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czech sport aircraft 08SC142, Pilot Operating Handbook

The Czech Sport Aircraft 08SC142 Pilot Operating Handbook is a comprehensive manual that provides essential information for operating this aircraft model. Users can download this manual for free from manualshive.com to ensure they have all the necessary information for a safe and efficient flight experience.

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SC-POH-1-1-17

 

Revision: - 

Date of issue: 2011-09-01

 

 

 

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Pilot’s Operating Handbook

 

 
 
 
 
 

 

 
 
 
 
 

 

 

 

Airplane Registration Number:

  N4465F

 Airplane Serial Number: 08SC142

 

Summary of Contents for 08SC142

Page 1: ...1 17 Revision Date of issue 2011 09 01 S Sp po or rt tC Cr ru ui is se er r i S Sp po or rt tC Cr ru ui is se er r Pilot s Operating Handbook Airplane Registration Number N4465F Airplane Serial Number...

Page 2: ...SC POH 1 1 17 Revision Date of issue 2011 09 01 S Sp po or rt tC Cr ru ui is se er r ii Intentionally left blank...

Page 3: ...e er r a ai ir rc cr ra af ft t i is s d de es si ig gn ne ed d a an nd d m ma an nu uf fa ac ct tu ur re ed d b by y Czech sport aircraft a s Na Z honech 1177 212 686 04 Kunovice Czech Republic Websi...

Page 4: ...SC POH 1 1 17 Revision Date of issue 2011 09 01 S Sp po or rt tC Cr ru ui is se er r iv Intentionally left blank...

Page 5: ...SC POH 1 1 17 Revision Date of issue 2011 09 01 RECORD OF REVISIONS S Sp po or rt tC Cr ru ui is se er r v RECORD OF REVISIONS No Affected pages Revision name Date of Issue Signature...

Page 6: ...SC POH 1 1 17 Revision Date of issue 2011 09 01 S Sp po or rt tC Cr ru ui is se er r vi Intentionally left blank...

Page 7: ...vii LIST OF EFFECTIVE PAGES Section Page Revision No Section Page Revision No i 2 2 8 ii 2 9 iii 2 10 iv 2 11 v 2 12 vi vii 3 3 1 viii 3 2 ix 3 3 x 3 4 xi 3 5 xii 3 6 xiii 3 7 xiv 3 8 xv 3 9 xvi 3 10...

Page 8: ...r viii LIST OF EFFECTIVE PAGES Cont d Section Page Revision No Section Page Revision No 4 8 6 9 4 9 6 10 4 10 6 11 4 11 6 12 4 12 6 13 6 14 6 15 5 5 1 6 16 5 2 5 3 7 7 1 5 4 7 2 5 5 7 3 5 6 7 4 5 7 7...

Page 9: ...t 1 ft 12 in 0 305 m 305 mm fpm Vertical speed in feet per minute 1 fpm 0 0051 m s GPS Global Positioning System hp Power unit 1 hp 0 7457 kW IAS Indicated Airspeed IC Intercom IFR Instrument Flight R...

Page 10: ...Pressure unit pound per square inch 1 psi 0 0689bar rpm Revolutions per minute s or sec Second SM Statute Mile 1 SM 1 609 m TAS True Airspeed US gal US gallon 1 US gal 0 83 UK gal 3 785 L V Volt VFR...

Page 11: ...STM LSA standards ASTM F 2245 09 Standard Specification for Design and performance of a Light Sport Airplane ASTM F 2279 06 Standard Practice for Quality Assurance in Manufacture of Fixed Wing Light S...

Page 12: ...SC POH 1 1 17 Revision Date of issue 2011 09 01 S Sp po or rt tC Cr ru ui is se er r xii Intentionally left blank...

Page 13: ...N S Sp po or rt tC Cr ru ui is se er r xiii CONTACT INFORMATION Czech Sport Aircraft a s Na Z honech 1177 212 686 04 Kunovice Czech Republic Website www czechsportaircraft com E mail office czechsport...

Page 14: ...SC POH 1 1 17 Revision Date of issue 2011 09 01 S Sp po or rt tC Cr ru ui is se er r xiv Intentionally left blank...

Page 15: ...CONTENTS S Sp po or rt tC Cr ru ui is se er r xv TABLE OF CONTENTS 1 General Information 2 Limitations 3 Emergency Procedures 4 Normal Procedures 5 Performance 6 Weight and Balance 7 Description of Ai...

Page 16: ...SC POH 1 1 17 Revision Date of issue 2011 09 01 S Sp po or rt tC Cr ru ui is se er r xvi Intentionally left blank...

Page 17: ...vision Date of issue 2011 09 01 SECTION 1 GENERAL INFORMATION S Sp po or rt tC Cr ru ui is se er r 1 1 SECTION 1 TABLE OF CONTENTS 1 GENERAL INFORMATION 1 1 Airplane specification 1 2 1 2 Summary of p...

Page 18: ...and notes in the POH WARNING Means that the non observation of the corresponding procedure leads to an immediate or important degradation of the flight safety i e to injury or death of persons CAUTIO...

Page 19: ...SC POH 1 1 17 Revision Date of issue 2011 09 01 SECTION 1 GENERAL INFORMATION S Sp po or rt tC Cr ru ui is se er r 1 3 S Sp po or rt tC Cr ru ui is se er r aircraft layout...

Page 20: ...Airframe All metal construction stressed skin single curvature metal skins riveted to stiffeners Construction is of 6061 T6 aluminum sheet metal riveted to aluminum angles with Avex rivets This high...

Page 21: ...ndurance 5 25 h mm Conditions Usable fuel 29 85 US gal 75 power of engine 5 000 RPM Altitude 3 000 ft Reserve 30 minutes Empty weight minimum equipment 842 3 lb Revision Date of issue 2011 09 01 1 5 1...

Page 22: ...m Best angle of climb speed vx 56 KIAS Best rate of climb speed vy 62 KIAS Stall speeds VS0 flaps down power idle 31 KIAS VS1 flaps up power idle 37 KIAS Fuel Total fuel quantity 30 12 US gal Total us...

Page 23: ...Flap extended speed range 2 3 2 4 Maneuvering speed 2 3 2 5 Maximum structural cruising speed 2 3 2 6 Never exceed speed 2 3 2 7 Service ceiling 2 3 2 8 Load factors 2 3 2 9 Approved manoeuvres 2 3 2...

Page 24: ...range Significance KIAS White arc 31 75 Flap Operating Range Green arc 38 108 Normal Operating Range Yellow arc 108 138 Maneuvers must be conducted with caution and only in smooth air Red line 138 Ma...

Page 25: ...speed at 1 320 lb 88 KIAS Manoeuvring speed at 900 lb 70 KIAS 2 5 Maximum structural cruising speed VNO Maximum structural cruising speed 108 KIAS 2 6 Never exceed speed VNE Never exceed speed 138 KIA...

Page 26: ...lb Max weight of fuel 180 lb Max baggage weight in rear fuselage 40 lb Max baggage weight in each wing locker 22 lb Empty weight minimum equipment 760 lb NOTE Actual empty weight is shown in Section 9...

Page 27: ...Rotax Service Instruction SI 912 016 MOGAS European standard min RON 95 EN 228 Super EN 228 Super plus US standard ASTM D4814 Canadian standard min AKI 91 CAN CGSB 3 5 Quality 3 CAUTION Fuels that co...

Page 28: ...0 rpm Cruising 75 68 4 hp at 5 000 rpm Engine RPM Max takeoff 5 800 rpm max 5 min Max continuous 5 500 rpm Cruising 75 5 000 rpm Idling 1 400 rpm minimum Oil pressure Minimum 12 psi below 3 500 rpm Ma...

Page 29: ...400 1 400 5 500 5 500 5 800 5 800 Oil Pressure 12 psi 12 29 psi 29 73 psi 73 102 psi 102 psi Oil Temperature 122 F 122 194 F 194 230 F 230 266 F 266 F Cylinder Head Temperature CHT 122 275 F 275 F Fue...

Page 30: ...d temperature indicator x Safety harness for every used seat x Additional instruments and equipment list for Night VFR flights x Attitude indicator x Instrument lights x Position lights x Anti collisi...

Page 31: ...31 kts WARNING DO NOT EXCEED MAXIMUM TAKEOFF WEIGHT 600kg 1320lbs WARNING IFR FLIGHTS AND INTENTIONAL FLIGHTS UNDER ICING CONDITIONS ARE PROHIBITED APPROVED FOR DAY NIGHT VFR FOR AVIATION EMERGENCY U...

Page 32: ...IDLE OFF CHOKE ON PILOT HEADSET MUSIC IN COPILOT HEADSET 0 12 30 BUZZER ELT CONTROL COCKPIT L INSTR L 12V EFIS EMS ALERTS VOLUME PEDAL SETTING PEDAL SETTING OFF ON OFF ON FLAPS DOWN FLAPS UP 18 1 psi...

Page 33: ...issue 2011 09 01 SECTION 2 LIMITATIONS S Sp po or rt tC Cr ru ui is se er r 2 11 FUEL DRAIN AEROSHELL OIL SPORT PLUS 4 CANOPY OPENED CANOPY CLOSED FUEL CAPACITY 57 Litres 15 US Gal MOGAS RON 95 AKI 9...

Page 34: ...C Cr ru ui is se er r 2 12 If BRS rescue system is installed CAUTION The owner operator of this airplane is responsible for the readability of placards during the aircraft service life located on the...

Page 35: ...ngine starting 3 5 3 7 Loss of oil pressure 3 5 3 8 High oil pressure 3 5 3 9 Emergency landing without engine power 3 6 3 10 Precautionary landing with engine power 3 6 3 11 Engine fire during start...

Page 36: ...09 01 SECTION 3 EMERGENCY PROCEDURES S Sp po or rt tC Cr ru ui is se er r 3 2 3 23 Loss of primary instruments 3 11 3 24 Loss of flight controls 3 12 3 25 Power lever linkage failure 3 12 3 26 Inadve...

Page 37: ...nsidered and applied as necessary to correct the problem CAUTION Airspeeds values are valid for standard AVIATIK WA037383 pitot static probe These emergency procedures are valid for WOODCOMP KLASSIC 1...

Page 38: ...e landing 7 Land straight ahead turning only to avoid obstacles NOTE Altitude loss during 180q turn is approximately 400 ft 3 5 Loss of engine power in flight 1 Airspeed maintain 60 KIAS 2 Altitude in...

Page 39: ...Other switches ON as necessary 3 7 Loss of oil pressure 1 Oil temperature check If oil temperature is rising 2 THROTTLE reduce power to minimum for flight 3 Land as soon as possible CAUTION Be prepare...

Page 40: ...with engine power A precautionary landing is generally carried out in the cases where the pilot may be disorientated the aircraft has no fuel reserve or possibly in bad weather conditions 1 Choose lan...

Page 41: ...y yourself or call for a fire brigade if you cannot do it 3 12 Engine fire in flight 1 FUEL selector OFF 2 THROTTLE MAX 3 CABIN HEATER PUSH OFF 4 Ignition Switch OFF after the fuel in carburetors is c...

Page 42: ...LE 2 Airspeed max permitted VNE 138 KIAS VNO 108 KIAS VA 88 KIAS 3 Engine RPM do not overrun max 5 800 rpm 3 15 Generator failure x GEN red LED annunciator illuminates and x Voltmeter indicates voltag...

Page 43: ...ransponder and GPS as necessary short time only Operating time of battery in good condition is up to 30 minutes The engine runs independently on generator functioning 3 17 Inadvertent spin recovery Th...

Page 44: ...8 If you fail to recover the engine power or normal flight conditions land on the nearest airfield if possible or depending on the circumstances perform a precautionary landing according to 3 10 or em...

Page 45: ...th a flat tire 1 During landing keep the damaged wheel above ground as long as possible using the ailerons control 2 Maintain the direction on the landing roll out applying rudder control 3 22 Landing...

Page 46: ...ontrols Lateral control failure Use the Aileron Trim and Rudder for aircraft banking CAUTION Avoid steep turns more than 15 of bank Do not extend wing flaps Longitudinal control failure Use the Elevat...

Page 47: ...ove mentioned cases there are no flight problems no vibrations good aircraft control and no change of flight characteristics x It is not possible to close the canopy Recommended procedure if the canop...

Page 48: ...SC POH 1 1 17 Revision Date of issue 2011 09 01 SECTION 3 EMERGENCY PROCEDURES S Sp po or rt tC Cr ru ui is se er r 3 14 Intentionally left blank...

Page 49: ...ck 4 2 4 2 Engine starting 4 5 4 3 Taxiing 4 7 4 4 Normal takeoff 4 7 4 5 Climb 4 8 4 6 Best angle of climb speed Vx 4 7 4 7 Best rate of climb speed Vy 4 8 4 8 Cruise 4 8 4 9 Descend 4 8 4 10 Approac...

Page 50: ...3 R three composite blades ground adjustable propeller 4 1 Preflight check Carry out the pre flight inspection every day prior to the first flight or after airplane assembly Incomplete or careless in...

Page 51: ...urn coordinator functioning x AVIONICS ON check functioning of Transponder Transceiver and Intercom x NAV L STROBE LDG L ON check functioning x COCKPIT L INSTR L ON check functioning x Control system...

Page 52: ...ASTER BAT OFF then turn the propeller by hand in direction of engine rotation several times to pump oil from the engine into the oil tank see the Rotax Operator s manual section 10 3 3 x Coolant quant...

Page 53: ...t will facilitate engine starting 4 2 Engine starting 4 2 1 Before engine starting 1 Control system free correct movement 2 Canopy clean close and lock 3 Safety harness fasten 4 Brakes fully applied 5...

Page 54: ...up Engine check Prior to engine check block the main wheels using chocks Initially warm up the engine to 2 000 rpm for approximately 2 min then continue to 2 500 rpm till oil temperature reaches 122...

Page 55: ...ystem check free movement 4 Cockpit canopy closed and locked Recommendation Before takeoff manually check the canopy is locked by pushing the canopy upwards 5 Safety harness fastened 6 FUEL selector L...

Page 56: ...LE MAX max 5 800 rpm for max 5 min max continuous power 5 500 rpm 2 Airspeed Vx 56 KIAS Vy 62 KIAS 3 Trims as necessary 4 Engine gauges oil temperature oil pressure and CHT within limits CAUTION If th...

Page 57: ...e In such cases the engine becomes under cooled and a loss of power may occur Descent at increased idle approximately 3 000 rpm airspeed 60 75 KIAS and check that the engine instruments indicate value...

Page 58: ...CAUTION Rapid engine cooling should be avoided during operation This happens above all during aircraft descent taxiing and low engine rpm or at engine shutdown immediately after landing Under normal...

Page 59: ...necessary 4 14 Aircraft parking and tie down 1 Ignition Switch OFF 2 MASTER BAT GEN OFF 3 FUEL selector OFF 4 Parking brake as necessary 5 Canopy close lock as necessary 6 Secure the airplane NOTE It...

Page 60: ...check of whole Lighting system and Battery condition before night flights 4 15 2 Before engine starting 1 COCKPIT L ON 2 INSTR L ON adjust illumination level 3 NAV L ON 4 LDG L ON check function OFF 4...

Page 61: ...r ru ui is se er r 5 1 SECTION 5 TABLE OF CONTENTS 5 PERFORMANCE 5 1 Takeoff distances 5 3 5 2 Landing distances 5 3 5 3 Rate of climb 5 3 5 4 Cruise speeds 5 4 5 5 RPM setting and fuel consumption 5...

Page 62: ...ting techniques If not stated otherwise the performance stated in this section is valid for maximum takeoff weight 1 320 lb and under ISA conditions The performance shown in this section is valid for...

Page 63: ...ft CONCRETE 463 1 270 GRASS 702 1 499 5 2 Landing distances Conditions Altitude 0 ft ISA Engine power idle Flaps 30 Normal brakes operation RUNWAY SURFACE Landing distance over 50 ft obstacle Landing...

Page 64: ...8 69 72 22 2 3 49 4 500 78 77 80 23 0 4 04 4 800 86 85 88 23 8 4 62 5 000 93 91 94 24 3 5 02 5 300 102 99 102 25 1 5 65 5 500 108 104 108 25 5 6 16 5 000 4 200 65 66 71 20 5 3 41 4 500 74 74 79 21 3 3...

Page 65: ...urance and Range at 29 85 US gal Endurance hh mm 8 18 7 11 6 16 5 47 5 09 4 46 Range NM 607 583 559 551 531 520 Endurance and Range at 23 78 US gal Endurance hh mm 6 37 5 43 5 00 4 36 4 06 3 47 Range...

Page 66: ...29 85 US gal Endurance hh mm 8 33 7 23 6 27 5 56 5 16 4 50 Range NM 616 591 568 559 539 524 Endurance and Range at 23 78 US gal Endurance hh mm 6 49 5 52 5 08 4 44 4 12 3 51 Range NM 491 471 453 445 4...

Page 67: ...29 85 US gal Endurance hh mm 8 45 7 35 6 34 6 02 5 21 4 57 Range NM 622 599 572 562 541 530 Endurance and Range at 23 78 US gal Endurance hh mm 6 58 6 02 5 13 4 48 4 15 3 56 Range NM 495 477 455 448 4...

Page 68: ...85 US gal Endurance hh mm 9 02 7 44 6 43 6 08 5 25 5 04 Range NM 624 596 572 559 538 532 Endurance and Range at 23 78 US gal Endurance hh mm 7 12 6 09 5 21 4 53 4 19 4 02 Range NM 497 475 455 445 428...

Page 69: ...85 US gal Endurance hh mm 9 15 7 54 6 53 6 16 5 32 5 11 Range NM 621 585 572 559 537 534 Endurance and Range at 23 78 US gal Endurance hh mm 7 22 6 17 5 29 5 00 4 24 4 07 Range NM 494 466 455 445 428...

Page 70: ...ERFORMANCE S Sp po or rt tC Cr ru ui is se er r 5 10 5 6 Airspeed indicator system calibration KIAS KCAS 30 36 35 40 40 45 45 49 50 53 55 57 60 62 65 66 70 71 75 75 80 79 85 83 90 88 95 92 100 97 105...

Page 71: ...5 7 Demonstrated wind performance Max demonstrated headwind velocity for take off and landing 24 knots Max demonstrated crosswind velocity for take off and landing 12 knots Wind components figure Exam...

Page 72: ...Revision Date of issue 2011 09 01 SC POH 1 1 17 SECTION 5 PERFORMANCE S Sp po or rt tC Cr ru ui is se er r 5 12 Intentionally left blank...

Page 73: ...g pressure Drain fuel from fuel installation Add oil hydraulic and cooling liquid up to the maximum specified value Retract wing flaps close the canopy and other lids and covers remove control surface...

Page 74: ...priate table 6 3 Operating weights and loading Weights Max takeoff weight 1 320 lb Max landing weight 1 320 lb Max weight of fuel 180 lb Max baggage weight in rear fuselage 40 lb Max baggage weight in...

Page 75: ...09 01 S Sp po or rt tC Cr ru ui is se er r 6 4 6 4 Weight and balance C G layout 6 5 C G range and determination 6 5 1 Aircraft C G range Empty weight C G range 28 5 to 29 5 of MAC 16 83 to 17 42 in o...

Page 76: ...HEEL WR LR LEFT MAIN WHEEL WL LL NOSE WHEEL WN LN negative arm TOTAL Empty weight WTE C G in MAC Aircraft moment MTE WEIGHT BALANCE REPORT Empty Weight CG Check Empty weight CG range 28 to 32 of MAC M...

Page 77: ...ulic fluid and unusable fuel Empty weight C G range 16 83 to 17 42 in 28 5 to 29 5 of MAC Operating C G range 16 54 to 20 67 in 28 to 35 of MAC MAC 59 06 in MOMENT lb in WEIGHT lb x ARM in MTE 100 AIR...

Page 78: ...l fuel depletion most rearward C G check Loading and C G check table ITEM WEIGHT lb ARM in MOMENT lb in EMPTY AIRCRAFT PILOT 27 56 PASSENGER 27 56 BAGGAGE COMPARTMENT 51 58 WING LOCKERS 23 62 FUEL TAN...

Page 79: ...72 PASSENGER 143 0 27 56 3 941 08 BAGGAGE COMPARTMENT 22 0 51 58 1 134 76 WING LOCKERS 22 0 23 62 519 64 FUEL TANKS 94 6 7 09 670 71 TOTAL WT 1 320 0 C G 19 63 in 33 2 MAC MT 25 912 98 WEIGHT BALANCE...

Page 80: ...G 19 63 in 33 2 MAC MT 25 242 26 4 6 Date of Issue 12 2007 Revision 2 0 WEIGHT BALANCE REPORT Forward CG Check WEIGHT lb ARM in MOMENT WEIGHT x ARM EMPTY AIRCRAFT 842 3 14 450 0 PILOT 88 0 27 6 2 428...

Page 81: ...ng oil coolant hydraulic fluid and unusable fuel Maximum fuel quantity in wing tanks 30 1 US gal 180 6 lb is used for most forward C G calculation Zero fuel quantity in wing tanks is used for most rea...

Page 82: ...C POH 1 1 17 SECTION 6 WEIGHT BALANCE Revision Date of issue 2011 09 01 S Sp po or rt tC Cr ru ui is se er r 6 11 6 7 Fuel weight quantity conversion chart 6 8 C G change in dependence of fuel quantit...

Page 83: ...d C G check in case of total fuel depletion 5 The starting position line drawing is the intersection point of empty weight with empty C G marked as c 6 Go vertically down to the pilot weight scale tha...

Page 84: ...SC POH 1 1 17 SECTION 6 WEIGHT BALANCE Revision Date of issue 2011 09 01 S Sp po or rt tC Cr ru ui is se er r 6 13...

Page 85: ...SC POH 1 1 17 SECTION 6 WEIGHT BALANCE Revision Date of issue 2011 09 01 S Sp po or rt tC Cr ru ui is se er r 6 14 Blank form of Load sheet Balance chart...

Page 86: ...LT VSI Compass RC Allen electric turn coordinator RC Allen directional gyro TruTrak ADI flight instrument Garmin SL40 transceiver PS Engineering PM3000 stereo intercom Garmin GTX327 transponder King A...

Page 87: ...SC POH 1 1 17 SECTION 6 WEIGHT BALANCE Revision Date of issue 2011 09 01 S Sp po or rt tC Cr ru ui is se er r 6 16 Intentionally left blank...

Page 88: ...SCRIPTION OF AIRPLANE AND SYSTEMS 7 1 General 7 2 7 2 Airframe 7 2 7 3 Flight controls 7 2 7 4 Instrument panel 7 3 7 5 Engine 7 3 7 6 Propeller 7 4 7 7 Landing gear 7 5 7 8 Baggage compartment 7 5 7...

Page 89: ...n is of 6061 T6 aluminum sheet metal riveted to aluminum angles with Avex rivets This high strength aluminum alloy construction provides long life and low maintenance costs thanks to its durability an...

Page 90: ...ced lubrication Dual contactless capacitor discharge ignition The engine is fitted with an electric starter AC generator and mechanical fuel pump Prop drive via reduction gear with integrated shock ab...

Page 91: ...system is independent of the power source and will operate even with Master switch and or breaker OFF Engine instruments The following analog engine instruments are located on the right side of instr...

Page 92: ...lbs Baggage may also be loaded into the baggage compartment inside each wing up to 22 lbs in each wing locker Make sure that baggage does not exceed maximum allowable weight and that the aircraft C G...

Page 93: ...oint of the each tank and on the bottom edge of the firewall on the gascolator Fuel selector valve is on the central console in the cockpit The electric fuel pump is located on firewall and it is used...

Page 94: ...battery to the electrical system Master generator switch MASTER GEN switch connects the alternator to the electrical system Circuit breakers and switches NOTE Circuit breakers and switches description...

Page 95: ...SC POH 1 1 17 SECTION 7 DESCRIPTION OF AIRPLANE AND SYSTEMS Revision Date of issue 2011 09 01 S Sp po or rt tC Cr ru ui is se er r 7 8 Intentionally left blank...

Page 96: ...CTION 8 TABLE OF CONTENTS 8 HANDLING AND SERVICING 8 1 Introduction 8 2 8 2 Ground handling 8 2 8 3 Towing instructions 8 3 8 4 Tie down instructions 8 3 8 5 Servicing operating fluids 8 3 8 6 Cleanin...

Page 97: ...it canopy possibly the whole airplane by means of a suitable tarpaulin 8 2 2 Jacking Since the empty weight of this aircraft is relatively low two people can lift the aircraft easily First of all prep...

Page 98: ...st possible damage caused by wind and gusts For this reason the aircraft is equipped with mooring eyes located on the lower surfaces of the wings Tie down procedures 1 FUEL selector OFF 2 MASTER BAT G...

Page 99: ...he valve seats due to its high lead content and forms increased deposits in the combustion chamber and lead sediments in the oil system Thus it should only be used in case of problems with vapor lock...

Page 100: ...e can lead to damages to the cooling system and engine Type of coolant used by aircrafts manufacturer see Section 9 Supplement No 02 Coolant liquid volume It is approximately 0 66 US gal 8 6 Cleaning...

Page 101: ...s listed in x S Sp po or rt tC Cr ru ui is se er r aircraft Maintenance manual for aircraft maintenance x Rotax engine Maintenance manual for engine maintenance x Woodcomp Klassic propeller manual for...

Page 102: ...1 17 SECTION 9 SUPPLEMENTS Revision Date of issue 2011 09 01 S Sp po or rt tC Cr ru ui is se er r 9 1 SECTION 9 TABLE OF CONTENTS 9 SUPPLEMENTS 9 1 List of inserted supplements 9 2 9 2 Inserted supple...

Page 103: ...lements necessary to safely and efficiently operate the aircraft when equipped with various optional systems and equipment not provided with the standard airplane 9 1 List of inserted supplements Date...

Page 104: ...depends on the Flight Instructor if student pilot is ready to continue on in next training step Training can be performed by Flight Instructor or by the experienced pilot who has minimum 20 hours on...

Page 105: ...lot will fly the airplane in local flight instructor giving advice as necessary 2 Pattern training flights up to 1 000 feet AGL High pattern procedures instructor giving advice as necessary 3 Pattern...

Page 106: ...gistration number Aircraft Serial Number This Supplement must be attached to the POH during airplane operation Information in this Supplement completes or replaces information in the basic POH for the...

Page 107: ...eful weight W Max Useful W Max Take Off WE W Max Useful 1320 lb 842 3 lb 477 7 lb This useful weight must be never exceeded ME 100 Aircraft Empty CG in x WE MAC ITEM WEIGHT lb ARM in MOMENT WEIGHT x A...

Page 108: ...wl x Cockpit light Instrument lighting x Adjustable pedals x Dual hydraulic brakes x Parking brake x Wheel fairings tricycle x Cabin heating Carburetor preheating x Leather upholstery x Paint x Sunsha...

Page 109: ...nt panel Instrument panel layout of S Sp po or rt tC Cr ru ui is se er r aircraft S N 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 36 37 38 39 40 41...

Page 110: ...n heating 20 ELT control unit and buzzer 42 Aileron trim indicator 21 Oil temperature gauge 43 Transponder 22 Fuel quantity indicator RH tank 44 Circuit breakers Switches and circuit breakers detailed...

Page 111: ...struments lighting dimmer RIGHT PART OF INSTRUMENT PANEL COMM transceiver circuit breaker 5A IC intercom circuit breaker 1A ENG INSTR engine instruments circuit breaker 1A NAV navigation device circui...

Page 112: ...indicator Electric directional gyor Electric turn coordinator CDI Engine RPM indicator Oil pressure and temperature gauges Fuel pressure and quantity gauges CHT indicator Voltmeter Engine hours count...

Page 113: ...ng operating fluids 8 5 2 Approved oil grades and specifications Type of oil used by aircrafts manufacturer AeroShell Oil Sport Plus 4 SAE 10W 40 API SL 8 5 3 Approved coolant grades and specification...

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