3 3 Revision item 3 7 1 3 6 Item 3 8 6 5revised item 3 8 6 7 added Mar08 2002 6 6...

Страница 11: ...ed 2 2 Item 2 4 revised 7 2 6 Instrument panel drawing revised 1 7 3 5 Item 3 8 6 note added August 22 2002 4 2 Item 4 2 2 revised I 5 2 Item 5 2 4 table revised fO 5 3 Items 5 3 1 and 5 3 3 revised Q...

Страница 12: ...ANUAL PIN 200 24 REASON Text corrections andrevision ofinstrument panel configuration REVISED PAGES 0 1 to 0 6 0 10 1 1 1 5 1 6 2 1to 2 5 2 8 to 2 22 3 1 to 3 6 4 1 to 4 8 5 2 5 3 6 1 to 6 7 7 1 to 7...

Страница 13: ...introduces the Revision n 9 of FLIGHT MANUAL P N200 24 REASON Text corrections and revision of instrumentpanel configuration REVISED PAGES 0 1 0 5 0 6 0 11 0 12 2 9 to 2 22 6 6 7 9 CTAAPPROVAL Date Na...

Страница 14: ...e introduces the Revision n 10 of FLIGHT MANUAL PIN 200 24 REASON Revision of instrument panelconfigurationand instrument panel new configuration drawing added REVISED PAGES 0 1 004 0 5 0 8 0 12 2 9 t...

Страница 15: ...he Revisionn 11 of FLIGHT MANUAL PIN 200 24 REASON Revision of instrument panel configuration and instrument panel new configuration drawing added REVISED PAGES 0 1 0 4 0 5 0 6 0 13 0 14 2 2 2 3 2 10...

Страница 16: ...he Revision n 12 of FLIGHT MANUAL PIN 200 24 REAsON Revision of instrumentpanel configuration arid instrumentpanel new configuration drawing added REVISED PAGES 0 5 0 6 0 14 2 11 to 2 26 6 7 7 11 7 12...

Страница 17: ...PIN 200 24 REASON Adding new model of the Rotax Engine Revisingprocedure oftemperature in the head ofthe cylinder Revising approved equipment list REviSED PAGES 0 5 0 6 0 15 0 16 2 2 2 3 2 24 2 25 3 6...

Страница 18: ...N 200 24 REASON Revision of instrument panel configuration and instrument panelnew configuration drawing added Revising approved equipment list Electrical drcuit added REVISED PAGES 0 1 0 4 0 5 0 6 0...

Страница 19: ...ageis a sandwich type construction with fiber glass epoxy resin and PVCfoam Th e wing isdivided intotwoparts the innerwing isfixed andthe outerwingisfbldable Bothwings have I shaped spars The innerwin...

Страница 20: ...fety harnesses Amdt 22 86 1 eft Oct 22 1986 Protection from injury Amdt 22 86 1 eft Oct22 1986 Electrical bonding Amdt22 86 1 eft Oct 22 1986 Propeller Clearance Amdt 22 85 1 eft Dec 12 1985 Maintenan...

Страница 21: ...ated information which is considered essential to emphasize CAUTION OPERATING PROCEDURES TECHNIQUES AND OTHER RELATED PROCEDURESWHICHMAYRESULTINDAMAGEORDESTRUCTIONOF THEEQUIPMENT IFNOTCAREFULLY FOLLOW...

Страница 22: ...s XIMANGO FLIGHTMANUAL AMT 200S SECTiON 1 1 4 Motorglider Three View Drawing Figure 1 1 I Page 1 4 Effectiveness June 26 2000 I Figure 1 1 AFM 200 24 FAA...

Страница 23: ...nsthevalue read onth13airspeed indicator when corrected for instrumenterror VA Maneuvering speed isthe maximum speed atWhich application offull aerodynamic control will not overstressthe airplane VB D...

Страница 24: ...pty weight of a motorglider is indicated in Section 6 for reference and in the latestweight and balance sheetas calculation data When a motorglideris repaired a new weight and balance sheet should be...

Страница 25: ...peed 2 3 Airspeed Indicator Markings VNE VRA VA VLE VLO 132 knots 245 km h 97 knots 180 km h 97 knots 180 km h 81 knots 150 km h 81 knots 150 km h MARKING VALUE OR RANGE SIGNIFICANCE Green arc 43 97 k...

Страница 26: ...RE BEFORE A NEW START THE STARTER ENGAGED L1GHTWILLREMAIN ON UNTILTHE STARTER RELAY IS REPLACED Fuel Fuel AVGAS Fuel tank capacity Usable capacity Unusablefuel 100 LL Octanes 2 x 11 89 U S Gallons 45...

Страница 27: ...on 2 5 Powerplantlnstrument Markings INSTRUMENT RADIALREDLINE GREENARC YELLOWARC Normal Operation Caution Tachometer maximum 1500 5500 0 1500 5800 RPM 5 min RPM 5500 5800 RPM Oil minimum 120 F 50 C 90...

Страница 28: ...Maximum Baggage weight 2 7 Center of Gravity Figure 2 2 1874 Ib 85 0 kg 11 Ib 5 kg solo 22 Ib 10 kg 2 pilots The reference line DATUM for C G position isthefrontface ofthe fire wall ft 4 25 4 30 4 35...

Страница 29: ...quipm nt 1 Airspeed indicator 1Altimeter 1Vertical speed indicator 1 Slip skid indicator 1 Compass 1Tachometer 1 Oil temperature i1 icator 1 Double fuel level indicator 1 Ammeter 1 Ojlpressure indicat...

Страница 30: ...GRUPO AEROMOT 2 14 Placards FLIGHTMANUAL AMT 200SSECTION 2 25 8 Figure 2 3 Standard version Page 2 6 Appr October 01 2002 c Rev 7 Figure 2 4 Optionar Factory IncorporatedOnIy AFM 200 24 FAA...

Страница 31: ...ANUAL AMT 2005 SECTION 2 4 Figure2 5 Optionaf Factory IncorporatedOnly 1 31 I 32 6 oooo oooo OO ooo0F t OO j 1 5cA Figure2 6 Optional Factory Incorporated Only AFM 200 24 FAA Page 2 7 Appr May 14 2002...

Страница 32: ...S e XIMANGO 24 31 FLIGHTMANUAL AMT 200S SECTION 2 Figure 2 7 Optional Factory Incorporated Only 24 1 3 0 6 1 I r 31 22 Page 2 8 Appr October 22 2004 Rev 8 Figure 2 8 Optional Factory Incorporated Only...

Страница 33: ...200S SECTION 2 o 4 A o Figure 2 9 Optional Factory Incorporated Only l2 J 31 0 0 0000 ffiJ 32 E 0 0 0 0 f r 1 oooo 5 A o 0 0 L _ l Figure 2 1 O Optional Factory In orporated Only Page 2 9 Appr October...

Страница 34: ...UPO AEROMOT _FLIGHT MANUAL AMT 2005 SECTION 2 25 1 24 Figure 2 111 Optional Factory Incorporated Only Figure 2 121 Optional Factory Incorporated Only Page 2 10 Appr October 1 0 2005 Rev 11 AFM 200 24...

Страница 35: ...2 13 Optional Factory Incorporated Orily 24 0 0 0 0 0 0 0 0 0 0 0 0 0 oO dl o O 000 04 A 3 1 0000000000 oC o 00 27 31 1 00000000 32 10 0 0 ff v I 0 C 4 lSc J i 17 D 2 5 6 Figure 2 14 Optional Factury...

Страница 36: ...HING THE ROTATION PUT THE RUDDER IN NEUTRAL APPLY MODERATE LOAD FACTOR TO RECOVER FROM DIVE AND NOT EXCEED VNE EXTEND SPOILERS TO KEEP AIRSPE D B LOW VNE IF NECESSARY Motorgliders sin 200 119 to 200 1...

Страница 37: ...MAXIM JM WEIGHT 18741b Location Hight side ofcanc py support 13 BAGGAGE COMPARTMENT MAX LOAD SOLO FLlGHT 11Ib MAX LOAd 2 CREWMEMBERS 22Ib OXYGEN INCLUDED Location Hight side of baggage compartment 14...

Страница 38: ...PECllON I PC I I DATE I Location Left side of baggage compartment 16 Optional RUDDER PEDALS ADJUSTMENT Slightly push both rudderpedals Pull handle Release to adjust rudder position 17 IPOWERbN 18 OPEN...

Страница 39: ...IS COLD THROTTLE IDLE SWITCH ON THE BATTERY AND MAGNETOS SWITCH ON THE AUXILIARY FUEL PUMP SELECT PROPELLER TO MINIMUM PITCH PUSH START BUTTON SWITCH ON THE ALTERNATOR SWITCH OFF THE AUXILIARY FUEL P...

Страница 40: ...AL TURN AUDiO AUDIO ALTERN _PUMP _ _ GYRO_ _HORJZON BANK_DME _ ADF ON o ON o ON o ON o o o o o 0 0 ON O LlGNn OM sT 3 OFF SILENCE TEST STROBE _ posmOH LAHDING GEAR 25 C Optional Motorgliders sin 200 1...

Страница 41: ..._ lAHDlNG GEAR POSmON_ STROBE INTERCOM BANK _ HORlZOH GYRO _ PUMP _ ALTERN MAGNETO B _ MAGNETO A _ MASTER 25 J Optional Motorgliders sin 200 164 and on 8 ALAR SYSTE I UGHTS JN EQUIP ENT o N O N O N ON...

Страница 42: ...IN OCKED LEFT TRANSIT RIGHT MAIN LANDING GEAR 3D B t E XTENDED RETRACTEp EXTENDEJ LOCKED OR IN LOCKED LEFT TRANSIT RIGHT MAIN LANDING GEAR Motorgliders sin 200 119 200 122 200 123 200 124 200 126 to 2...

Страница 43: ...1TUlT sOC ln lIo I oOro 000 0 tlo ODU _ oJL lUI o 0 0 ALnltltATol _FUSES 32 C Motorgllder sin 200 152 0 0 0 o CO_1 AUDIO CO_2 1f w2 OCERCQ o o o a GPS TOR ENCODER Fun O O 00 ARTFICIAL TURN OIUc nONAL...

Страница 44: ...IWS FUSES 32 G Motorglider sin 200 164 and on o aAo o co n lAY UOlOIO o o o o E l Ut v o nu TO O O O OOA fUELfU S Tl flnII U DDU M S11101 1 o o o o r cllowun OiL fUEL LO UTT HlH J n lllICHOI o o o o...

Страница 45: ...control lever 37 IMICI Location Speaker s plate 38 Optional 1 GPSLimited to VFR use onlyI Location Al50ve any GPS 39 IPHONEI Location Speaker s plate 40 Optional IMIC EMERGENcYI Location Speaker s pla...

Страница 46: ...E 0 ENGINE TIME o o 44 Optional AUX POWER 12V o 1A MAXIMUM 45 Optional 9i COMMUNICATION MIC MIC PHONE _ EMERGENCY Motorgliders sin 200 131 200 132 200 1 4 and 200 135 46 Optional COMMUNICATION PHONE M...

Страница 47: ...FLIGHTMANUAL AMT 2005 SECTION 2 48 Optional DATA 48 0 Optional 48 A Optional DATA 48 8 Optional DATA EFISLH 48 C Optional DATAEFISRH I DATA EMS o DAl AEFtS 50 stAtic 51 f6TAC Y AFM 200 24 FAA Page 2 2...

Страница 48: ...On each main landing gear 2 TAILWHEELTIRE PRESSURE 36 2 psi 2 5kg cm2 Location On tail wheel support 3 4 ENGINE LUBRICANT OIL MOTOR OIL API CLASSIFICATION SG ORHIGHER SEEROTAX51 912 016 51 914 019 CA...

Страница 49: ...from both sides of f iselage cones MAIN LANDING GEAR HYDRAULICOIL AEROSHELL FLUID41 Location Near landing gear filling cap 8 CAUTION PAYATTENTION rN THE DISASSEMBLY OFCOMPRESSED INTERNALSPRING SEE MAI...

Страница 50: ...ELECTRICAL BOX RELAYS AND CAPACITOR Remove the cover to access Location Electrical box cover 14 2A SHUNT 2A SHUNT SA CAPACITOR Location Inside of the electrical box SA CAPACITOR 2A SHUNT 2A SHUNT 10A...

Страница 51: ...AFT US ING BOTH HANDS 3 3 Emergency bail out Shut down the engine magneto off Can0p y jettison Unfasten the seat belt and jump overthewing trailing edge Open the parachute ina safe distance from motor...

Страница 52: ...rspeed below VNE if necessary Note Altitude loss when the rotation stops to the point when the normal flight is re established is between 550 to 750 ft 180to 240 m for one spinturn 3 6 Engine failure...

Страница 53: ...fire Lateral canopy window open Master and alternator switches turn off After the electrical fire stops Remove and check one by one all the fuses to detect the damaged circuit Turn on the masterandal...

Страница 54: ...knots 90 km h Note If there isavailabletime andenough altitude morethan 656ftor200 m andwhen there is no fire it is recommendedto put the propeller in horizontal position bypushing the starterbuttbn N...

Страница 55: ...check oil pressure Cowl flap close If the oil pressure does not decrease reduce engine power to IDLE turn off magnetos and follow Engine Inoperative Landing checklist as item 3 8 1 3 8 6 2 Low oil pr...

Страница 56: ...decreases setpoweraccordingly checkCHTcontinuollsly and land as soon as practical 3 8 6 6 Abnormal raise of engine speed RPM I Reduce engine power to IDLE and turn off magnetos Follow Engine Inoperat...

Страница 57: ...ider 4 2 t Left Wing Fuel tank level check Fueltankcap closed vemt hole clear Airbrakes checkfor proper travel W rlg hinge mechanism Control lever locked and aligned with the red mark fitting of wing...

Страница 58: ...heck Tail wheel tire shock absorber check locking pin installed and cables clearance between tire and fus elage cone normal 2 inches min l inches Note There is no locking pin on motorgliders equipped...

Страница 59: ...button push CAUTION DO NOT OPERATE THESTARTER FOR MORE THAN 10 SECONDS AND NOT MORE THAN 6 CONSECUTIVESTARTS LET THE STARTER COOL FOR 2 MINUTES IFTHESTARTER ENGAGEDLIGHT STAYS ON AFTER ENGINE STARTS T...

Страница 60: ...recommended Due to long wing span caution is recommended during taxi and take off 4 7 Normal Flight 4 7 1 Prior to take off Parking brake set Engine instruments green arc Propeller low pitch Magnetos...

Страница 61: ...TITlJDEIN STANDARD ATMOSPHER 4 7 3Cruise Propeller pitch cruise procedure performed at 3800 RPM by moving the pitch lever approx 30 degrees tothe left and returning to the originatposition Obsenie tha...

Страница 62: ...left position Propeller horizontal position using starter Master switch as required Cowl flap close JIl TURN OFF ALL ELECTRIC EQUIPMENT NOT ESSENTIAL TO FLIGHT 4 7 5 In flight engine st rt Fuel select...

Страница 63: ...se the same procedure as abov except for starter Minimum 203 km h prior to engine start 4 7 7 D scent with Engine running Fuel selector fullest tank Cowl flap close Spoilers as required Trim set Altim...

Страница 64: ...ument panel is used to cancel the aural warning when using spoiler if the landing gear is retracted The system will operate normally when speed brakes are re racted and locked or the landing gear is d...

Страница 65: ...T20QS SECTION 5 125 100 75 50 25 SECTIONS PERFORMANCE Landing gear retracted Spoiler retracted Engine on A c v I r V V Vc Knots AFM 200 24 FAA 25 50 75 75 100 100 125 125 150 150 Page 5 1 Appr Effecti...

Страница 66: ...re at 59 F 15 oC RUNWAY RUNWAY TAKE OFF DISTANCE 738 ft 840ft TAKE OFF DISTANCE DISTANCE rO 49ft 1060 ft 1148 ft TAKE OFF PEED VI 49 knots 49 knots I 5 2 4 Take off distance variation with altitude an...

Страница 67: ...nsumption 4 49 gallon hour 18 5 I h at 97 knots 180 km h engine at 5000 RPM Altitude Sea level 5 3 3 Climb Weight 1874 Ib 850 kg Altitude Sea lev 1 Ambient temp rature 59 F 15 C Initial climb rate 0 t...

Страница 68: ...z ftl min 700 nlln 400 300 2 JD 1 JD o 4 10 5 5 30 20 Vi knom 9 J F f b I a J 3111 f V i l TD J V V 60 at 7 I 1 2 1 I 0 r t l I I i I I J t 0 j II I I I I t I I I I I I j I I I J lag 5 4 Flight polar...

Страница 69: ...quipment 6 2 Determining the cehterof gravity C G The minimum and maximumpilot s weight correspondingtothe centering limits arefound in the weighing sheet of eaclimotorglider without ballast andwith a...

Страница 70: ...ing equation X P2xD P1 P2 d Calculate Balance reading Tare Weight kg Front P1 Rear P2 I Table 6 1 Note Balance precision 0 221b 0 1 kg at least 6 2 2 Arithmetical calculation Use the basicernptyweight...

Страница 71: ...PPEDPILOT 309 140 3 44 1 050 1062 96 147 00 FUEL 143 65 4 07 1 24 582 01 80 60 BAGGAGE 22 10 5 97 1 82 131 34 18 20 TOTAL TOTAL WEIGHT MOMENT 1839 201b 8091 85ft lb 835 kg 1118 14kg m Where X 1118 14...

Страница 72: ...OMENTUM Ib kg ft m ft lo kg m Basicemptyweight Pilot s 3 44 1 050 Baggi lge 5 97 1 82 Full fuel tanks 4 07 1 24 Winglet tips 4 0 1 82 5 02 1 53 Optional equipr nent installed Otherequipment TOTAL Tabl...

Страница 73: ...ked points on axes should be located inside the C G envelope The frontcentering limit is 4 23 ft 1290 mm or31 3 of M A C The rear centering Iimitis 4 5 ft 1372 mm or 39 of M A C up to 14991b 680 kg Fr...

Страница 74: ...RAFrSPRUCE OMII 1 890 TACHOMETER ROTAX 966403 0 716 1 801 BATTERY GILL G35 27 0 0 24 GILL G35S 29 0 0 24 GILL G25 21 0 0 24 POWER SONIC PS 12180 13 0 0 16 FUELLEVELIND DOUBLE WESTACH 2DA 4V O Z43 1 77...

Страница 75: ...EC HORIZ RCA RCA26AK3 4 040 1 650 DIREC GYRO RCA RCA15AK1 4 070 1 650 ELECTRICAL ELEfRIC 1394T100 1 104 1 730 TURN BANK GYRO ELT ANY TSOC9 l 2 200 6 00 AMERI KING AK450 2 000 6 00 ENCODER AMERI KING A...

Страница 76: ...Page 6 8 Effectiveness June 26 2000 s n FLIGHTMANUAL X MANGO AMT200S SECTION 6 This page was intentionallyleftblank...

Страница 77: ...rons Relativewidth Aileron span Aileron surface area 7 2 3 Spoilers Position Spoiler span Type 7 2 4 Horizontal Stabilizer Horiz stabiHzerspan Horiz stabilizersurface area Elevatorsurface Horiz stabil...

Страница 78: ...35 m c 7 3 2 Landing gear operation Landing gear control lever operation FIG A Push down the controlleyer 1 and movebackwardsmoothly 2 the control lever will lift up by spring action FIG B Push the co...

Страница 79: ...ressure through an equalizertube and rigid flexible hosesto a brake caliper disc at each main wheel The brake fluid reservoir is locateo at the firewall engine sidenear the top UH Operation Parking Th...

Страница 80: ...led while keeping the toe brakes fully applied The parking brake is release when the brake handle is pushed Normal Braking For normal braking during taxiing and landing the toe brakes of pilot or copi...

Страница 81: ...imum pitch 2200 RpM 7 6 Fuel system The engine is fed from two fuel tanks located in the wing leading edge box near the fuselage and beside the landing gearwhe L Thefueltanks are independentandtheir l...

Страница 82: ...e ruptured Canopy may notjettison at lowairspeeds butitwill open and you canpush itawayfrom the aircraft 7 8 Seat belts Each seat is equipped with adjustable seatbelts Theyare attached tothe fuselage...

Страница 83: ...N 7 7 10lJlstrument panels 13 00 08 00GO 0888 Standard Note items 9 10 11 30 31 35 and 50 are optionals Double Optional Factory Incorporated Only Note itens 9 10 11 30 31 37 39 40 and 42 are optionals...

Страница 84: ...S u XIMANGO FLIGHT MANUAL AMT 200S SECTION 7 Ri ht Side Optional Factory Incorporated Only 57 23 o o Page 7 8 October 22 2004 Rev 8 Optional Configuration Factory Incorporated Only AFM 200 24 FAA...

Страница 85: ...ANGO AMT200S SECTION 7 20 12 0 60 r c r r 0 0 1 OOOO 0000 58 0 GJ f 13 1 r su 0 I 2 1 110 0 0 14 23 Optional Configuration Factory Incorpbrated Only 0143 oor Q 11l I Optional Configuration Factory Inc...

Страница 86: ...O FLIGHT MANUAL AMT 2005 SECTION 7 44 13 14 0000 0000 12 0000 1 000 0000 000 I I Optional Configuration Factory Incorporated Only Optional Configuration Factory Incorporated Only Page 7 10 July 17 200...

Страница 87: ...ION 7 G 44 ill 8 44 66 66 46 46 45 19 45 23 Optional Configuration Factory Incorporated Only I 0 12 D 000 14 59 25 1 Iiii iiI f 21 19 8 908 r o u U Optional Configuration Factory Incorporated Only AFM...

Страница 88: ...SECTION 7 17 15 16 20 32 33 o a o 0 0 00 0 0 0 21 27 J Lr 28 J 26 G _C JF L 88G ooogg 023 8 1 I 0 0 00 0 00000 um 13 00000000 12 1li5J 1 4 1 0 Optional Configuration Factory Incorporated Only Page 7...

Страница 89: ...ariometer GPS Optional 18 Compass 54 IndicatorVariometer GPS Optional 19 Slip skid 55 Audio Box Optional 20 Test buttons and switches 56 Speaker Optional 21 Throttle 57 Light Dimmer button Optional 22...

Страница 90: ...8A20N MAIN SOARING jMASTER S0 l NG PP7A20 PP1C10 PP5A10 20A SOAR NG BUS BAR BATTERY DIAGRAM Motorgliders sin 200 119 200 122 200 123 200 124 200 126 and 200 127 PPBA20N PP6A20 MAIN SOARING MASTER SOAR...

Страница 91: ...rglider sIn 200 133 and on L _ __ PP1 M _ o STARTER RB AY 41 EMS OlD 18 CHT INDICATOR 22t 1 I P1 CHT SENDER 20t 2 r l CHT RED BlACK STARTER RElAY PP1A4 PPl5Al6N 8AITERY CHARGER PLUG MASTER T M20 N TCH...

Страница 92: ...TION A ETO A JK2A18 I IGNITION B t l MAGNETO B STARTER AND MAGNETO DIAGRAM Motorgliders sin 200 119 200 122 and on G 1 1 G ALTERNATOR B r r P P1 OA 1 0 rc K K3 A2 O i 30An _ l ALTERNATOR c MAIN BUS BA...

Страница 93: ...K F3A22N 2A PILOT F11A22 F10AZi TURN BANK F12A22N 2A COPILOT MAIN Bus BAR DIREC F4A22 FJA22 GO GYRO F6A22N 2A PILOT DIREC F13A22 FHA22 GO GYRO F1 22N 1 2A COPILOT An FBA22 F7A22 INDICATOR FBA22N 2A PI...

Страница 94: ...GRUPO AEROMOT s XIMANGO FLIGHT MANUAL AMT 2005 SECTION 7 Page 7 18 July 17 2007 Rev_ 14 FLIGHT INSTRUMENT DIAGRAM Motorgliders sin 200 133 and on AFM 200 24 FAA...

Страница 95: ...n Q2 4 NC u n u T GW5D22 GW48ZZ GW1E122 IGlfrGEAR l EPI GEAR 5 3 IC oow G V3B22 c 0 0 2A GW12A22 GEAR UGHT SOARING 0 BUS RETRACTED OR Gw11A22H ilS4 GW10A22 INTRAHSIT 1 1 TEST GHIC22 2 11 Pi f AZl STA...

Страница 96: ...G c n U L MCnH S Y s T GEA U E 1IICRCSWlTCII M n U N n 4 I U T n I RIGHT GEAR tHTGEAR M CXJ l oN ICJ 5 3 0 OOW r A U 1 U I N G 0 GENlUGHT B I u I S lHTfW ISIT 1 l w A 2 0 j1rA R 10 N U LOW I N I 12 G...

Страница 97: ...E4AZZN PRESSURE SENDER GND BAT ZA OIL TEMP L J _ _j PRESSURE INDICATOR ZA ENGINE L _ ENDER RPM OIL TEMPERATURE I PRESSURE AND HPM INDICATION Optional Configuration 2A F1A22 TURN AN BANK OPTIONAL 2A F...

Страница 98: ...7E22N BLACK LEFT LEVEL INDICATOR 0015 RED a En a B22 SENDER a7E22N RIGHT FUEL LEVEL DIAGRAM Standard configuration P6 D815 04C22 1 RED 1 21 05C 2 15 Q5A22 Q 5822 YELLOW 2 2 SENDER M Q7822N Q7E22N BLAC...

Страница 99: ...to the engine propeller etc are described in the specific Maintenance Manual for each component I 8 3 8 4 Prior to first fligtltof the day Remove the upperengine cover and Check the airfilter Clean o...

Страница 100: ...GRUPOAEROMOT S XIMANGO FLIGHT MANUAL AMT 2005 SECTION 8 This page intentionally left blank Page 8 2 Effectiveness June 26 2000 AFM 200 24 FM...

Страница 101: ...m t I I i I 18 s Q 2 II f i l J 1 i...

Страница 102: ......

Страница 103: ...lTEC 03 I ReLAY i STANCCR OJ I AMliNNA fI I I c b lAI OO lMl tJAfl clIN I ANTENNA mANS OONOEI KAd l Ayem KING 01 leAnER I G35S l Gill 01 SP EAKER l fELEX rurd 4A IID SuP I QM I IAiRC1 AFl SPRUCE OJ Hi...

Страница 104: ...AEAQNAW AIACRAFTSJN 1 300 61156 _2 Al JoDF RELAt O D SCOMPClNemeS INSTALAOOS fAmJiCF INSTAllEE COfi JiNtS ___ __ __ 06 llli _ _ _ _ _ m 115t 2 w2 IOfAX RELAtoR ODE INSPECAOc iF NAL FiNAL INSPECTIONREP...

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