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EVEKTOR-AEROTECHNIK SportStar plus, Руководство по эксплуатации самолета

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FLIGHT MANUAL 

Doc. No. SP2006FMENKT 

December 20, 2006

 

7 - 3 

Section 7 

Airplane and System 

Description 

7.  AIRPLANE AND SYSTEM DESCRIPTION 

7.1  Introduction 

This section describes systems of the airplane and its operation. 
More detailed information on optional systems and equipment are 
available in section 9, Supplements.  

7.2  Airframe 

The airframe of  SPORTSTAR

PLUS

 airplane is of semimonocoque 

structure consisting of metal reinforcement, frames and duralumin 
sheet skin. 

7.2.1  Fuselage 

The fuselage is of semimonocoque structure consisting of 
reinforcements and duralumin skin. Fuselage section is rectangular 
in the lower part and eliptic in the upper part. The fin is an integral 
part of fuselage. The cockpit for two-member crew is located in the 
middle part of the fuselage that is accessible after uncovering the 
single-piece organic glass canopy. The engine compartment in the 
front part of the fuselage is separated from the cockpit by the steel 
fire wall  to which the engine bed is attached.  

7.2.2  Wing 

The wing is of rectangular shape, single-spar structure with the 
auxiliary spar  with suspended  ailerons and split wing flaps. 
Riveting is used for connecting individualstructural elements.  Fiber-
glass wing tips are riveted on the wing ends.   

7.2.3  Horizontal tail unit (HTU) 

The VTU of conventional type consists of  the stabilizer and 
elevator with the trim tab. Single-spar structure of HTU consists of 
duralumin ribs, spar and skin. Top view of HTU is of rectangular 
shape.   

7.2.4  Vertical tail unit (VTU) 

VTU is of trapezoidal shape. Its fin is an integral part of  the 
fuselage.  The rudder is suspended on the fin by means of two 
hinges. The VTU structure consists of  the duralumin spar and skin. 

Содержание SportStar plus

Страница 1: ...mber Registration mark Document number SP2006FMENKT Date of issue December 20 2006 This manual must be on the airplane board during operation This manual contains information which must be provided to...

Страница 2: ......

Страница 3: ...FLIGHT MANUAL Doc No SP2006FMENKT December 20 2006 0 1 Section 0 Technical Information CONTENTS 0 TECHNICAL INFORMATION 3 0 1 Log of Revisions 3 0 2 List of Effective Pages 5 0 3 FM Sections 8...

Страница 4: ...FLIGHT MANUAL Doc No SP2006FMENKT 0 2 December 20 2006 Section 0 Technical Information Intentionally left blank...

Страница 5: ...issued in form of revisions which will have new or changed pages as appendix and the list of which is shown in the Log of Revisons table The new or changed text in the revised pages will be marked by...

Страница 6: ...FLIGHT MANUAL Doc No SP2006FMENKT 0 4 December 20 2006 Section 0 Technical Information Rev No Affected Section Affected Pages Date Appro ved Date Date of Insertion Sign...

Страница 7: ...Dec 20 06 0 4 Dec 20 06 2 6 Dec 20 06 0 5 Dec 20 06 2 7 Dec 20 06 0 6 Dec 20 06 2 8 Dec 20 06 0 7 Dec 20 06 2 9 Dec 20 06 0 8 Dec 20 06 2 10 Dec 20 06 2 11 Dec 20 06 2 12 Dec 20 06 1 1 1 Dec 20 06 1...

Страница 8: ...Dec 20 06 4 9 Dec 20 06 4 10 Dec 20 06 4 11 Dec 20 06 4 12 Dec 20 06 6 6 1 Dec 20 06 4 13 Dec 20 06 6 2 Dec 20 06 4 14 Dec 20 06 6 3 Dec 20 06 4 15 Dec 20 06 6 4 Dec 20 06 4 16 Dec 20 06 6 5 Dec 20 06...

Страница 9: ...06 8 4 Dec 20 06 8 5 Dec 20 06 8 6 Dec 20 06 7 7 1 Dec 20 06 8 7 Dec 20 06 7 2 Dec 20 06 8 8 Dec 20 06 7 3 Dec 20 06 7 4 Dec 20 06 7 5 Dec 20 06 7 6 Dec 20 06 7 7 Dec 20 06 7 8 Dec 20 06 7 9 Dec 20 06...

Страница 10: ...6 Section 0 Technical Information 0 3 FM Sections Section GENERAL 1 LIMITATIONS 2 EMERGENCY PROCEDURES 3 NORMAL PROCEDURES 4 PERFORMANCE 5 WEIGHT AND BALANCE 6 AIRPLANE AND SYSTEM DESCRIPTION 7 AIRPLA...

Страница 11: ...General CONTENTS 1 GENERAL 3 1 1 Introduction 3 1 2 Certification basis 3 1 3 Warnings cautions notes 3 1 4 Descriptive data 4 1 4 1 Airplane description 4 1 4 2 Powerplant 4 1 4 3 Main technical data...

Страница 12: ...FLGHT MANUAL Doc No SP2006FMENKT 1 2 December 20 2006 Section 1 General Intentionally left blank...

Страница 13: ...nation F 2245 04 issued by ASTM International Committee F37 This type of aircraft complies with the Czech UL 2 airworthiness requirements it has been type certified by the Light Aircraft Association o...

Страница 14: ...description 1 4 2 Powerplant The standard powerplant consists of ROTAX 912ULS 100 hp engine and WOODCOMP KLASSIC 170 3 R propeller For further description see Section 7 Airplane and system descriptio...

Страница 15: ...ft 2 50 m HTU Area 20 88 sq ft 1 94 sq m Elevator area 8 40 sq ft 0 78 sq m Vertical tail unit Height 4 07 ft 1 24 m VTU Area 10 76 sq ft 1 00 sq m Rudder area 4 31 sq ft 0 40 sq m Landing gear Wheel...

Страница 16: ...FLGHT MANUAL Doc No SP2006FMENKT 1 6 December 20 2006 Section 1 General 1 4 4 Three view drawing Figure 1 1...

Страница 17: ...calibrated airspeed CLOCK aircraft clock ft foot 1 ft 0 305 m GPS global positioning system HTU horizontal tail unit IAS indicated airspeed IC intercom IFR instrument flight rules ISA international st...

Страница 18: ...ns per minute RWY runway sq ft foot squared sq m meter squared VA manoeuvring airspeed VFE maximum flap extended speed flaps in 50 position VFR visibility flight rules VLOF airplane lift off speed V M...

Страница 19: ...marking 4 2 4 Powerplant 5 2 5 Powerplant instrument marking 6 2 6 Miscellaneous instrument marking 6 2 7 Weight 6 2 8 Centre of gravity 7 2 9 Approved manoeuvres 7 2 10 Manoeuvring load factors 7 2...

Страница 20: ...FLIGHT MANUAL Doc No SP2006FMENKT 2 2 December 20 2006 Section 2 Limitations Intentionally left blank...

Страница 21: ...ns and their meaning for operation are stated in the table below Speed KIAS mph IAS Meaning VNE Never exceed speed 146 168 Do not exceed this speed in any operation VNO Maximum structural cruising spe...

Страница 22: ...Red line 38 44 VS0 at maximum weight flaps in landing position 50 White arc 38 70 44 81 Operating range with extended flaps Lower limit VS0 at maximum weight flaps 50 Upper limit VFE Green arc 43 105...

Страница 23: ...imum 135 C 275 F Oil temperature maximum 130 C 266 F optimum operation 90 110 C 190 230 F Oil pressure maximum 7 bar 102 PSI minimum 0 8 bar 12 PSI optimum operation 2 5 bar 29 73 PSI Fuel pressure mi...

Страница 24: ...PM 1400 5500 5500 5800 5800 C 90 110 50 90 110 130 130 Oil temperature indicator F 190 230 120 190 230 266 266 bar 0 8 2 5 0 8 2 5 7 7 Oil pressure indicator PSI 12 29 73 12 29 73 102 102 C 135 Cylind...

Страница 25: ...20 to 34 MAC Reference datum is the wing leading edge 2 9 Approved manoeuvres SPORTSTAR PLUS airplane is approved to perform the following manoeuvres steep turns up to bank angle of 60 climbing turns...

Страница 26: ...N REQUIRED FOR SUCH FLIGHTS IS INSTALLED AND FLIGHT PERFORMED BY A PILOT WITH APPROPRIATE RATING INTENTIONAL FLIGHTS UNDER ICING CONDITIONS ARE PROHIBITED Instruments and equipment for daylight flight...

Страница 27: ...preventing environmental contamination This should be adhered especially when cold fuel from an underground tank is tanked Approved fuel grades automotive petrol with min RON 95 EN 228 Premium EN 228...

Страница 28: ...maximum 0 79 U S gallons 3 0 litres 2 15 Maximum number of passengers Maximum number of passengers including pilot 2 2 16 Other limitations SMOKING IS PROHIBITED on the airplane board 2 17 Limitation...

Страница 29: ...l quantity U S gal Baggage weight or LOAD LIMITS Max take off weight 550 kg Empty weight 305 kg Max baggage weight 25 kg PERMITTED CREW WEIGHT kg 120 100 75 50 25 max 25 kg 134 148 166 184 202 1 2 12...

Страница 30: ...FLIGHT MANUAL Doc No SP2006FMENKT 2 12 December 20 2006 Section 2 Limitations Intentionally left blank...

Страница 31: ...gine starting at flight 4 3 5 Engine fire 5 3 5 1 Fire on the ground 5 3 5 2 Fire during take off 5 3 5 3 Fire in flight 6 3 6 Fire in the cockpit if manual extinguisher available aboard 7 3 7 Gliding...

Страница 32: ...FLIGHT MNAUAL Doc No SP2006FMENKT 3 2 December 20 2006 Section 3 Emergency Procedures...

Страница 33: ...ne running flaps in landing position 50 Emergency landing 53 KIAS 61 mph IAS engine stopped flaps in landing position 50 3 3 Engine failure 3 3 1 Engine failure at take off run 1 THROTTLE lever idle 2...

Страница 34: ...and carry out Engine starting in flight paragraph 3 4 Emergency landing paragraph 3 8 1 3 4 Engine starting at flight NOTE It is possible to start the engine by means of the starter within the whole r...

Страница 35: ...air flow turns the propeller and engine will start 11 Ignition BOTH 12 If engine starting is unsuccessful then continue according to paragraph 3 8 1 Emergency landing 3 5 Engine fire 3 5 1 Fire on th...

Страница 36: ...nition OFF 6 ATC report if possible 7 Master switch OFF NOTE For extinguishing the engine fire you can perform slip under assumption that you have sufficient altitude and time WARNING AFTER EXTINGUISH...

Страница 37: ...l extinguisher use 4 After fire extinguishing aerate the cockpit 5 Carry out safety landing according to 3 8 2 WARNING NEVER AGAIN SWITCH THE DEFECTIVE SYSTEM NOTE If a defective electrical system cir...

Страница 38: ...Airspeed 60 KIAS 69 mph IAS 6 Radiostation notify situation to ATC if possible 7 FUEL SELECTOR OFF 8 Ignition OFF 9 Master switch OFF before touch down 3 8 2 Safety landing with engine operating 1 Ar...

Страница 39: ...keep the airplane on main landing gear wheels as long as possible 2 In case of main landing gear damage touch down at he lowest possible speed and if possible keep direction at running 3 9 Unintention...

Страница 40: ...r occurs due to its acceleration in the carburettor and further cooling by evaporating fuel Carburettor icing mostly happens during descending and aproaching for landing low engine RPM Carburettor ici...

Страница 41: ...ssembly and disassembly 3 4 4 Pre flight check 4 4 5 Normal procedures and checklist 8 4 5 1 Before engine starting 8 4 5 2 Engine starting 8 4 5 3 Before taxiing 10 4 5 4 Taxiing 10 4 5 5 Before take...

Страница 42: ...FLIGHT MANUAL Doc No SP2006FMENKT 4 2 December 20 2006 Section 4 Normal Procedures Intentionally left blank...

Страница 43: ...ormal procedures 4 2 1 Take off Climbing speed up to 50 ft flaps in take off pos 15 56 KIAS 65 mph IAS Best rate of climb speed VY flaps in take off pos 15 56 KIAS 65 mph IAS Best rate of climb speed...

Страница 44: ...ding to the following procedure Figure 4 1 Scheme of airplane preflight check WARNING CHECK BEFORE PRE FLIGHT CHECK THAT IGNITION IS SWITCHED OFF NOTE The word condition used in procedures of pre flig...

Страница 45: ...light condition if installed condition of the Pitot tube draining of fuel tank see chapter8 page 8 6 closing of fuel tank cap 3 Left wing tip check surface condition attachment check fuel tank vent c...

Страница 46: ...led and Pitot tube 13 Right landing gear leg see 1 14 Front part of the fuselage right hand side check tilting canopy attachment and condition condition of the nose landing gear leg nose wheel conditi...

Страница 47: ...nd side check tilting canopy attachment and condition 18 Cockpit check NOTE Turn handle clockwise to open cockpit When keyway is in handle axix cockpit is locked Unlock it first with key to keyway per...

Страница 48: ...ICS SWITCH if installed check OFF 10 Ignition check OFF 11 Canopy close 4 5 2 Engine starting 1 Master switch ON 2 Fuel gauge indicators check of fuel quantity 3 FUEL SELECTOR LEFT Pull the safety but...

Страница 49: ...EN if inst switches ON 14 Electric fuel pump if installed OFF NOTE After starting up engine adjust throttle for smooth engine running at about 2500 RPM Check oil pressure Pressure must increase within...

Страница 50: ...n hose is led only into the left tank and returning fuel will overfill the left tank 20 AVIONICS SWITCH if installed ON 21 Radiostation avionics ON 22 Other electrical equipment ON as necessary 4 5 3...

Страница 51: ...ine instruments check 4 Control stick free 5 Wing flaps take off pos 15 6 Trim NEUTRAL 7 Fuel gauge indicator check on fuel quantity 8 FUEL SELECTOR check LEFT 9 CARBURETTOR PREHEATER if installed che...

Страница 52: ...mph IAS 4 Brakes brake 5 After reaching 150 ft set flaps to retracted pos 0 6 Trim as necessary WARNING TAKE OFF IS PROHIBITED IF ENGINE RUNNING IS IRREGULAR IF CHOKE IS OPEN IF VALUES OF ENGINE INSTR...

Страница 53: ...to equally consume fuel from both tanks and minimize airplane tendency to bank with unbalanced tanks Do not fly with the fuel selector set to RIGHT if the left tank is full to avoid fuel bleed from le...

Страница 54: ...OF POSSIBLE ENGINE UNDERCOOLING AND SUBSEQUENT LOSS OF POWER PERFORM DESCENDING AT INCREASED IDLE AND CHECK OBSERVANCE OF THE ALLOWED VALUES ON ENGINE INSTRUMENTS 4 5 10 Before landing 1 Fuel quantity...

Страница 55: ...pos 30 or 50 2 Maintain airspeed 60 KIAS 69 mph IAS 3 Trim as necessary 4 CARBURETTOR PREHEATER if installed OFF 4 5 11 Balked landing 1 THROTTLE lever max take off power 2 Flaps take off pos 15 3 Ai...

Страница 56: ...retracted pos 0 2 Trim NEUTRAL 3 Outside lights if installed OFF 4 Transponder if installed OFF 4 5 14 Engine shut off 1 THROTTLE lever idle 2 Engine instruments check 3 AVIONICS SWITCH OFF 4 Radiost...

Страница 57: ...afety button Now the handle is blocked in the OFF position Safety button prevents unintentionally switch the selector from the OFF position 4 PARKING BRAKE handle if installed brake as necessary 5 Can...

Страница 58: ...FLIGHT MANUAL Doc No SP2006FMENKT 4 18 December 20 2006 Section 4 Normal Procedures Intentionally left blank...

Страница 59: ...calibration 4 5 2 2 Stall speeds 6 5 2 3 Take off distance 7 5 2 4 Landing distance 7 5 2 5 Climb performance 8 5 3 Additional information 10 5 3 1 Cruise 10 5 3 2 Horizontal speeds 11 5 3 3 Endurance...

Страница 60: ...FLIGHT MNAUAL Doc No SP2006FMENKT 5 2 December 20 2006 Section 5 Performance Intentionally left blank...

Страница 61: ...by the airplane type certificate owner The stated performance data has been computed from actual flight tests with the SPORTSTAR PLUS airplane and ROTAX 912 ULS engine in good condition and using aver...

Страница 62: ...575 kg KIAS KCAS KIAS KCAS KIAS KCAS 38 40 41 43 40 41 43 45 43 44 43 44 45 47 45 46 45 46 50 51 47 48 47 47 55 55 50 50 50 50 60 60 53 53 53 53 65 64 55 55 55 54 70 68 57 57 57 56 75 73 60 59 60 59...

Страница 63: ...3 53 60 61 55 56 55 55 65 65 57 57 57 57 70 69 60 60 60 60 75 74 63 63 63 62 80 78 65 65 65 64 85 82 67 66 67 66 90 87 70 69 70 69 95 91 73 72 73 71 100 96 75 74 75 73 105 100 77 75 77 75 110 105 80 7...

Страница 64: ...termined on the basis of flight tests using average piloting technique 575 kg Altitude loss 1268 lb KIAS KCAS ft Retracted 0 43 45 Take off 15 41 43 Landing 50 38 40 Retracted 0 46 49 Take off 15 44 4...

Страница 65: ...e of wind Add 4 on every 1 kt 1 15 mph of tail wind RWY inclination Add 8 of the take off run distance on 1 of ruway inclination up the slope 5 2 4 Landing distance Conditions engine idle flaps Landin...

Страница 66: ...tter preheating OFF airplane weight 1268 lbs 575 kg ambient air temperature ISA SportStar plus Rate of Climb Woodcomp Klassic 170 3 R propeller Rotax 912 ULS engine 150 200 250 300 350 400 450 500 550...

Страница 67: ...FLIGHT MANUAL Doc No SP2006FMENKT December 20 2006 5 9 Section 5 Performance Best rate of climb for various altitudes is mentioned in the following table...

Страница 68: ...bs 575 kg ambient air temperature ISA SportStar plus Horizontal speeds Rotax 912 ULS engine Woodcomp Klassic 170 3 R propeller 50 55 60 65 70 75 80 85 90 95 100 105 110 115 120 3500 3600 3700 3800 390...

Страница 69: ...Maximum Continuous Power MTP Maximum Takeoff Power 5 min 4300 rpm 4800 rpm 5000 rpm 5500 rpm 5800 rpm KIAS 82 93 97 109 116 KCAS 78 88 92 103 110 0 ft ISA KTAS 78 88 92 103 110 KIAS 78 89 94 106 KCAS...

Страница 70: ...5 50 4 46 Range at 120 0 l km 1220 1050 1000 910 31 7 USGAL NM 659 567 540 491 26 4 UKGAL miles 758 652 621 565 Endurance at 100 0 l h m 7 05 5 22 4 52 3 59 Range at 100 0 l km 1020 870 830 760 26 4 U...

Страница 71: ...ngine maximum take off power carburetter preheating OFF flaps landing position 50 airplane weight 1268 lbs 575 kg ambient air temperature ISA BALKED LANDINGCLIMB 0 100 200 300 400 500 600 700 800 35 4...

Страница 72: ...re not considerably affected by rain or insect stuck on the airplane surface 5 3 6 Demonstrated crosswind performance Maximum demonstrated speed of wind at airplane operation 24 kts 28 mph Maximum dem...

Страница 73: ...FLIGHT MANUAL Doc No SP2006FMENKT December 20 2006 5 15 Section 5 Performance 5 3 7 Ceiling Service ceiling of SPORTSTARPLUS 13 030 ft 5 3 8 Noise data Not measured...

Страница 74: ...FLIGHT MNAUAL Doc No SP2006FMENKT 5 16 December 20 2006 Section 5 Performance Intentionally left blank...

Страница 75: ...3 6 2 Weight and Balance Record 4 6 3 Permitted Payload Range 5 6 4 Operational Weight and Balance Computation 6 6 4 1 Computational Procedure 6 6 5 Airplane Loading Schedule Chart 8 6 6 Table of Stat...

Страница 76: ...FLIGHT MANUAL Doc No SP2006FMENKT 6 2 December 20 2006 Section 6 Weight and Balance Intentionally left blank...

Страница 77: ...Permitted Payload Range within which the airplane may be safely operated and a method to determine whether the operational weight and CG location will be within the permitted limits range Procedure fo...

Страница 78: ...lance 6 2 Weight and Balance Record Moment kg mm Basic weight of empty airplane Weight kg Moment kg mm Arm mm Removed Weight kg Moment kg mm Arm mm Serial No Weight change Added Weight kg Description...

Страница 79: ...tted Payload Range Signature Approved Date 0 2 25 18 0 4 50 35 0 6 75 54 0 8 100 72 1 120 86 25 kg 12 kg 0 kg 25 kg 12 kg 0 kg 25 kg 12 kg 0 kg 25 kg 12 kg 0 kg F U E L L I N G Fuel volume Fuel volume...

Страница 80: ...Schedule Chart 5 Determine Take off weight of the airplane add together the airplane empty weight crew fuel and baggage and record the result into the Loading Schedule Chart 6 Check whether the calcu...

Страница 81: ...Weight and Balance computation the intersection of Take off Weight and Total Static Moment will be inside the CG Moment envelope WARNING SAFETY OF FLIGHT PERFORMED WITH THE AIRPLANE LOADED OUTSIDE PE...

Страница 82: ...oading Schedule Chart Sample Aircraft Your Aircraft No Item Arm m Weight kg Moment kg m Weight kg Moment kg m 1 Empty Airplane 0 264 m 336 kg 88 8 kg m 2 Crew 0 545 m 181 kg 98 6 kg m 3 Baggage Max 55...

Страница 83: ...7 110 60 0 7 7 6 35 0 25 2 17 1 120 65 4 8 8 7 40 0 28 8 19 6 130 70 9 9 9 7 45 0 32 4 22 0 140 76 3 10 10 8 50 0 36 0 24 5 150 81 8 11 11 9 55 0 39 6 26 9 160 87 2 12 13 0 60 0 43 2 29 4 170 92 7 13...

Страница 84: ...0 40 50 60 70 80 90 100 110 120 130 140 150 160 170 180 190 200 210 220 230 240 250 0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95 100 105 110 115 120 125 130 135 140 145 150 Load Moment kg...

Страница 85: ...CG Moment Envelope SportStar plus CG Moment Envelope 350 360 370 380 390 400 410 420 430 440 450 460 470 480 490 500 510 520 530 540 550 560 570 580 590 600 50 60 70 80 90 100 110 120 130 140 150 160...

Страница 86: ...onal Weight and CG Envelope SportStar plus Operational Weight and CG Envelope 350 360 370 380 390 400 410 420 430 440 450 460 470 480 490 500 510 520 530 540 550 560 570 580 590 600 18 19 20 21 22 23...

Страница 87: ...6 6 13 Section 6 Weight and Balance 6 10 Equipment List The equipment installed in the airplane of particular serial number is shown in the following Equipment list Airplane Serial No Registration Dat...

Страница 88: ...FLIGHT MANUAL Doc No SP2006FMENKT 6 14 December 20 2006 Section 6 Weight and Balance Airplane Serial No Registration Date Description Type Part No Manufacturer Installed...

Страница 89: ...Lateral control 4 7 3 3 Rudder control 4 7 3 4 Elevator trim tab control 4 7 4 Controls in cockpit 5 7 5 Instrument panel 5 7 6 Inside and outside marking and placards 5 7 7 Landing gear and brakes 6...

Страница 90: ...12 2 Fuel selector 11 7 12 3 Fuel filter 11 7 12 4 Indication of fuel quantity 11 7 12 5 Fuel tank draining 12 7 13 Electrical system 13 7 13 1 Lighting 13 7 13 2 Electrical system scheme 13 7 14 Pit...

Страница 91: ...ddle part of the fuselage that is accessible after uncovering the single piece organic glass canopy The engine compartment in the front part of the fuselage is separated from the cockpit by the steel...

Страница 92: ...actuated by the control stick From the control stick the movement is transferred through the system of levers and pull rods to ailerons 7 3 3 Rudder control Rudder control is controlled by pedals of...

Страница 93: ...ating knob 10 Fuel selector if installed 11 Rudder control pedals 4 Cockpit heating canopy defog 12 Emergency parachute selector if installed system lever if installed 5 Hot air supply knob if install...

Страница 94: ...cylinders and brake pads By depressing the brake pedals compression of brake pumps occurs which generates pressure in brake circuit and hydraulic cylinders press the brake pads onto the brake disks B...

Страница 95: ...echanism The on groun adjustable composite 3 blade propeller WOODCOMP KLASSIC 170 3 R is standardly mounted on the engine ROTAX 912 ULS Other propeller type can be installed on customer s request see...

Страница 96: ...ometer Oil temperature on engine input is measured by the sensor located behind the oil pump Working range of oil thermometer is 120 300 F Colour code is stated in section 2 Oil pressure gauge Oil pre...

Страница 97: ...p 1 ensuring oil feeding from reservoir 4 located on the fire wall through the oil cooler 5 and the oil cleaner 6 to the lubricated points of engine The pressure sensor 2 is located behind the oil pum...

Страница 98: ...s distributed to the spark plugs through high voltage cables Ignition sequence of individual engine cylinders Ignition circuits are controlled by the ignition switch on the instrument panel Positions...

Страница 99: ...w the handle can be freely moved between LEFT and RIGHT position Safety button prevents unintentionally switch the selector to OFF position To move selector to OFF closed position it is necessary pull...

Страница 100: ...006 Section 7 Airplane and System Description in level flight and it takes approx 2 minutes to level fuel after transition from climb descent 7 12 5 Fuel tank draining Draining of the fuel tank is spe...

Страница 101: ...is pulled out Circuit beakers are listed in the Aircraft Maintenance and Inspection Procedures After switching Master switch on and by turning the ignition key to START position the starter is activa...

Страница 102: ...pressure is sensed through openings on the tube circumference System of pressure distribution to individual instruments are made by means of flexible plastic hoses Transparent draining reservoirs are...

Страница 103: ...nger The heat exchanger is located on the exchaust pipe collector Air from outside atmosphere is warmed up in the exhaust pipe collector and delivered through air hoses into the cockpit Hot air quanti...

Страница 104: ...FLIGHT MANUAL Doc No SP2006FMENKT 7 16 December 20 2006 Section 7 Airplane and System Description Intentionally left blank...

Страница 105: ...G SERVICING AND MAINTENACE 3 8 1 Introduction 3 8 2 Airplane inspection period 4 8 3 Modifications or airplane repairs 5 8 4 Road transport 5 8 4 1 Airplane towing 5 8 4 2 Airplane parking 6 8 4 3 Air...

Страница 106: ...FLIGHT MANUAL Doc No SP2006FMENKT 8 2 December 20 2006 Section 8 Airplane Handling Servicing and Maintenance Intentionally left blank...

Страница 107: ...vice bulletins Mandatory bulletins Information bulletins letters and further instructions Mandatory bulletins are especially important for keeping up airworthiness and the manufacturer considers them...

Страница 108: ...f the LSA airplane An owner of an LSA airplane shall ensure that any needed corrective action must be completed as specified in a notice or by the next scheduled annual inspection Should an owner oper...

Страница 109: ...Inspection Procedures of SPORTSTARPLUS 8 4 Road transport 8 4 1 Airplane towing It is possible to move the airplane on a short distance by holding the fuselage end in the position before the fin enven...

Страница 110: ...g out of hangar after termination of flight day or according to need Anchoring of the airplane is necessary for its protection against possible damage caused by wings and gusts For this purpose the ai...

Страница 111: ...part of fuselage can be supported by the rest located in the area of the skid Wings van be jacked by pushing on the wing from below in the area of the main spar It is necessary to avoid jacking by gra...

Страница 112: ...g airplane surface Residuum of oil and fat can be removed form the airplane surface excluding the canopy by suitable detergents posibbly by petrol The canopy only to be cleaned by washing with ample s...

Страница 113: ...06 S2006AOIUSS05 GPS COMM receiver KLX 135 Dec 20 06 S2006AOIUSS06 Flight clock LC 2 Dec 20 06 S2006AOIUSS07 Transceiver FILSER ATR 600 Dec 20 06 S2006AOIUSS08 GPS NAV COMM receiver GARMIN GNS 430 43...

Страница 114: ...FLIGHT MANUAL Doc No SP2006FMENKT 9 2 December 20 2006 Section 9 Supplements Instal Date Doc No Title of inserted supplement...

Страница 115: ...FLIGHT MANUAL Doc No SP2006FMENKT December 20 2006 9 3 Section 9 Supplements 9 3 Supplements inserted...

Страница 116: ...FLIGHT MANUAL Doc No SP2006FMENKT 9 4 December 20 2006 Section 9 Supplements Intentionally left blank...

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