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AIRCRAFT OPERATING INSTRUCTIONS FOR LIGHT SPORT

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1. 30 a EET i i I HH el CAE Example ER TH 2 HI Wind velocity 15 kts H NM AM Wind direction 55 ES ESSERE Aa I BE 2 2 Er EEE 3 HH HAN D E S o NS 3 HAS ba Cy i SATE og HHE 20 S PERTH A SY e UL ES o E S HN rth e 15 S E 9 ri S ES a D 2 5 he Z HHA ASAAN HAH E PAN L E Bi z O pa S a BERA o 5 80 l o TD E gt zm EES 0 OS JH 90 4 1 B E 5 100 E EH EMNE D oe Ara NHS HESSE ERG 7103 m 0 5 10 15 20 25 30 Crosswind component kts Figure 5 1 Influence of wind on take off and landing December 20 2006 ve lus Section 5 port R Performance LAA AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 5 3 7 Ceiling Service ceiling of SPORTSTAR gt 13 030 ft 5 3 8 Noise data Not measured December 20 2006 5 15 Section 5 lus Le Performance port d m AIRCRAFT OPERATING INSTRUCTIONS LAA Doc No SP2006AOIUS Intentionally left blank 5 16 December 20 2006 lu Le SportStak ue LAA AIRCRAFT OPERATING INSTRUCTIONS BENE Doc No SP2006AOIUS CONTENTS 6 WEIGHT AND BALANCE eene nnns 3 6 1 Introduction ss 3 6 2 Weight and Balance Record
2. Figure 7 1 Cockpit control elements 1 Control stick 8 Choke 2 Instrument panel 9 Master switch 3 Carburetter pre heating knob 10 Fuel selector 1f 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 installed 13 Flaps control lever 6 Throttle lever 14 Trim control lever 7 Ignition 15 Headset sockets 7 5 Instrument panel See section 9 supplements 7 6 Inside and outside marking and placards See Aircraft Maintenance and Inspection Procedures December 20 2006 7 5 Section 7 ms Aa System SportStar Je Description 7 7 7 7 1 7 7 2 7 8 7 9 AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Landing gear and brakes Landing gear The airplane is equipped with a sort of fixed nose landing gear Main landing gear legs are produced from composite spring Nose landing gear leg is welded from two pieces the tube and the yoke in which the nose wheel is mounted The nose landing gear is spring loaded by a rubber rope The nose wheel is steerable wheel control is coupled with rudder control by means of two pull rods Wheels can be fitted with fiber glass aerodynamic pants Brakes The SPORTSTAR airplane is equipped with dis
3. 3 4 4 Pre flight check 4 4 5 Normal procedures and checklist 8 4 5 1 Before engine starting 8 4 5 2 ENGNG SITU msi side orke ten a un 8 4 5 3 Before TAMING rca wan uae vate atus 10 O M PA 10 4 5 5 Before take off ooccconcconoccnconiconoccnoconooncnonocanonnncanonanons 10 256 TAKE A 12 AoT Oc ME 12 O 13 4 5 9 Pee 14 4 5 10 Before landing 14 4 5 11 Balked landing nannannonnnnnnennannnnnnnnnnnnennsnnnnnnnrnnrenrenrennenne 15 BOA NM 15 4 5 13 After landing nnn 16 4 5 14 Engine sbut oft ss 16 4 5 15 Airplane parking 17 lus Section 4 SportStar AIRCRAFT OPERATING INSTRUCTIONS oe Doc No SP2006AOIUS December 20 2006 4 1 Section 4 lus Nr Norma SportStar e Procedures LAX AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Intentionally left blank 4 2 December 20 2006 lu ection Le SportStar ur P LAA AIRCRAFT OPERATING INSTRUCTIONS e Doc No SP2006AOIUS 4 NORMAL PROCEDURES 4 1 Introduction Section 4 describes operations and recommended procedures for normal operation of the airplane Normal procedures following from system installation and optional equipment which require supplementation of these Instructions are shown in section 9 Supplements 4 2 Recommended speeds for normal procedures
4. lus Section 6 SportStar Weight and LAX Balance AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 6 6 Table of Static Moments CREW BAGGAGE FUEL Weight Moment 100 Weight Moment 100 Quantity Weight Moment 100 Ib Ib in lb bin USGAL Ib Ib in 0 0 0 0 0 0 0 0 0 0 0 0 100 21 5 2 0 9 1 0 6 0 16 120 25 7 4 1 7 2 0 12 0 32 140 30 0 6 2 6 3 0 18 0 48 160 34 3 8 3 4 40 240 64 180 38 6 10 4 3 5 0 30 0 80 200 42 9 12 5 1 6 0 36 1 96 220 47 2 14 6 0 7 0 42 1 113 240 51 5 16 6 8 8 0 48 1 i29 260 55 8 18 G 9 0 54 1 145 280 60 1 20 8 5 10 0 60 1 16 1 300 64 4 22 9 4 11 0 66 1 17 7 320 68 6 24 10 2 12 0 72 1 19 3 340 72 9 26 11 1 13 0 78 1 209 360 77 2 28 11 9 140 84 1 225 380 81 5 30 12 8 15 0 90 1 241 400 85 8 32 13 6 16 0 96 1 25 7 420 90 1 34 14 5 17 0 102 1 273 440 94 4 36 15 4 18 0 108 2 289 460 98 7 38 16 2 19 0 114 2 305 480 103 0 40 17 1 20 0 120 2 32 2 500 107 3 42 17 9 21 0 126 2 338 520 111 5 44 18 8 22 0 132 2 35 4 540 115 8 46 19 6 23 0 138 2 370 560 120 1 48 20 5 24 0 144 2 38 6 50 21 3 25 0 150 2 40 2 52 22 2 26 0 156 2 418 54 23 0 27 0 162 2 43 4 55 235 280 168 2 450 29 0 174 3 466 30 0 180 3 482 31 0 186 3 498 December 20 2006 6 9 Section 6 fus Mead SportStar Bal eS AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS EX 6 7 Airplane Lo
5. 3 3 3 Engine failure ee 3 3 3 1 Engine failure at take off run 3 3 3 2 Engine failure at take off ocooocccnnicnnconncccncocicononnnnnconanonanonos 3 3 3 3 Engine failure in flight 4 3 4 Engine starting at flight 4 3 5 Engine MEL 5 3 5 1 Fire on the ground 5 3 5 2 Fire during take off 5 Fe 6 3 6 Fire in the cockpit if manual extinguisher available MDA PP A 7 3 7 Gliding MEN Lune 7 3 8 Emergency landing ion 8 3 8 1 Emergency landing with non operating engine 8 3 8 2 Safety landing with engine operating 8 3 8 8 Landing with burst tire 9 3 8 4 Landing with damaged landing gear 9 3 9 Unintentional spin recovery 9 3 10 Other emergency procedures 10 3 10 1 Vibration 10 3 10 2 Carburettor mg 10 December 20 2006 3 1 Section 3 Emergency Procedures SportStar AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Ax December 20 2006 lu Le SportStar p P LAA AIRCRAFT OPERATING INSTRUCTIONS PEU AA Doc No SP2006AOIUS 3 EMERGENCY PROCEDURES 3 1 Introduction section 3 describes operations and procedures for emergency situation solutions that could possibly occur during airplane operation 3 2 Speeds for pe
6. 4 6 3 Permitted Payload Range 5 6 4 Operational Weight and Balance Computation 6 6 4 1 Computational PDrocecdure 6 6 5 Airplane Loading Schedule Chart 8 6 6 Table of Static Moments 9 6 7 Airplane Loading Graph 10 6 8 CG Moment Envelope eene nennen 11 6 9 Operational Weight and CG Envelope 12 610 Equipment LIS aia 13 December 20 2006 6 1 lu TI SportStar Le Bal SE AIRCRAFT OPERATING INSTRUCTIONS LAA Doc No SP2006AOIUS Intentionally left blank 6 2 December 20 2006 N T lus Section 6 SportSt R Weight and LAX Balance AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 6 WEIGHT AND BALANCE 6 1 Introduction This Section includes Weight and Balance Record of empty airplane 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 for weighing the airplane and the calculation method for establishing the permitted payload range are contained in the Aircraft Maintenance and Inspection Procedures for the SPORTSTAR Light Sport Aircraft December 20 2006 6 3 Section 6 Weight and Balance SportS
7. EVEKTOR AEROTECHNIK a s Letecka 1384 Tel 420572 537 111 LAA 686 04 Kunovice Fax 420 572 537 900 CZECH REPUBLIC email marketing evektor cz AIRCRAFT OPERATING INSTRUCTIONS FOR SportStar LIGHT SPORT AIRGRAFT Serial number Registration mark Document number SP2006AOIUS 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 the pilot and also contains supplementary information provided by the airplane manufacturer Evektor Aerotechnik a s This aircraft must be operated in compliance with the information and limitations stated in this manual Copyright 2006 EVEKTOR AEROTECHNIK a s lu Le SportStcir c LAA AIRCRAFT OPERATING INSTRUCTIONS HEN Doc No SP2006AOIUS CONTENTS 0 TECHNICAL INFORMATION eene nnn 3 0 1 Log of Revisions ss 3 0 2 List of Effective Pages eese 5 US AOLSECIONS roe E E 8 December 20 2006 0 1 Section 0 lus Len Technical port R Inf ti ER AIRCRAFT OPERATING INSTRUCTIONS LA Doc No SP2006AOIUS Intentionally left blank 0 2 December 20 2006 des ection Ze SponSt 27 Inf i AIRCRAFT OPERATING INSTRUCTIONS gt gt Doc No SP2006A01US 0 TECHNICAL INFORMATION 0 1 Log of Revisions All revisions or supplements to this manual except actual weighing data are issued in
8. KTAS 72 86 91 December 20 2006 5 11 Section 5 Performance SportStar AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Le LO 5 3 3 Endurance Conditions flaps retracted 0 carburetter preheating OFF airplane weight 1268 Ibs ambient air temperature ISA ENDURANCE AND RANGE 55 MCP 65 MCP 75 MCP MCP Max Continuous Altitude 2000 ft ISA pim Engine speed 1 h 14 1 18 6 20 5 25 1 Fuel consumption USgal h 3 7 4 9 5 4 6 6 UKgal h 3 1 4 1 4 5 5 5 km h 144 166 174 196 IAS knots 78 89 94 106 mph 90 103 108 122 km h 139 158 166 185 CAS mph 86 98 103 115 km h 143 163 171 191 TAS knots 77 88 92 103 mph 89 101 106 119 Endurance at 120 0 I h m 8 30 6 26 5 50 4 46 Range at 120 0 I km 31 7 USGAL NM 26 4 UKGAL miles Endurance at 100 0 I h m Range at 100 0 I km 22 0 UKGAL miles Endurance at 75 0 I h m Range at Endurance at Range at Endurance at Range at 25 0 135 5 5 UKGAL miles 155 December 20 2006 Ne AX 5 3 4 Balked landing climb 800 4 700 4 600 Rate of climb fpm 200 100 500 400 300 lus Section 5 po
9. December 20 2006 1 5 Section 1 General SportStar AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 1 43 Main technical data Wing Span Area MAC depth Wing loading Aileron area Flap area Fuselage length width height cockpit canopy max width Horizontal tail unit Span HTU Area Elevator area Vertical tail unit Height VTU Area Rudder area Landing gear Wheel track Wheel base Main and nose landing gear wheel diameter Ze 28 37 ft 112 7 sq ft 4 1 ft 10 76 Ibs sa ft 2 62 sq ft 5 60 sq ft 19 62 ft 3 55 ft 7 66 ft 3 87 ft 8 20 ft 20 88 sq ft 8 40 sa ft 4 07 ft 10 76 sq ft 4 31 sq ft 6 12 ft 4 43 ft 14 In December 20 2006 Len lus Section 1 e SportStcr SS LAA AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 1 4 4 Three view drawing 19 62 ft Figure 1 1 December 20 2006 1 7 Section 1 lus Le e portStcin 7 AIRCRAFT OPERATING INSTRUCTIONS LAA Doc No SP2006AOIUS 1 5 Definitions and abbreviations NOTE The abbreviations on placards in the airplane cockpit are printed in BOLD CAPITAL LETTERS in the text of this Aircraft Operating Instructions ACCU accumulator ALT ENC encoding altimeter ATC air traffic control bar bar 1 bar 100 kPa BEACON anti collision beacon E Celsius degree CAS calibrated airspeed CLOCK aircraft clock ft foot 1 ft 0 305 m GPS global positioning syste
10. NOTE It is possible to start the engine by means of the starter within the whole range of operation speeds as well as flight altitudes The engine started up immediately after switching the ignition to START position If the engine is shut down the altitude loss during engine starting can reach up to 1000 ft Gliding speed 57 KIAS 66 mph IAS Altitude check Master switch ON Unnecessary electrical equipment switch off FUEL SELECTOR LEFT Choke as needed December 20 2006 lu Le SportStair p LAA AIRCRAFT OPERATING INSTRUCTIONS EEN Doc No SP2006AOIUS 7 THROTTLE lever idle choke opened or increased idle choke closed The propeller is rotating 8 Ignition BOTH The propeller is not rotating 9 Ignition START 10 If engine starting does not occur increase gliding speed up to 108 KIAS 124 mph IAS see NOTE so that 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 the ground 1 FUEL SELECTOR OFF 2 Brakes brake 3 THROTTLE lever full 4 HOT AIR knob if installed push After the engine stops 5 Ignition OFF 6 Master switch OFF 7 Airplane leave 8 Manual extinguisher if available use 3 5 2 Fire during take off 1 FUEL SELECTOR OFF 2 THROTTLE lever full 3 Airspeed 63 KIAS 73 mph IAS 4 HOT AIR knob if in
11. Red line 146 168 Maximum speed for all operations VNE December 20 2006 AC LA 2 4 Powerplant Engine manufacturer Engine type Power Engine speed Cylinder head temperature Oil temperature Oil pressure Fuel pressure Fuel grades Oil grades Reducer gear ratio Propeller manufacturer Propeller type Propeller diameter Maximum prop speed SportStar AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Section 2 Limitations Bombardier Rotax GMBH ROTAX 912ULS maximum take off maximum continuous maximum take off maximum continuous idle maximum maximum optimum operation maximum minimum optimum operation minimum see 2 13 see 2 14 2 43 1 WOODCOMP s r o KLASSIC 170 3 R 100 HP 93 8 HP 5800 RPM max 5 minutes 5500 RPM 1400 RPM 275 F 266 F 190 230 F 102 PSI 12 PSI 29 73 PSI 2 2 PSI 3 blade composite on ground adjustable 68 in 2600 RPM NOTE If installed a different propeller type see section 9 Supplements for propeller limitations December 20 2006 Section 2 lus Len Limitations port R AIRCRAFT OPERATING INSTRUCTIONS LA Doc No SP2006AOIUS 2 5 Powerplant instrument marking The colour code of instruments is shown in the following table Red line Green arc Yellow arc Red line Instrument Units Lower Normal Caution Upper limit operation rang
12. letters and further instructions Mandatory bulletins are especially important for keeping up airworthiness and the manufacturer considers them mandatory although they do not come into effect before Airworthiness Directive is issued by aviation authority of user s country All correspondence with the airplane manufacturer distributor or service center must contain the airplane serial number The airplane serial number is shown on the title sheet of this Instructions and on the production plate behind the rest of pilot seats The manufacturer delivers along with aircraft SPORTSTAR the Aircraft Operating Instructions AOI and the Aircraft Maintenance and Inspection Procedures AMIP Qualification requirements to perform maintenance and repairs are mentioned in the AMIP item 4 1 1 Owner Operator Responsibilities Each owner operator of an LSA airplane shall read and comply with the maintenance and continued airqworthiness information and isntructions provided by the manufacturer December 20 2006 8 3 Section 8 lu Airplane Handling SportStar Le Servicing and Maintenance AIRCRAFT OPERATING INSTRUCTIONS LAA Doc No SP2006AOIUS Each owner operator of an LSA airplane shall be responsible for providing the manufacturer with current contact information where the manufacturer may send the owner operator supplemental notification bulletins The owner operator of an LSA airplane shall be responsible for noti
13. 2006 0 7 Section 0 lus Nr Technical SportSt R Information LAX AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 0 3 AOI Sections section GENERAL 1 LIMITATIONS 2 EMERGENCY PROCEDURES 3 NORMAL PROCEDURES 4 PERFORMANCE 5 WEIGHT AND BALANCE 6 AIRPLANE AND SYSTEM DESCRIPTION 7 AIRPLANE HANDLING SERVICING AND MAINTENANCE 8 SUPPLEMENTS 9 0 8 December 20 2006 fu i Je SporlStk um AA AIRCRAFT OPERATING INSTRUCTIONS Do No SP2006AOIUS CONTENTS T GENERAL nono dida 3 1 4 Ile vele ei Le TEE 3 1 2 Certification E TC A 1 2 1 Data se 110 EEE 4 1 3 Warnings Cautions notes 4 1 4 Descriptive data ratas 5 1 4 1 Airplane description 5 1 42 TE EE EN AE 5 1 4 3 Main technical data 6 1 4 4 Three view drawing 7 1 5 Definitions and abbreviations es 8 December 20 2006 1 1 Section 1 lus Len SportSidk N7 AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Intentionally left blank 1 2 December 20 2006 lu i Je SportStiR 2 AA AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 1 GENERAL 1 1 Introduction PARTICIPANT S RESPONSIBILITY There are inherent risks in participating in aviation activities these risks are significant up to and potentially including death Operators and passengers of recreational aviation aircraft by participation accep
14. 250 200 Conditions engine flaps Carburetter preheating OFF airplane weight 1268 lbs ambient air temperature ISA SportStar Rate of Climb Woodcomp Klassic 170 3 R propeller Rotax 912 ULS engine ie AX maximun take off power retracted 0 90 December 20 2006 Un lus Section 5 port t R Performance PA AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Best rate of climb for various altitudes is mentioned in the following table smell bouton ur speed of climb Hp ft ISA KIAS lAS mph ft min o 61 71 880 1000 61 70 80 gt 5000 60 69 59 6000 60 69 540 7000 60 69 480 v 8000 60 69 420 9000 59 68 370 gt 1000 59 68 310 December 20 2006 5 9 Section 5 Performance 9 3 9 3 1 Doc No SP2006AOIUS Additional information Cruise Conditions flaps SportStar AIRCRAFT OPERATING INSTRUCTIONS Xd retracted 0 carburetter preheating OFF airplane weight 1268 lbs ambient air temperature ISA SVO peedsure payesqued e LO e LO E FF 8 8 8 8 E R 8 SB 0 bre 0089 00 S 0095 N J ory OOGG VIG 00 S A D J 5 Vi 00 S 2 Ment I 0075 E VI A c 26 N V oo
15. 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 Vy flaps retracted 0 63 KIAS 73 mph IAS Best angle of climb speed Vx flaps in take off pos 15 53 KIAS 61 mph IAS Best angle of climb speed Vx flaps retracted 0 55 KIAS 63 mph IAS 4 2 2 Landing Approaching speed for normal landing flaps in landing position 50 60 KIAS 69 mph IAS 4 3 Assembly and disassembly Description of assembly and disassembly is given in the SPORTSTAR Aircraft Maintenance and Inspection Procedures December 20 2006 4 3 Section 4 lus Le E portStci 7 P d PO AIRCRAFT OPERATING INSTRUCTIONS LA Doc No SP2006AOIUS 4 4 Pre flight check Carry out pre flight check according to the following procedure Figure 4 1 Scheme of airplane preflight check CHECK BEFORE PRE FLIGHT CHECK THAT IGNITION IS SWITCHED OFF NOTE The word condition used in procedures of pre flight check means visual check of surface damage deformation scratches attrition corrosion icing or other effects decreasing flight safety 4 4 December 20 2006 Ze December 20 lus Section 4 SportStar AIRCRAFT OPERATING INSTRUCTIONS is Doc No SP2006AOIUS Left landing gear leg check e landing gear leg attachment and condition e landing gear wheel condition e tire co
16. 67 Dec 20 06 416 Dec20 06 68 Dec 20 06 417 Dec20 06 69 Dec 20 06 418 Dec20 06 610 Dec 20 06 Po e 20 06 o 612 Dec 20 06 po eg Dec 20 06 Po Dec 20 06 5 51 Deca 1 5 amp 2 Dec2006 53 Dewo 1 1 54 Dec2006 55 Dec2006 1 1 1 5 amp 6 Dec2006 57 Dec2006 1 1 58 Dec2006 1 1 aa Dec2006 510 Devo 1 1 po 311 Dea 1 Lt _ _ _ EE 0 6 December 20 2006 lu Le SportStcir c LAA AIRCRAFT OPERATING INSTRUCTIONS EEN Doc No SP2006AOIUS a 8 8 1 Dec 20 06 o pp 82 Dec20 06 pp ss Dec20 06 o au Dec20 06 es Dec20 06 ff ess Dec20 06 7 74 Dec20 06 8 amp 7 Dec20 06 72 Dec20 06 8 8 Dec20 06 1 73 Dec2006 Y 1 74 Dec20 06 d 1 75 Dec20 06 r6 Dec2006 1 77 Dec20 06 r8 Dec20 06 79 Dec20 06 9 ai Dec20 06 710 Dec20 06 92 Dec20 06 7 11 Dec20 06 93 Dec 20 06 712 Dec20 06 94 Dec20 06 713 Dec20 06 __ 7414 Dec20 06 715 Dec2006 716 Dec20 06 IS O LI LL LL LI LL LL LI LL IL LI LL LL LL ILL LI LL LL LI LL LL LL LL ll LI LL LL LIKA gt December 20
17. Dec20 06 05 Dec20 06 27 Dec20 06 06 Dec20 06 28 Dec20 06 07 Dec20 06 29 Dec20 06 08 Dec20 06 2 10 Dec 20 06 o zm Dec20 06 1 l zg Dee 20 06 LL LL LL LL LL ll E NUM 1 1 1 Dec 20 06 1 2 Dec 20 06 1 3 Dec 20 06 3 3 1 Dec 20 06 1 4 Dec 20 06 3 2 Dec 20 06 1 5 Dec 20 06 ds Dec 20 06 1 6 Dec 20 06 3 4 Dec 20 06 1 7 Dec 20 06 3 5 Dec 20 06 1 8 Dec 20 06 3 6 Dec 20 06 1 9 Dec 20 06 3 7 Dec 20 06 110 Dec 20 06 3 8 Dec 20 06 3 9 Dec 20 06 3 10 Dec 20 06 EEE EE el December 20 2006 0 5 Section 0 lus Len am SportStak e Information LAX AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS e Section Page Date Section Page Date 4 41 Dec20 06 5 5 12 Dec20 06 4 2 Dec20 06 543 Dec20 06 43 Dec20 06 5 14 Dec20 06 44 Dec20 06 515 Dec 20 06 45 Dec20 06 516 Dec 20 06 46 Dec2006 1 1 47 Dec2006 48 Devo 1 1 49 Dec20 06 6 6 1 Dec 20 06 410 Dec20 06 62 Dec 20 06 41 Dec20 06 63 Dec 20 06 412 Dec20 06 64 Dec 20 06 413 Dec20 06 65 Dec 20 06 414 Dec20 06 66 Dec 20 06 445 Dec20 06
18. NEUTRAL Fuel gauge indicator check on fuel quantity FUEL SELECTOR check LEFT CARBURETTOR PREHEATER if installed check function then OFF NOTE Ift CARBURETTOR PREHEATER is switched ON then engine RPM drop reaches approximately 50 RPM Engine instruments check Flight instruments check Radiostation avionics check set Ignition check BOTH Choke close in inserted position Master switch check ON oafety harnesses tighten up Canopy closed Transponder if installed ON or ALT December 20 2006 4 11 Section 4 lus Le Normal SportStar Procedures LAX AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 4 5 6 Take off 1 THROTTLE lever max take off power 2 During take off run smootly lighten up the nose landing gear until airplane take off occurs 3 Airpeed 56 KIAS 65 mph IAS 4 Brakes brake 5 After reaching 150 ft set flaps to retracted pos 0 6 Trim as necessary TAKE OFF IS PROHIBITED IF ENGINE RUNNING IS IRREGULAR e IF CHOKE IS OPEN e IF VALUES OF ENGINE INSTRUMENTS ARE NOT WITHIN THE REQUIRED RANGE 4 5 7 Climb 1 THROTTLE lever max continuous power 2 Airspeed Vy 63 KIAS 73 mph IAS for the best rate of climb or Vx 55 KIAS 63 mph IAS for the best angle of climb 3 Engine instruments check 4 Trim as necessary 4 12 December 20 2006 Ne lus Section 4 NT SportSteir LAA AIRCRAFT OPERATING INSTRUCTIONS Greg Doc No SP2006AOIUS 4 5 8 Cruise 1 THROTTLE lever as nec
19. Not used Dec 20 06 S2006AOIUSS019 Stall warning system ACI type T1b Dec 20 06 Intercom PCD7100 I December 20 2006 Section 9 lus Le Supplements port R AIRCRAFT OPERATING INSTRUCTIONS LAA Doc No SP2006AOIUS Instal Date Doc No Title of inserted supplement 9 2 December 20 2006 Lee lus Section 9 port R Supplements LAA AIRCRAFT OPERATING INSTRUCTIONS DO No SP2006AOIUS 9 3 Supplements inserted December 20 2006 9 3 Section 9 lus Le Supplements portSt R AIRCRAFT OPERATING INSTRUCTIONS LA Doc No SP2006AOIUS Intentionally left blank 9 4 December 20 2006
20. Un lus Section 7 SportStar Airplane ie ea LAA AIRCRAFT OPERATING INSTRUCTIONS FOR Doc No SP2006AOIUS 7 15 Supplementary equipment 7 15 1 Ventilation and heating system Cockpit ventilation is ensured by two sliding windows located on the tilting canopy Cocpit heating is ensured by hot air from the heat exchanger 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 quantity is regulated by the flap which is controlled by the HOT AIR knob on the instrument panel The cockpit heating system can be equipped with a windshield blowing system 7 16 Navigation and communication equipment Description of operation of navigation and communication equipment see section 9 Supplements December 20 2006 7 15 Section 7 dus he reen System SportStar D ipti uM AIRCRAFT OPERATING INSTRUCTIONS LAA Doc No SP2006AOIUS Intentionally left blank 7 16 December 20 2006 Nin lus Section 8 SportStar Airplane Handi LA AIRCRAFT OPERATING INSTRUCTIONS LEI Doc No SP2006AOIUS CONTENTS 8 AIRPLANE HANDLING SERVICING AND MAINTENACE ona 3 8 1 Introduction ss 3 8 2 Airplane inspection period 4 8 3 Modifications or airplane repairs 5 8 4 Road t
21. 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 means of black vertical line on the margin of page and the revision number and date will be shown on the bottom margin of page f o dd u unu u u u _ _0 e V k v _ u u Um a gt RRTw lt t ns Rev Affected Affected Date Appro Date Date of Sign No Section Pages Insertion I EE EE December 20 2006 0 3 Section 0 lus Nu pus SportStci 7 Information LAX AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Rev Affected Affected Date Appro Date Date of Sign 0 4 December 20 2006 lu Le SportStcir c LAA AIRCRAFT OPERATING INSTRUCTIONS EEN AA Doc No SP2006AOIUS 0 2 List of Effective Pages p M M Section Page Date Section Page Date T epge 2 21 Dec20 06 fof z Dec20 6 o 01 Dec20 06 23 Dec20 06 02 Dec20 066 24 Dec 20 06 03 Dec20 06 25 Dec 20 06 04 Dec20 06 26
22. framework is composed of metal structure on which the organic glass canopy is fixed by bolts The canopy is attached to the fuselage in the front part by two swivel pins by means of which it can be folded up forwards In order to make opening easier the actual weight of canopy is balanced by two gas struts besides the canopy is provided with holders on the lower framework for easier handling The canopy is provided with the lock in the rear upper part of framework for locking 7 11 Power unit 7 11 1 General The engine ROTAX 912 ULS 100 hp is used to power SPORTSTAR 5 airplane ROTAX 912 ULS is a four cylinder four stroke engine with opposite cylinders central cam shaft and OHV valve mechanism 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 sec 9 for detailed information 7 11 2 Engine control Engine power is controlled by means of THROTTLE lever which is located in the middle of the instrument panel and which controls engine power range from idle up to maximum take off Engine power controller is mechanically interconnected with the flap on carburetters If the lever is fully pushed in then this position corresponds to maximum engine power If the lever is fully pulled out then this position corresponds to idle Rapid changes in engine power setting can be made by pressi
23. ipti TOTUM AIRCRAFT OPERATING INSTRUCTIONS LAA Doc No SP2006AOIUS 7 12 el SNS ICONS a nat ste ete ess es 10 7 12 1 Fuel tanks nennen nnne nnns 10 7 12 2 Fuel A 11 12 FANT T 11 7 12 4 Indication of fuel quantity oocconncoccconconncocncocnnnnonnnonnnnnnos 11 7 12 5 Fuel tank draining anernrennrrnnrvnnrvnnvnnrvnnrnnnvnnnnnnrnnnennnnnnennne 12 113 Blecthecal Syste Mecon 13 A RE 13 7 13 2 Electrical system scheme 13 7 14 Pitot static system eese 14 7 15 Supplementary equipment 15 7 15 1 Ventilation and heating system 15 7 16 Navigation and communication equipment 15 7 2 December 20 2006 Ne lus Section 7 SportStar Airplane hun cue de LAA AIRCRAFT OPERATING INSTRUCTIONS oe Doc No SP2006AOIUS 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 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
24. mph IAS carry out December 20 2006 lu Le SportStair ol LAA AIRCRAFT OPERATING INSTRUCTIONS ee Doc No SP2006AOIUS 3 8 3 Landing with burst tire CAUTION WHEN LANDING AT HOLDING KEEP THE WHEEL WITH BURST TIRE ABOVE THE GROUND AS LONG AS POSSIBLE BY MEANS OF AILERONS IN CASE OF NOSE WHEEL BY MEANS OF ELEVATOR 1 At running hold airplane direction by means of foot control and brakes 3 8 4 Landing with damaged landing gear 1 In case of nose landing gear damage touch down at the lowest possible speed and try to 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 Unintentional spin recovery NOTE The airplane has not when using normal techniques of pilotage tendency to go over to spin spontaneously otandard procedure of recovery from spin 1 THROTTLE lever idle 2 Control stick ailerons neutral position 3 Pedals kick the rudder pedal push against spin rotation direction 4 Control stick push forward and hold it there until rotation stops 5 Pedals immediately after rotation stopping set the rudder to neutral position 6 Control stick recover the diving December 20 2006 3 9 i lu s SportStar Ax Procedures 3 10 AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS CAUTION ALTITUDE LOSS PER ONE TURN AND RECOVERING FROM THE SPIN IS 500
25. 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 soar 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 December 20 2006 7 3 Section 7 ms Aa System SportStar Je Description 7 3 7 3 1 7 3 2 7 3 3 7 3 4 AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Control Airplane control consists of ailerons elevator and rudder Directional control is connected by means of pull rods with nose landing gear control Main landing gear brakes are controlled by pedals of directional co
26. 7 140 132 145 137 150 141 155 146 160 151 165 155 168 158 December 20 2006 5 5 i lu SportSicar Ax AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 5 2 2 Stall speeds Conditions wing level stall engine at idle power turning flight stall engine at 75 max continuous power airplane weight 1268 lbs NOTE The stated stall speeds are valid for all flight altitudes Altitude losses shown in the table present max values determined on the basis of flight tests using average piloting technique 575 kg Flaps Stall speed Altitude loss 1268 Ib position KIAS KCAS ft Retracted 0 43 45 Take off 159 41 43 Landing 50 38 40 Retracted 0 46 49 Take off 15 44 46 200 Landing 50 41 43 Wing level flight Turn flight coordinated turn 30 bank 575 ko Flaps Stall speed n Sun loss 1268 lb position IAS mph CAS mph np Retracted 0 50 52 Wing level flight Take off 15 Li 47 49 200 Landing 50 44 46 200 T fligh dinated 9 ud s paw Take off 159 81 83 Landing 50 47 48 5 6 December 20 2006 Section 5 Performance SportStar AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Ze 5 2 3 Take off distance Conditions engine flaps max take off power Take off 15 carburetter preheating OFF airplane weight 1268 lb
27. AFT OPERATING INSTRUCTIONS Section 9 Supplements Doc No SP2006AOIUS 9 SUPPLEMENTS 9 1 Introduction This section contains the appropriate supplements necessary to safely and efficiently operate the airplane when equipped with various optional systems and equipment not provided with the standard airplane 9 2 List of inserted supplements Instal Dec 20 06 S2006AOIUSS01 Title of inserted supplement Transceiver KY97A Dec 20 06 S2006AOIUSS02 Intercom PM 1000 Dec 20 06 S2006AOIUSS03 Transponder KT76A Dec 20 06 S2006AOIUSS04 Airplane description of S N Dec 20 06 52006AOIUSS05 GPS COMM receiver KLX 135 Dec 20 06 52006AOIUSS06 Flight clock LC 2 Dec 20 06 52006AOIUSS07 Transceiver FILSER ATR 600 Dec 20 06 52006AOIUSS08 GPS NAV COMM receiver GARMIN GNS 430 430A Dec 20 06 52006AOIUSS09 Transponder ATC GARMIN GTX 327 Dec 20 06 S2006AOIUSS010 PS ENGINEERING INCORPORATED S2006AOIUSS011 Rocket activated parachute rescue system Magnum Speed Soft 650 Dec 20 06 S2006AOIUSS012 Horizon RCA 26 Dec 20 06 S2006AOIUSS013 Float operation CZAW 1150 Dec 20 06 S2006AOIUSS014 Horizon LUN 1202 Dec 20 06 S2006AOIUSS015 Towing gear Dec 20 06 S2006AOIUSS016 Pitot tube heating Dec 20 06 S2006AOIUSS017 Emergency Locator Transmitter AK 450 S2006AOIUSS018
28. EFLECTION OF THE NOSE WHEEL IS 10 AT MANUAL ENGINE STARTING GRASP THE PROPELLER BLADE AREA I E NOT ONLY PROPELLER EDGE Airplane parking It is the most suitable solution to place the airplane into a hangar possibly into another covered room with stable temperature good venting low humidity and dust free environment In case of parking out of the hangar it is necessary to anchor the airplane and at long term parking to cover the canopy possibly the whole airplane with suitable tarpaulins Airplane anchoring The airplane is anchored at parking 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 airplane is equipped with fixing eyes on the lower side of wings Procedure 1 Check of fuel selector off position of all switches ignition and master switch Lock manual control e g by using safety belts Close vent windows Close and lock the cockpit canopy 0O RR N Anchor the airplane to the ground by means of cables pulled through fixing eyes which are located on the lower side of wings Further it is necessary to anchor the nose landing gear NOTE In case that long term airpplane anchoring is supposed namely in winter period it is suitable to cover the canopy eventually the whole airplane by appropriate tarpaulins which must be properly secured to the air
29. Modifications or airplane repairs All airplane repairs and modifications of airplane must be carried out by qualified personnel in an approved service center see AMIP item 4 1 1 Before any repairs modification is made to the aircraft consult the Civil aviation authority of the country in which the airplane is registered to assess effect of the repair modification on the airworthiness Basic repairs of airplane are described in the Aircraft Maintenance and Inspection Procedures of SPORTSTARFS 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 enventually by holding the root part of wings The hand towing bar can be used for airplane relocation which will be fastened to the nose wheel axis To turn the airplane on the spot push on the fuselage end part in the area before the fin lift the nose wheel and turn the airplane in required direction SWITCH OFF IGNITION BEFORE GROUND HANDLING WITH THE AIRPLANE CAUTION AVOID EXCESSIVE PRESSURES ON THE AIRFRAME STRUCTURE ESPECIALLY ON THE WING TIPS HTU VTU ETC WHEN HANDLING THE AIRPLANE BY MEANS OF THE TOWING BAR PROPELLER BLADES MUST BE SET TO HORIZONTAL POSITION December 20 2006 8 5 Section 8 lus Airplane Handling SportStar LA Servicing and Maintenance AIRCRAFT OPERATING INSTRUCTIONS 8 4 2 8 4 3 Doc No SP2006AOIUS MAXIMUM D
30. NS LAA Doc No SP2006AOIUS 6 9 Operational Weight and CG Envelope SportStar US Operational Weight and CG Envelope 1300 1280 1260 1 1240 1220 1 1200 1180 1 1160 1140 1 1120 1 1100 1080 1060 1040 1 1020 1000 980 960 1 940 920 1 900 880 1 860 840 1 820 800 780 760 740 720 700 Loaded Airplane Weight Ib 18 19 T T CN co ka LO c RD o Q N N N N N N N N m co 20 21 32 33 34 35 36 Loaded Airplane CG position MAC 6 12 December 20 2006 lu Le SportStak ue Bal LAN AIRCRAFT OPERATING INSTRUCTIONS per DOC No SP2006AOIUS 6 10 Equipment List The equipment installed in the airplane of particular serial number is shown in the following Equipment list Airplane Serial Registration Date No Description Type Part No Manufacturer Installed December 20 2006 6 13 Section 6 Weight and Balance SportStar AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Le LO Airplane Serial Registration Date No Description Type Part No Manufacturer Installed 6 14 Dece
31. P2006AOIUS NOTE It is not recommended to fully tank the fuel tanks Due to fuel thermal expansion keep about 2 11U S gallons of free space in the tank to prevent fuel bleed through the vents in the wing tips thus 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 Premium plus AVGAS 100 LL Due to higher lead content in AVGAS the wear of valve seats and deposits in the combustion chamber and lead sediments in the lubrication system will increase Therefore use AVGAS only if you encouter problem with vapour lock or if the other fuel types are not available For other suitable fuel types refer to the engine Operator s Manual NOTE Use only fuel suitable for the respective climatic zone Risk of vapour formation if using winter fuel for summer operation 2 14 Oil Performance classification SF SG according to API Oil volume minimum 0 53 U S gallons maximum 0 79 U S gallons 2 15 Maximum number of passengers Maximum number of passengers including pilot 2 December 20 2006 2 9 i lu ne SportStar Le AIRCRAFT OPERATING INSTRUCTIONS LAA Doc No SP2006AOIUS 2 16 Other limitations SMOKING IS PROHIBITED on the airplane board PASSENGER NOTICE This aircraft conforms to ASTM Consensus Standards of airworthiness developed and maintained by the aviation
32. RUCTIONS Doc No SP2006AOIUS Intentionally left blank 1 10 December 20 2006 LA CONTENTS 2 HIMA TIONS gt 3 ZN Tu d ET EE 3 22 Ee 3 2 3 Airspeed indicator marking 4 2 4 For si nr bri Bniiairetesusieeseni sape ped lt a Ud 5 2 5 Powerplant instrument marking 6 2 6 Miscellaneous instrument marking 6 KS af VM 6 20 ETT 7 2 9 Approved manoeuvres arrarnnvnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnunnunne 7 2 10 Manoeuvring load factors 7 2 11 FIG CREW Lanes nisjene 7 212 KINAS OF OPSF NON ais 8 21 A 8 214 We E H 2 15 Maximum number of passengers H SL Welle E 10 2 17 Limitation placards 10 lu Le SportStcir AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS December 20 2006 2 1 Section 2 Limitations SportStar AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Intentionally left blank Ax December 20 2006 lu Le SportStcir AA AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 2 LIMITATIONS 2 1 Introduction Section 2 contains operation limitation instrument marking and basic placards necessary for safe operation of airplane and its engine standard Systems and equipment Limitation for optional
33. THROTTLE lever idle 2 Touch down on main landing gear wheels carry out 3 Brakes after nose landing gear wheel touch down as necessary December 20 2006 4 15 Section 4 lus Nr Norma SportStar e Procedures LAX AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 4 5 13 After landing 1 Flaps 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 Radiostation avionics OFF 5 Other electrical equipment OFF 6 Ignition OFF 7 BEACON if installed OFF 8 Master switch OFF 4 16 December 20 2006 Ze lus Section 4 SportStar 4 5 15 Airplane parking jm 2 3 AIRCRAFT OPERATING INSTRUCTIONS Hoodies Doc No SP2006AOIUS Ignition check OFF Master switch check OFF FUEL SELECTOR OFF Pull the safety button on the fuel selector turn the handle to the OFF position and then release safety button Now the handle is blocked in the OFF position Safety button prevents unintentionally switch the selector from the OFF position PARKING BRAKE handle if installed brake as necessary Canopy close lock as necessary NOTE It is recommended to use parking brake if installed for short time parking only between flights during a flight day After ending the flight day or at low temperatures of ambient air do not use parking brake but use the w
34. UBSEQUENT LOSS OF POWER PERFORM DESCENDING AT INCREASED IDLE AND CHECK OBSERVANCE OF THE ALLOWED VALUES ON ENGINE INSTRUMENTS 4 5 10 Before landing 2 FUEL SELECTOR LEFT 3 Engine instruments check 4 Brakes check by depressing pedals 5 Safety harnesses tighten up 6 Free area of landing check 1 Fuel quantity check CAUTION FUEL GAUGES DISPLAY TRUE FUEL QUANTITY ONLY ON GROUND AND IN A LEVEL FLIGHT TO READ TRUE FUEL QUANTITY AFTER TRANSITION FROM CLIMB DESCENT WAIT APPROX 2 MINUTES TO FUEL TO LEVEL 7 CARBURETTOR PREHEATER if installed ON December 20 2006 CARBURETTOR PREHEATER if installed as necessary lu ection Le SportStar M LAA AIRCRAFT OPERATING INSTRUCTIONS ee AAA Doc No SP2006AOIUS 8 Approaching speed 59 KIAS 68 mph IAS 9 Flaps take off pos 15 10 Trim as necessary 11 Parking brake if installed check for lever down CAUTION PARKING BRAKE MUST BE RELEASED LEVER DOWN TO PREVENT LANDING WITH BRAKED WHEELS FINAL 1 Flaps landing 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 Airspeed 56 KIAS 65 mph IAS 4 Flaps in 150 ft retracted pos 0 5 Trim as necessary 6 THROTTLE lever max continuous power 7 Instruments check 8 Climb at airspeed 63 KIAS 73 mph IAS 4 5 12 Landing 1
35. UP TO 1000 FT Other emergency procedures 3 10 1 Vibration 3 10 2 If abnormal vibrations occur on the airplane then 1 Set engine RPM to the mode in which the vibrations are the lowest 2 Land on the nearest possible airport possibly perform safety landing according to par 3 8 2 Safety landing Carburettor icing Carburettor icing happens when air temperature drop in the carburettor 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 icing shows itself by engine power decreasing and by engine temperature increasing Hecommended procedure for engine power regeneration is as follows 1 CARBURETTOR PREHEATER if installed ON 2 THROTTLE lever set idle and cruising power again NOTE Ice coating in the carburettor should be removed by decrease and reincrease of engine power 3 If the engine power is not successfully increased then carry out landing at the nearest suitable airport or if it is not possible carry out precautionary landing according to par 3 8 2 Precautionary landing December 20 2006 Ze CONTENTS d NORMAL PROCEDURES 1 erre eren ena nna nana 3 AOC E 3 4 2 Recommended speeds for normal procedures 3 4 2 1 Take off ss 3 A O UA 3 4 3 Assembly and disassembly
36. ading Graph SportStar P Loading Graph 500 480 460 440 Crew 420 400 380 360 340 320 300 280 260 240 220 200 180 AT 30 ade em noble Lei Luet ET eer Ee ees Dala 4 25 140 P 120 20 100 l 15 80 19 Load Weight Ib 60 40 20 Ee T aba Baggage Fuel quantity USGAL 85 I 90 LO e Lo o LO o LO o LO o co t t LO LO ce ce r N 00 Load Moment 100 Ib in LO o N ceo 20 6 10 December 20 2006 a lus Section 6 e SportStar Bal PA AIRCRAFT OPERATING INSTRUCTIONS x Doc No SP2006AOIUS 68 CG Moment Envelope SportStar 5 CG Moment Envelope 1300 1280 1 1260 1240 1 1220 1200 1 1180 1160 1 1140 1120 1 1100 4 1080 1060 1040 1 1020 1000 980 960 1 940 920 1 900 1 880 860 1 840 4 820 4 800 780 1 760 740 720 700 1 Loaded Airplane Weight Ib 50 60 70 eo e e e e eo o e Q o eo 00 O e T N m t LO ce N 00 pie E 190 200 210 220 Loaded Airplane Moment 100 Ib in December 20 2006 6 11 Section 6 lus en Weight and port TGR Bal per AIRCRAFT OPERATING INSTRUCTIO
37. community under ASTM Technical Committee F37 PASSENGER WARNING This aircraft was manufactured in accordance with Light Sport Aircraft airworthiness standards and does not conform to standard category airworthiness requirements 2 17 Limitation placards The following placards are located on the instrument panel iN Ur The following placards are located on the the tilting canopy PASSENGER NOTICE THIS AIRCRAFT CONFORMS TOASTM CONSENSUS STANDARDS OF AIRWORTHINESS DEVELOPED AND MAINTAINED BY THE AVIATION COMMUNITY UNDER ASTM TECHNICAL COMMITTEE F37 PASSENGER WARNING THIS AIRCRAFT WAS MANUFACTURED IN ACCORDANCE WITH LIGHT SPORT AIRCRAFT AIRWORTHINESS STANDARDS AND DOES NOT CONFORM TO STANDARD CATEGORY AIRWORTHINESS REQUIREMENTS The following placards is located in the baggage compartment MAX 55 Ibs 2 10 December 20 2006 Ne AX SportStar Section 2 Limitations AIRCRAFT OPERATING INSTRUCTIONS Do No SP2006A0IUS ly The following placards are located on the tilting canopy This Light Sport Aircaft has been approved only for VFR day flights under no icing conditions Aerobatics and intentional spins are prohibited AIRSPEED IAS Never exceed Manoeuvring Max Flap Extended Stalling Never exceed Manoeuvring Max Flap Extended Stalling ENGINE SPEED Max Take off max 5 min Max Continuous Idling Unusable quantity of fuel 0 5 USgal or This airplane has been ap
38. curing the rudder pedals see section 7 3 3 if installed adjustable rudder pedals RIGHT AND LEFT PEDAL OF RUDDER CONTROL MUST BE SET TO THE SAME POSITIONS AND WELL SECURED Aircraft Operating Instructions and other required documents check on completness and validity December 20 2006 4 7 Section 4 lus Nr Norma SportStar e Procedures LAX AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 4 5 Normal procedures and checklist 4 5 1 Before engine starting 1 Pre flight check and check on weight and centre of gravity position done 2 Safety harnesses check fasten 3 Control stick free 4 Rudder pedals free 5 Wing flaps function check 6 Trim tab function check 7 PARKING BRAKE handle if installed release brakes 8 Brakes function check 9 AVIONICS SWITCH 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 button on the fuel selector turn the handle to the left and then release safety button Now the handle can be freely moved between left and right position Safety button prevents unintentionally switch the selector to OFF position 4 Electric fuel pump if installed ON 5 THROTTLE lever idle 6 Choke as necessary open by pulling up and lock by turning 7 Space in the propeller area free 8 BEACON if installed ON if necessary 9 Brakes apply 4 8 December 20 2006
39. drain valve of each wing tank located on its bottom Procedure 1 Put a transparent cup under the drain valve 2 Using screwdriver or appropriate jig press and turn drain valve counterclockwise to open it 3 Drain required quantity of fuel December 20 2006 8 7 Section 8 lus Airplane Handling SportStar LA Servicing and Maintenance AIRCRAFT OPERATING INSTRUCTIONS 8 6 Doc No SP2006AOIUS NOTE Draining serves to elimination of impurities and deposits from the fuel Drain until clean fuel flows from the drain valve 4 Using screwdriver or appropriate jig turn drain valve clockwise to close it 5 Repeat procedure for the opposite tank Cleaning and care Always use appropriate cleaning agents when cleaning 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 stream of tepid water with addition of appropriate detergents Use soft rag sponge or wash leather Use suitable polishing agent after wiping rests of water CAUTION NEVER DRY CLEAN THE CANOPY AND NEVER USE PETROL NOR CHEMICAL SOLVENTS Coating upholstery and carpets in the cocpit can be removed from the cocpit brushed and if need be cleaned with warm water with addition of appropriate detergent Dry up upholstery after doing this December 20 2006 Ze Spert top AIRCR
40. e limit E ARN RPM indicator RPM 1400 5500 5500 5800 5800 Oil temperature F 190 230 120 190 266 indicator 230 266 Oil pressure PSI 12 29 73 12 29 102 indicator 73 102 Cylinder head F e 275 temperature 1 pp j 2 6 Miscellaneous instrument marking There are not other instruments with colour marking Weight Empty weight standard equipment Maximum take off weight Maximum landing weight Maximum weight in baggage compartment EXCEEDING DO NOT EXCEED MAXIMUM WEIGHTS THEIR LEADS TO 695 lbs 2 1268 Ibs 1268 Ibs 55 lbs AIRPLANE OVERLOADING AND TO DEGRADATION OF FLIGHT DETERIORATION OF MANOEUVRABILITY CHARACTERISTICS AND December 20 2006 lu Le SportStcir AA AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 2 8 Centre of gravity Empty airplane C G position 20 2 MAC standard equipment Operating C G range 20 to 34 MAC Reference datum is the wing leading edge 2 9 Approved manoeuvres SPORTSTAR airplane is approved to perform the following manoeuvres steep turns up to bank angle of 60 climbing turns lazy eights stalls except for steep stalls normal flight manoeuvres AEROBATICS AS WELL AS INTENTIONAL SPINS ARE PROHIBITED 2 10 Manoeuvring load factors Maximum positive load factor 4 0 Maximum negative load factor 2 0 2 11 Flight crew Minimum crew 1 pilot Minimum weight of crew 121 lbs Maximu
41. edge or in the lower engine cowling Position lights are switched by POS LIGHTS switch and anticollision beacon by BEACON switch Landing headlight is switched by LDG LIGHT or REFLECTOR switch 7 13 2 Electrical system scheme See Aircraft Maintenance and Inspection Procedures Supplements December 20 2006 7 13 Section 7 fus pp Pa System SportStar D ipti TOTUM AIRCRAFT OPERATING INSTRUCTIONS LAA Doc No SP2006AOIUS T 14 Pitot static system Pitot static tube for sensing static and total pressure is located under the left half of the wing Total pressure is sensed through the opening in the Pitot static tube face Static 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 located in the pressure branch of static and total pressure on the left fuselage side by the wing leading edge Static pressure is led to altimeter airspeed indicator variometer and altitude encoder if installed Total pressure is led only to the airspeed indicator Wing Pilot cockpit OF Alt encoder E if installed Static pressure L Total pressure Condensate reservoir Pitotstatic tube Pam DS Figure 7 5 Scheme of pitot static system 7 14 December 20 2006
42. essary 2 Airspeed max 103 KIAS 118 mph IAS 3 Engine instruments check 4 Fuel quantity check CAUTION FUEL GAUGES DISPLAY TRUE FUEL QUANTITY ONLY ON GROUND AND IN A LEVEL FLIGHT TO READ TRUE FUEL QUANTITY AFTER TRANSITION FROM CLIMB DESCENT WAIT APPROX 2 MINUTES TO FUEL TO LEVEL NOTE It is recommended to alternately switch the tanks during cruise 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 left tank vent When the left tank fuel gauge indicates approx 1 8 of fuel quantity needle in the middle between 1 4 and 0 then switch to the right tank to consume remaining fuel and then switch back the left tank to complete the flight at left tank If the engine conks out due to fuel consumption from either tank then immediately switch the fuel selector to other tank and engine run will be recovered within 7 seconds 5 CARBURETTOR PREHEATER if installed as necessary December 20 2006 Section 4 Normal Procedures 4 5 9 Descent SportStair Av AIRCRAFT OPERATING INSTRUCTIONS LA Doc No SP2006AOIUS THROTTLE lever as necessary Airspeed as necessary Trim as necessary Engine instruments check CAUTION AT LONG APPROACHING AND DESCENDING FROM HIGH ALTITUDE IT IS NOT SUITABLE TO REDUCE THROTTLE TO MINIMUM FOR THE REASON OF POSSIBLE ENGINE UNDERCOOLING AND S
43. fire extinguishing aerate the cockpit 5 Carry out safety landing according to 3 8 2 NEVER AGAIN SWITCH THE DEFECTIVE SYSTEM NOTE If a defective electrical system circuit was detected as the fire source then switch off appropriate circuit breaker and switch over Master switch to ON position 3 7 Gliding flight NOTE Gliding flight can be used for example in case of engine failure Wing flaps position Retracted 0 Take off 15 Airspeed 57 KIAS 53 KIAS 66 mph IAS 61 mph IAS December 20 2006 3 7 Section 3 Emergency Procedures 3 8 Emergency landing SportStak Le AIRCRAFT OPERATING INSTRUCTIONS LAA Doc No SP2006AOIUS 3 8 1 Emergency landing with non operating engine 1 2 o o E OQ Airspeed Landing area oafety harness Flaps Airspeed Radiostation 7 FUEL SELECTOR 8 Ignition 9 Master switch 57 KIAS 66 mph IAS choose determine wind direction tighten up landing position 50 60 KIAS 69 mph IAS notify situation to ATC If possible OFF OFF OFF before touch down 3 8 2 Safety landing with engine operating 1 O o E Co Area for landing Radiostation Safety harness Flaps Airspeed Landing choose determine wind direction carry out passage flight with speed of 59 KIAS 68 mph IAS flaps in take off position 15 notify situation to ATC if possible tighten up landing position 50 60 KIAS 55
44. fying the manufacturer of any safety of flight issue or significant service difficulty upon discovery The owner operator of an LSA airplane shall be responsible for complying with all manufacturer issued notices of corrective action and for complying with all applicable aviation authority regulations in regard to maintaining the airworthiness of 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 operator not comply with any mandatory service requirement the LSA airplane shall be considered not in compliance with applicable ASTM Standards and may be subject to regulatory action by the presiding aviation authority 8 2 Airplane inspection period Periodical inspections and reviews of airplane must be carried out at the latest in the following intervals after first 25 2 hours of operation after every 50 3 hours of operation after every 100 5 hours of operation annual inspection Details on periodical inspections are provided in the Aircraft Maintenance and Inspection Procedures of SPORTSTAR PLUS Refer to the Rotax 912 Operator s Manual for engine maintenance Refer to the Propeller Maintenance Manual for propeller maintenance December 20 2006 Nin lus Section 8 SportStar Airplane Handi us JA AIRCRAFT OPERATING INSTRUCTIONS IR and Doc No SP2006AOIUS 8 3
45. heel chocks instead December 20 2006 4 17 Section 4 lus Le B portStak 7 Proced pes AIRCRAFT OPERATING INSTRUCTIONS LA Doc No SP2006AOIUS Intentionally left blank 4 18 December 20 2006 Ne lus Section 5 port B Performance LA AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS CONTENTS 9 PERFORMANCE Jenna 3 5 1 id tele Tei d Le TEE 3 5 2 Approved data cooccccccconconcoccoccccocconconcnaronrnncnnnarnaronrnnrnacanes 4 5 2 1 Airspeed indicator system calibration 4 EE 6 A is o A 7 9 2 4 Lancing Bel EC ue 7 5 2 5 Climb performance 8 5 3 Additional information 10 5 3 1 CS ease E O A 10 5 3 2 Horizontal speeds r rarrnnrvnnevnrrnnrvnrrvanevanrnnrvnnevnnrnnrvnnevnsene 11 5 3 3 0 01 11 0 EE 12 5 3 4 Balked landing cm 13 5 3 5 Effect on flight performance and characteristics 14 5 3 6 Demonstrated crosswind performance 14 uo JOSIIPIB ases 15 5 920 e e E ER EE 15 December 20 2006 5 1 Section 5 Performance SportStar AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Intentionally left blank Ax December 20 2006 Un lus Section 5 port t R Performance PA AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 9 PERFORMANCE 5 1 Introduction Section 5 provides data for airspeed calibration stall speeds take off performance and nonap
46. ik a s 804 Water Street Letecka 1384 Kerrville Texas 78028 686 04 Kunovice USA Czech Republic phone 001 830 896 8910 tel 420 572 537 111 fax 001 830 896 8913 fax 420 572 537 900 e mail sportac ktc com e mail marketing 2 evektor cz 1 3 Warnings cautions notes The following informations apply to warnings cautions and notes used in the Aircraft Operating Instructions MEANS THAT NON OBSERVATIONS OF THE CORRESPONDING PROCEDURE LEADS TO AN IMMEADIATE OR IMPORTENT DEGRADATION OF THE FLIGHT SAFETY CAUTION MEANS THAT NON OBSERVATIONS OF THE CORRESPONDING PROCEDURE LEADS TO A MINOR OR TO A MORE OR LESS LONG TERM DEGRADATION OF THE FLIGHT SAFETY NOTE Draws the attention to any special item not directly related to safety but which is important or unusual 1 4 December 20 2006 1 4 1 4 1 1 4 2 lu i Ze SportSidk Sz LA AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Descriptive data Airplane description SPORTSTAR airplane is an all metal low wing of semimonocoque structure with two side by side seats and nose wheel landing gear For further description see Section 7 Airplane and system description 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 description For concrete engine and propeller type see Section 9 Supplements Airplane description
47. intentionally switch the selector to OFF position To move selector to OFF closed position it is necessary pull the safety button on the fuel selector turn the handle to the OFF position and then release safety button Now the handle is blocked in the OFF position Safety button prevents unintentionally switch the selector from the OFF position during parking 7 12 3 Fuel filter The fuel filter separates all mechanical impurities from fuel The fuel filter is located in the cockpit on the left airframe panel 7 12 4 Indication of fuel quantity Fuel quantity is measured by a float fuel gauge transmitter in each tank and indicated on fuel gauge on the instrument panel LH fuel gauges indicates fuel quantity in the left primary tank RH indicator in the right tank True fuel quantity is indicated only on ground and December 20 2006 7 11 Section 7 dus PD Pa System SportStar D ipti TOTUM AIRCRAFT OPERATING INSTRUCTIONS LA Doc No SP2006AOIUS 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 specified in chapter 8 Main fuel pump Fuel distribution with nozzle Firewall Electrical fuel pump Fuel if installed Fuel pressure filter if installed Pilot cockpit Fuel line 31 Carburetter Return line Draining point Venting line 9 Pump Elec
48. k hydraulic brakes on main landing gear wheels Brake system is composed of brake pedals these are a part of rudder control pedals brake pumps hoses for leading brake liquid brake yokes with wheel 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 Braking pressure can be regulated only by force of brake pedals depressing The airplane can be equipped by mechanical manually controlled parking brake PARKING BRAKE handle is located in between the pilot seats Seat and safety harnesses SPORTSTAR is a two seat airplane with side by side seats Seats are fixed non adjustable and fitted with light upholstery Each of seats is fitted with four point safety harness which is composed of safety belts shoulder straps and lock The safety harness is anchored in the middle of the frame behind the baggage compartment and on the seat sides Baggage compartment Baggage compartment is positioned behind seat rests Maximum weight of baggage is 55 Ibs 25 kg and is stated on the placard in the baggage compartment The baggage compartment is fitted with rubber straps for baggage fixation December 20 2006 Ne lus Section 7 SportStar Airplane hun cue de LAA AIRCRAFT OPERATING INSTRUCTIONS oe Doc No SP2006AOIUS 7 10 Canopy The cocpit canopy is of a semidrop shape The
49. lu ection Le SportStar M LAA AIRCRAFT OPERATING INSTRUCTIONS eae AA Doc No SP2006AOIUS 10 Ignition START see CAUTION after starting up BOTH CAUTION ACTIVATE STARTER FOR 10 SEC AS A MAXIMUM THEN LET IT COOL DOWN FOR 2 MINUTES AFTER STARTING UP ENGINE DO NOT CARRY OUT SUDDEN RPM CHANGES AFTER POWER DECREASE WAIT FOR ABOUT 3 S IN ORDER TO REACH CONSTANT RPM BEFORE REACCELERATION 11 THROTTLE lever as necessary see NOTE 12 Oil pressure up to 10s min pressure 13 GEN AUX GEN 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 10s Increase engine RPM until oil pressure is stabilised over 2 bar 29 PSI Electric fuel pump operates during engine starting period only It is not intended for long continuous operation for long time 15 Engine instruments check 16 Choke as necessary 17 Engine warming up see NOTE NOTE Begin warming up with engine running at 2000 RPM for about 2 minutes continue at 2500 RPM Warming time depends on outside air temperature until oil temperature reaches 122 F December 20 2006 4 9 Section 4 Normal port t R P d ens AIRCRAFT INSTRUCTIONS Doc No SP2006AOIUS 18 FUEL SELECTOR RIGHT Verify proper engine feeding from the right tank for approx 1 minute 19 FUEL SELECTOR LEFT NOTE otart engine with
50. m HTU horizontal tail unit IAS indicated airspeed IC intercom IFR instrument flight rules ISA international standard atmosphere kg kilogram KIAS indicatedair speed in knots KCAS calibrated airspeed in knots mph mile per hour mph CAS calibrated airspeed in miles per hour km h CAS calibrated airspeed in km h kis knots 1 kt 1 852 km h litres litre lbs pounds 1 Ib 0 45 kg m meter MAC mean aerodynamical chord max maximum min minimum or minute mm milimeter m s meter per second OAT outside air temperature December 20 2006 Ze OFF position ON position Pa PSI RPM RWY sq ft sq m VA Vre position VFR VLor V METER Vne VNo Vso Vs VTU Vx Vy XPDR December 20 2006 Section 1 General SportStar AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS system is switched off or control element is in off system is switched on or control element is in on pascal 1Pa 1N m pound per sq in 1PSI 6 89 kPa revolutions per minute runway foot squared meter squared manoeuvring airspeed maximum flap extended speed flaps in 50 visibility flight rules airplane lift off soeed voltmeter never exceed speed maximum structural cruising speed stall speed with wing flaps in 50 position stall speed with wing flaps in 0 position vertical tail unit best angle of climb speed best rate of climb speed transponder Section 1 lus Len SportSidk N7 AIRCRAFT OPERATING INST
51. m weight of crew acc to chapter 6 DO NOT EXCEED MAXIMUM WEIGHTS THEIR EXCEEDING LEADS TO AIRPLANE OVERLOADING AND TO DEGRADATION OF FLIGHT CHARACTERISTICS AND DETERIORATION OF MANOEUVRABILITY December 20 2006 2 7 Section 2 lus Len Limitations SportStar Je AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 2 12 Kinds of operation 2 13 The airplane is standardly approved for VER daylight flights NIGHT FLIGHTS ACCORDING TO VFR FLIGHTS ACCORDING TO IFR BY INSTRUMENTS ARE APPROVED ONLY WHEN INSTRUMENTATION 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 flights according to VFR 1 Airspeed indicator the color marking according to par 2 3 1 Sensitive barometric altimeter 1 Magnetic compass 1 Fuel gauge indicator 1 Oil temperature indicator 1 Oil pressure indicator 1 Cylinder head temperature indicator 1 Engine speed indicator 1 Safety harness for every used seat CAUTION ADDITIONAL EQUIPMENT NECESSARY FOR AIRPLANE OPERATION IS GIVEN IN APPROPRIATE OPERATION REGULATION OF AIRPLANE OPERATOR S COUNTRY Fuel Fuel tank volume each 15 85 U S gallons Total 31 7 U S gallons Usable fuel 31 2 U S gallons Unusable fuel 0 5 U S gallons 0 25 US gal per tank December 20 2006 lu Le SportStcir AA AIRCRAFT OPERATING INSTRUCTIONS Doc No S
52. mber 20 2006 Ne lus Section 7 SportStar Airplane hin cue LAA AIRCRAFT OPERATING INSTRUCTIONS FOR Doc No SP2006AOIUS CONTENTS 7 AIRPLANE AND SYSTEM DESCRIPTION 3 LL The ge e TE CONN EE c 3 L2 PA a a nek 3 7 2 1 PUGS lo a na en pe etes tee nes 3 Dee NO a E 3 7 2 3 Horizontal tail unit HTU 3 7 2 4 Vertical tail unit VII 3 T3 CONVO A o A 4 7 3 1 Longitudinal control 4 3 2 Lateral control ois canicisisniwnnewevicnesecisusnvaedesiewseaxeusesnsusxdansanencseueseess 4 739 RO COM Ol escusa coca 4 7 3 4 Elevator trim tab Control 4 7 4 Controls in COC OU estes 5 7 5 Instrument d CT EE 5 7 6 Inside and outside marking and placards 5 7 7 Landing gear and brakes 6 7 7 1 LAMENTO ne a aan ne T 6 T E il E 6 7 8 Seat and safety harnesses EN RENE 6 7 9 Baggage compartment eese 6 A Pc TUM 7 7 11 NI mtd 7 Nata 7 Talle TOMS CONTO Mtm 7 7 11 3 Engine intruments n noenennennannenennennenrsnnnnnrrsrrerenrrnrerrenenne 8 7 11 4 Engine cooling system rrnrnnnrnnnnnnnnnnnnnnrnnnrvnnnnnrnnerrnnnnnnnne 8 7 11 5 Engine lubrication system ocooocccocncoccncocncnononanonnnonnnnonanonnos 9 7 11 6 Engine intake system 10 7 11 7 lgnition system 10 December 20 2006 7 1 Section 7 fus Pp Pa System SportStar D
53. nd its feeding to the engine Fuel system of SPORTSTAR airplane is composed of integral fuel tanks fuel line fuel selector fuel filter mechanical fuel pump located on the engine auxiliary electrical fuel pump can be installed distribution pipe of fuel with return branch of fuel fuel gauges and fuel tanks draining valves Fuel tanks Fuel is contained in the wing integral tanks having volume 15 85 U S gallons each Each tank is fitted with air venting output is under the wing tip and draining valve on the bottom side of the wing Fuel is led from the tanks through the hoses to the fuel December 20 2006 Ne lus Section 7 SportStar Airplane hun cue de LAA AIRCRAFT OPERATING INSTRUCTIONS oe AA Doc No SP2006AOIUS selector located on a central console under the instrument panel and then through a fuel filter to the engine pump and carburetors Fuel return hose goes from the fuel pump into the left tank which is due to considered as a primary tank See figure 7 4 for Scheme of fuel system 7 12 2 Fuel selector The fuel selector serves for tank selection and fuel delivery interruption in case of engine fire or long parking of airplane To move selector from OFF closed position it necessary pull the safety button on the fuel selector turn the handle from the OFF position to the left and then release safety button Now the handle can be freely moved between LEFT and RIGHT position Safety button prevents un
54. ndition and inflation e condition and attachment of wheel covers mudguards if installed Left wing check e wing surface condition e leading edge condition e landing light condition if installed e condition of the Pitot tube e draining of fuel tank see chapter8 page 8 6 e closing of fuel tank cap Left wing tip check e surface condition e attachment check e fuel tank vent cleanness e condition and attachment of the position lights and the anticollision beacon if installed Left aileron check e Surface condition e attachment e free movement Left wing flap check e surface condition e attachment Rear part of fuselage check e Surface condition e condition of antennas top and bottom fuselage surface if installed Tail units check 2006 4 5 Section 4 Normal Procedures 8 9 10 11 12 13 14 15 4 6 SportStar Ze AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS e tail skid condition e surface condition e condition of rudder and elevator attachment e freedom of rudder and elevator movement e condition of trim tab condition of elevator trim tab control Rear part of fuselage check e surface condition Right wing flap see 5 Right aileron see 4 Right wing tip see 3 Right wing see 2 except the landing light if installed and Pitot tube Right landing gear leg see 1 Front part of the fuselage right hand side check e tilting can
55. ng down the round button on the lever body and by its pulling out or pushing in Small changes in power setting can be performed through lever turning conterclockwise power increase The lever is fitted with the locking ring counterclockwise turning of which ensures locking of the lever in requested position December 20 2006 1 7 Section 7 fus Pp Pa System SportStar D ipti TOTUM AIRCRAFT OPERATING INSTRUCTIONS LAA Doc No SP2006AOIUS 7 11 3 Engine intruments The following analog instruments located on the instrument panel serve for engine performance monitoring The digital engine monitoring system can be installed in the airplane instead of analog engine instruments RPM indicator The electrical RPM indicator is controlled by signal from the generator RPM transmitter Working range of the RPM indicator is 0 7000 RPM Colour code is stated in section 2 Cylinder head thermometer The cylinder head thermometer transmitter senses temperature of cylinder No 3 Working range of the cylinder head thermometer is 120 300 F Colour code is stated in section 2 Oil thermometer 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 pressure on the oil input into engine is measured by means of sensor which is located behing the oil filter Working range is 0 150 PSI C
56. ntrol Airplane is equipped with dual control enabling flight with two member crew Longitudinal control Longitudinal control is actuated by the control stick Longitudinal movement of control stick is transferred to the elevator by mechanical system of pull rods and levers Lateral control Lateral control is actuated by the control stick From the control stick the movement is transferred through the system of levers and pull rods to ailerons Rudder control Rudder control is controlled by pedals of foot control The rudder is interconnected with foot control pedals by cable system Foot control pedals adjustable into three positions can be installed as an option Way of adjustment of ruder pedals 1 Release the pin from the adjusting groove 2 Set pedal to one of three possible positions 3 Check on the pin locking on in the adjusting groove RIGHT AND LEFT PEDAL OF RUDDER CONTROL MUST BE ADJUSTED IN THE SAME POSITIONS AND SECURED Elevator trim tab control The elevator trim tab is controled by the lever located in between the pilot seats The control lever is interconnected with the trim tab by means of bowdwen cables December 20 2006 ve lus Section 7 SportStar Airplane Bs LAA AIRCRAFT OPERATING INSTRUCTIONS SEENEN Doc No SP2006AOIUS 7 4 Controls in cockpit 3 97 6 8 2 FEE EE
57. olour code is stated in section 2 7 11 4 Engine cooling system Engine cooling is combined cylinder heads are cooled by water cylinders are cooled by air Cooling circuit of cylinder heads is designed as a closed system containing pump expansion reservoir 1 with pressure closure 3 cooler of cooling liquid 2 and drainage reservoir 4 Scheme of cylinder head cooling system is shown in Fig 7 2 When changing the cooling liquid is filled up through the cap of expansion reservoir 1 during airplane operation it is replenished into drainage reservoir 4 between the lines of maximum and minimum level 7 8 December 20 2006 LAA 7 11 5 ve lus Section 7 SportStar Airplane Bs AIRCRAFT OPERATING INSTRUCTIONS SESS DUO Doc No SP2006AOIUS Figure 7 2 Scheme of cylinder head cooling system Engine lubrication system Engine lubrication system is performed with the dry crank case Engine lubrication system is equipped with oil pump 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 pump The oil recervoir is aerated by the hose 7 which is led under the airplane Oil pressure and temperature are indicated on instruments in right side of the instrument panel Oil is replenished through the lid in the upper part of the oil reservoir 4 i om EE Fig
58. opy attachment and condition e condition of the nose landing gear leg e nose wheel condition e condition of the nose weel control rods Engine Checks before the first flight of day it is necessary to remove upper engine cowling e condition of engine bed e condition of engine attachment e condition of exhaust system e condition of engine cowlings e visual check on fuel and electrical system condition e check on cooling liquid volume in the expansion tank on the engine body replenish as required up to max 2 3 of the expansion tank volume December 20 2006 ve lus Section 4 portSteir LAA AIRCRAFT OPERATING INSTRUCTIONS ae AA Doc No SP2006AOIUS Checks before every flight e cleanness of air intakes e check on oil level between marks flattenings on the dip stick e check on cooling liquid level in the overflow bottle level should be between min and max mark e proper closing of the upper cowling 16 Propeller check e attachment e condition of blades hub and spinner 17 Front part of fuselage left hand side check e 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 perpendicular position to the handle axis e all switches OFF e instrument equipment check on condition e check on presence of loose object in the cockpit e check on adjusting and se
59. plane structure December 20 2006 Nin lus Section 8 SportStar Airplane Handi an AN AIRCRAFT OPERATING INSTRUCTIONS ib e Doc No SP2006AOIUS 8 4 4 Airplane jacking Airplane jacking presents no big difficulties due to relatively low airolane empty weight and can be performed by two persons First it is necessary to prepare two suitable rests which will support the airplane The airplane can be jacked in the following way by pushing from the above to the fuselage rear part in the position before the fin the front part of fuselage can be jacked and subsequently supported under the fire wall Rear part of fuselage can be slightly jacked only by grasping in the position near the auxiliary skid and by pushing from below and then the lower 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 grasping the wing tip 8 4 5 Levelling Levelling procedure is described in the Maintenance manual for SPORTSTAR airplane 8 4 6 Road transport The airplane can be transported on communication after its laoding on an appropriate trail It is necessary to dismount wings The airplane must be secured against possible movement This way you will preclude possible damage to the airplane 8 5 Draining of fuel tank Draining should be done prior to first flight each day There is a
60. possible by using hereafter explained Loading graph method using weights arms and moment indexes 6 4 1 Computational Procedure 1 Record into the Airplane Loading Schedule Chart current empty weight and static moment of the airplane which you read from the table 6 2 Weight and Balance Record 2 Record the weight of crew fuel and baggage into the Airplane Loading Schedule Chart 3 See the Table of Static Moments or Airplane Loading Graph to read static moments for given weights of crew fuel and baggage 4 Record found moments into the Airplane Loading 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 calculated Take off weight does not exceed Airplane Maximum Take off Weight 1268 Ib If yes then it is necessary to reduce weight of some of the useful load items fuel baggage WARNING EXCEEDING MTOW MAY LEAD TO DETERIORATION OF SAFETY OF FLIGHT 7 Determine Total Static Moment of loaded airplane add together the static moment of empty airplane crew fuel and baggage and record the result into the Loading Schedule Chart 8 Plot Takeoff Weight and Total Static Moment into the SPORTSTAR CG Moment Envelope 9 Check whether the intersection of Take off weight horizontal line and Total Static Moment vertical line is inside the envelope If YES then
61. proved additional information provided by the airplane type certificate owner The stated performance data has been computed from actual flight tests with the SPORTSTAR airplane and ROTAX 912 ULS engine in good condition and using average piloting techniques CAUTION THE PERFORMANCE STATED IN THIS SECTION IS VALID FOR ROTAX 912 ULS 100 HP TOGETHER WITH WOODCOMP KLASSIC 170 3 R PROPELLER INSTALLED IN THE AIRPLANE OTHERWISE SEE SECTION 9 SUPPLEMENTS FOR ACTUAL PERFORMANCE December 20 2006 5 3 Section 5 fus e SportStar AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Y 5 2 Approved data 5 2 1 Airspeed indicator system calibration NOTE Assumed zero instrument error Valid for airplane take off weight 1268 lbs Flaps deflection 0 Flaps deflection 15 aps deflection 50 Flap KCAS KIAS KCAS KIAS KCAS 38 40 138 5 4 December 20 2006 Lee lus Section 5 port t R Performance LAA AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Flaps deflection 0 Flaps deflection 15 Flaps deflection 50 IAS CAS IAS CAS IAS CAS mph mph mph mph mph mph 44 46 47 49 47 48 50 52 50 52 50 51 55 57 53 54 53 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 15 73 105 100 77 75 77 75 110 105 80 78 80 78 115 109 81 79 81 79 120 114 125 118 130 123 135 12
62. proved only for VFR day flights under no icing conditions Aerobatics and intentional spins are prohibited AIRSPEED IAS 168 MPH 99 MPH 81 MPH 44 MPH ENGINE SPEED 5800 rpm Max Take off max 5 min 5800 rpm 5500 rpm Max Continuous 5500 rpm 1400 rpm Idling 1400 rpm Unusable quantity of fuel 0 5 USgal LOAD LIMITS Max take off weight 1268 Ibs Empty weight 672 Ibs Max baggage weight 55 lbs PERMITTED CREW WEIGHT Ibs Fuel quantity U S gal 31 7 26 4 19 8 13 2 6 6 o max 55 Ibs 350 381 421 461 500 SS Se 12 26 Ibs 378 410 450 489 529 a No baggage 405 437 476 516 556 Fuel reserve 1 8 on the fuel indicator NOTE 2 1 U S gallons The values stated on the placard LOAD LIMITS are valid for the empty weight of the airplane with standard equipment The placard with values valid for the actual empty weight of the airplane will be placed in the cockpit Other placards and labels are shown in Aircraft Maintenance and Inspection Procedures December 20 2006 Section 2 Limitations SportStar AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Intentionally left blank Ax December 20 2006 lu Le SportStar p LAA AIRCRAFT OPERATING INSTRUCTIONS ee Doc No SP2006AOIUS CONTENTS 3 EMERGENCY PROCEDURES eere nnns 3 2 1 MON socia piri texdu kun ERN UU UI Fes Or a ae 3 3 2 Speeds for performing emergency procedures
63. ransport GE 5 8 4 1 Airplane towing VU 5 8 4 2 A Airplane parking 6 8 4 3 A Airplane anchomg 6 8 4 4 A Airplane jacking 7 ES Le EEE 7 E EE tee KE LA resesi nnne NEEE EEEE 7 8 5 Draining of fuel tank eese eene 7 0 0 Cleaning nd C r uaasssssseaenemennesee 8 December 20 2006 8 1 Section 8 fus Ne A es SportStar Servicing and LAX Maintenance AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Intentionally left blank 8 2 December 20 2006 Nin lus Section 8 SportStar Airplane Handi LA an AIRCRAFT OPERATING INSTRUCTIONS ib e Doc No SP2006AOIUS 8 AIRPLANE HANDLING SERVICING AND 8 1 MAINTENACE Introduction This section includes the procedures for airplaine handling maintenance and operation recommended by the manufacturer It is necessary to follow the set down lubrication plan scope and periodocity of preventive maintenance depending on climatic and flight conditions according to the Aircraft Maintenance and Inspection Procedures of SPORTSTAR Light Sport Aircraft Airplane owner should be in a permanent touch with the manufacturer either directly or through the network of business representatives which enables him to get the newest information concerning airplane operation handling and maintenance The manufacturer distributes this information to users through Service bulletins Mandatory bulletins Information bulletins
64. rforming emergency procedures Airspeed for the best gliding ratio 57 KIAS 66 mph IAS flaps retracted Precautionary landing 53 KIAS 61 mph IAS engine 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 Brakes as necessary 3 FUEL SELECTOR OFF 4 Ignition OFF 5 Master switch OFF 3 3 2 Engine failure at take off 1 Gliding speed with flaps in take off position 15 min 53 KIAS 61 mph IAS with flaps retracted 0 min 57 KIAS 66 mph IAS 2 Altitude Land in take off direction if below 150 ft Land in take off direction or you can perform turn up to 90 if altitude is 150 400 ft You can try start engine if altitude is above 250 ft December 20 2006 3 3 Section 3 Emergency Procedures O ON DO R ww SportStak Dra AIRCRAFT OPERATING INSTRUCTIONS LA Doc No SP2006AOIUS You can perform turn up to 180 if altitude is above 400 ft THROTTLE lever idle Flaps as needed FUEL SELECTOR OFF Ignition OFF ATC report Master switch OFF After touch down brake as needed 3 3 3 Engine failure in flight 3 4 1 2 Gliding speed 57 KIAS 66 mph IAS Altitude take a decision and carry out Engine starting in flight paragraph 3 4 Emergency landing paragraph 3 8 1 Engine starting at flight Oo O A N gt
65. rs t Ya E a VJ d 000s s VA 006 G Vet i NE Pp EN or E O Yon I 3 NN A oor Y o o Noa J o 2 vials o pM Xo 0097 o Sz VE N 1 dH BN mer 22 EE y 001 Q e d 4 5 VEN 00 S VL MG 002v VI KN 7 i 00Lv LAN B 000 st c lt lt HD GD 0066 T E E E E H 8 8 8 8 008 Tm ww 1 4 a 0048 I ww b d LITT OOGE December 20 2006 Un lus Section 5 port t R Performance PA AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 5 3 2 Horizontal speeds In the following table states Indicated airspeeds IAS corresponding calibrated air speeds CAS and true air speeds TAS versus altitude all for various engine speeds 55 MTV 65 MTV 75 MTV MCP MTP Maximum Maximum Continuous Takeoff Power Power LL IL 5 min 4300 rpm 4800 rpm 5000 ES 5500 Gil 5800 oq ias 82 93 9 109 116 LT leas 78 88 o 108 110 Frias 78 88 92 103 110 Kas 78 89 94 106 4A KCAS 75 85 90 100 ktas 77 88 92 103 Kas 74 86 91 108 Men KCAS 72 83 8 IB ktas 76 88 92 103 klas 70 83 88 100 ea KCAS 69 80 84 95 Frias 75 87 92 103 Klas 66 80 85 96 9A KCAS 65 77 8 92 ktas 73 86 91 103 klas 62 76 8 Tow KCAS 62 74 78
66. rt t R Performance AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Conditions engine maximum take off power carburetter preheating OFF flaps landing position 50 airplane weight 1268 Ibs ambient air temperature ISA BALKED LANDING CLIMB pas m 7m A TT T Ts cL ee l IE Flaps Takeoff 15 EIN Flaps Landing 30 MEN t Flaps Landing Il 50 m 35 40 45 50 55 60 65 70 75 Climbing speed KIAS December 20 2006 5 13 Section 5 lus va See SportStar 5 3 5 5 3 6 LA AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Effect on flight performance and characteristics Flight performances and characteristics are not considerably affected by rain or insect stuck on the airplane surface Demonstrated crosswind performance Maximum demonstrated speed of wind at airplane operation 24 kts 28 mph Maximum demonstrated speed of cross wind for take off and landing 10 kts 12 mph Maximum demonstrated speed of tail wind 6 kts 7 mph
67. s altitude O ft ISA ambient air temperature ISA Take off run Take off distance to height of 50 ft 15 ft Dray concrete 620 ft 1440 ft Grass 720 ft 1540 ft Corrections Influence of wind Add 4 on every 1 kt 1 15 mph of tail wind Add 8 of the take off run distance on 1 of ruway inclination up the slope RWY inclination 5 2 4 Landing distance Conditions engine idle flaps Landing 50 carburetter preheating OFF airplane weight 1268 Ibs altitude O ft ISA ambient air temperature ISA Landing distance from Braked landing run height of 50 ft 15 ft Dray concrete 1310 ft 590 ft Grass 1250 ft 520 ft Corrections December 20 2006 Influence of wind Add 4 5 on every 1 kt 1 15 mph of tail wind Add 8 of the landing run distance on 1 of ruway inclination down the slope RWY inclination Section 5 lus some SportStak AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 5 2 5 Climb performance 900 850 800 700 650 600 550 500 450 400 Rate of climb fp m 0 ft ISA e EEE B EE LT 2000 ft ISA er Ta 4000tI8A L mee A den a A ai 7 6000 ft ISA ee A A g 8000 t ISA 7 gt Ee 4 10000 ft ISA 150 E 1 1 1 1 1 1 1 I 1 1 1 jr ae 1 1 pr 1 1 1 LJ 1 1 1 I KZ 1 1 45 50 55 60 65 70 TD 80 85 Climbing speed KIAS 350 300
68. stalled push December 20 2006 3 5 Section 3 Emergency Procedures SportStir c AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS After the engine stops 1 O ON Oo o Gliding speed 53 KIAS 61 mph IAS Ignition OFF Master switch OFF Land Airplane leave Manual extinguisher if available use 3 5 3 Fire in flight 1 N o O1 bk WO D FUEL SELECTOR OFF THROTTLE lever full HOT AIR knob if installed close Gliding speed 57 KIAS 66 mph IAS Ignition OFF ATC report if possible Master switch OFF NOTE For extinguishing the engine fire you can perform slip under assumption that you have sufficient altitude and time AFTER EXTINGUISHING THE ENGINE FIRE START ENGINE ONLY IF IT NECESSARY TO SAFE LANDING FUEL LEAK IN ENGINE COMPARTMENT COULD CAUSE FIRE AND FIRE COULD RESTORE AGAIN If you start engine again switch off all switches switch on the Master switch and then subsequently switch on only equipment necessary to safe landing Emergency landing carry out according to paragraph 3 8 1 Airplaine leave December 20 2006 dar i A SportStar a AIRCRAFT OPERATING INSTRUCTIONS iii Doc No SP2006AOIUS 11 Manual extinguisher if available use as needed 3 6 Fire in the cockpit if manual extinguisher available aboard 1 Fire source identify 2 Master switch in case that the source of fire is electrical equipment OFF 3 Manual extinguisher use 4 After
69. systems and equipment are stated in section 9 Supplements 2 2 Airspeed Airspeed limitations and their meaning for operation are stated in the table below Speed KIAS mph IAS Meaning Vne Never exceed 146 168 Do not exceed this speed in speed any operation Vno Maximum 103 118 Do not exceed this speed with structural exception of flight in smooth cruising speed air and even then only with increased caution Va Manoeuvring 86 99 Do not make full or abrupt speed control movement above this speed because under certain conditions the aircraft may be overstressed by full control movement Vee Maximum flap 70 81 Do not exceed this speed with extended speed the given flap setting December 20 2006 2 3 Section 2 Limitations SportStar AIRCRAFT OPERATING INSTRUCTIONS Ax Doc No SP2006AOIUS 2 3 Airspeed indicator marking Airspeed indicator markings and their color code significance are shown in the table below Marking Range Meaning KIAS mph IAS Red line 38 44 Vso at maximum weight flaps in landing position 50 White arc 38 70 44 81 Operating range with extended flaps Lower limit Vs at maximum weight flaps 50 Upper limit Vee Green arc 43 105 50 121 Normal operation range Lower limit Vs at maximum weight flaps 0 Upper limit Vno Yellow arc 105 146 121 168 Manoeuvres must be conducted with caution and only in smooth air
70. t the risks inherent in such participation of which the ordinary prudent person is or should be aware Pilots and passengers have a duty to excersise good judgment and act in a responsible manner while using the aircraft and to obey all oral or written warnings or both prior to and or during use of the aircraft This Flight manual has been prepared to provide pilots and instructors with information for safe and efficient operation of the SPORTSTAR airplane It also contains supplementary information considered to be important by the airplane manufacturer 1 2 Certification basis The aircraft described herein complies with the Standard opecification for Design and Performance of a Light Sport Airplane Designation 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 of the Czech Republic and the type certificate ULL 07 2003 supplement was issued in December 19th 2006 December 20 2006 1 3 Section 1 Ze Genera port R AIRCRAFT a INSTRUCTIONS Doc No SP2006AOIUS 1 2 1 Data location The certification documentation is available from the US General importer or airplane manufacturer on a request of competent aviation authority and or Designated Airworthiness Representative Contact address US General Importer Airplane Manufacturer Sport Aircraft International LLC Evektor Aerotechn
71. tar AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Ur OU gi juauo N 1UBISM Weight and Balance Record aue dure Adwa jo 1UBIam oiseg ural u gi ura uw a jueulo N wy JUBIONA 108WON wuy 14619M perowoy nem eDueuo JUBbIamMm ON PUS euejdJre peJnjoejnueJA UONBOINIPOW 10 Jed jo uonduoseq ON Liga December 20 2006 Section 6 Weight and Balance SportStar AIRCRAFT OPERATING INSTRUCTIONS Ne AG 6 3 2 Doc No SP2006AOIUS Permitted Payload Range ainyeubis ojeq sql 0 sql 9c sql GG sql 0 Sql 9c Sql GG sql 0 sql 9c sql GG BAGGAGE sql 0 sql 9c 62 el 6G 061 sql GG sq 1ybiam any 99 GEL 8 6L v 9c ZL I suoje ml euunjoA jan cO FU 90 80 euJnjoA any peAouddy ONITIANSA LOVIN 9 9 Leo Jybiem dwg ojeq sqi M919 jo JUBISM wuntwuixen L December 20 2006 ection lu Weight and SportStar Ax Bal are AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS 6 4 Operational Weight and Balance Computation An important part of preflight planning is to determine that the aircraft is loaded so its weight and CG location are within the allowable limits This is
72. the flight may be safely performed as regards weight and balance If NOT then it is necessary to change weight of some of the useful load items crew fuel baggage so that after a repeated 6 6 December 20 2006 N T lus Section 6 SportSt R Weight and LAX Balance AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006A0IUS 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 PERMITTED LIMITS OF WEIGHT AND STATIC MOMENTS MAY BE DETERIORATED December 20 2006 6 7 Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS ort Star Doc No SP2006AOIUS 6 5 Airplane Loading Schedule Chart Type Model Serial No Loading Schedule Chart Sample Aircraft Your Aircraft No Item Arm Weight Moment 100 Weight Moment 100 Zeg in Ib lb in Ib lb in 1 Empty Airplane 10 39 in 740 75 Ib 77 1 Ib in 2 Crew 21 45 in 399 04 Ib 85 6 Ib in Baggage 3 Max 55 Ib 42 65 in 11 02 Ib 4 7 Ib in Fuel 4 Max 32 USGAL 26 75 in 60 41 Ib 16 2 Ib in 5 Takeoff weight Sum of weights 1 4 MTOW 1268 lb 1211 Ib 184 Ib in Total moment Sum of moments 1 4 December 20 2006
73. the fuel selector set to to LEFT If you would start the engine with the fuel selector set to RIGHT and the left tank is full than fuel bleed from the left tank vent may occur and pollute environment because a fuel return hose is led only into the left tank and returning fuel will overfill the left tank 20 AVIONICS SWITCH ON 21 Radiostation avionics ON 22 Other electrical equipment ON as necessary 4 5 3 Before taxiing 1 Transponder if installed SBY 2 Outside lights if installed as necessary 4 5 4 Taxiing 1 THROTTLE lever as necessary 2 Brakes check by depressing 3 Rudder pedals function check 4 Direction of taxiing control by rudder pedals these are mechanically connected with nose wheel control possibly by slacking up left and right wheel of the main landing gear 4 5 5 Before take off 1 Brakes brake 2 Ignition check carry out see NOTE 4 10 December 20 2006 Ze Oo O N OORA C 10 11 12 13 14 15 16 17 18 lus Section 4 SportStar AIRCRAFT OPERATING INSTRUCTIONS Gett Doc No SP2006AOIUS NOTE Carry out ignition check in the following way Set engine speed to 4000 RPM Switch ignition gradually to L BOTH R position and return to BOTH RPM drop with one ignition circuit switched off must not exceed 300 RPM Maximum RPM difference at using one of the L or R circuits is 120 RPM Engine instruments check Control stick free Wing flaps take off pos 15 Trim
74. trical circuit 2 Fuel gauge Check valve Figure 7 4 Scheme of fuel system 7 12 December 20 2006 Ne lus Section 7 SportStar Airplane ee LAA AIRCRAFT OPERATING INSTRUCTIONS ON AA Doc No SP2006AOIUS 7 13 Electrical system The airplane is equipped with 14 V DC electrical installation A generator with power of 250 W is the primary source of electrical energy The secondary source of energy is the accumulator 12V 16Ah that is located in the engine compartment on the fire wall It is used for engine starting and in case of generator failure as an emergency source of energy and also serves as the smoothing filter of power system DC voltage is distributed to individual systems by main busbar Each system is protected by circuit breaker If overloading of any of the circuits occurs then the circuit breaker 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 activated The starter is power supplied from the accumulator before engine start After engine has been started and idle RPM reached generator starts supplying current into electrical network 7 13 1 Lighting Airplane can be equipeed with a external lighting External lighting can be composed of position lights and anticollision beacons which are located in wing tip and landing headlight which is located in left wing leading
75. ure 7 3 Scheme of engine lubrication system December 20 2006 7 9 Section 7 ms Aa System SportStar Je Description 7 11 6 7 11 7 7 12 7 12 1 AIRCRAFT OPERATING INSTRUCTIONS Doc No SP2006AOIUS Engine intake system Engine intake system ensures delivery of sufficient air into engine Air is taken into the engine through openings on the engine covers through the air filters The intake system can be equipped with carburettor heating system Hot air from the heat exchanger located on the exhaust collector is taken to the mixing chamber Amount of in taken hot air is regulated by flaps in mixing chamber inlets Flaps are controlled by the CARBURETTOR PREHEATER knob on the instrument panel Ignition system The engine is equipped with the double contactless ignition system Each ignition circuit has own source of energy control unit 2 ignition coils and 4 spark plugs It is fully autonomous on the other circuit of accumulator High voltage current is 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 of ignition switch OFF engine ignition is off R only ignition circuit B is on L only ignition circuit A is on BOTH both circuits are on START both circuits are on and starter is cranking the engine Fuel system Fuel system serves for keeping fuel in the airplane a

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