EVEKTOR-AEROTECHNIK EV-97? EUROSTAR ?model 2000 version R Pilot Operating Handbook Download | Manualshive

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PILOT’S OPERATING HANDBOOK

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01/2001

Revision:

Document No.:

EV2000RLPEN

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Summary of Contents for EV-97? EUROSTAR ?model 2000 version R

Page 1: ...ecka 1384 686 04 Kunovice CZECH REPUBLIC tel 420 572 537 111 fax 420 572 537 900 marketing evektor cz www evektor cz PILOT S OPERATING HANDBOOK EV 97 model 2000 version R I N F O M A I O N O N R R T I...

Page 2: ...d by Signature Authority Stamp Date of approval This English edition of the EV 97 EUROSTAR Flight Manual has been translated with care and is accurate to best of our knowledge However in all official...

Page 3: ...e airworthiness authority The new or amended text in the revised pages will be indicated by a black vertical line in the left hand margin and the Revision No The date will be shown on the left hand bo...

Page 4: ...1 2 1 01 2001 ii 10 2001 2 2 01 2001 iii 10 2001 2 3 01 2001 iv 10 2001 2 4 10 2001 v 01 2001 2 5 10 2001 2 6 10 2001 2 7 01 2001 1 1 0 01 2001 2 8 01 2001 1 1 01 2001 2 9 10 2001 1 2 01 2001 2 10 01...

Page 5: ...2001 7 1 01 2001 4 6 01 2001 7 2 01 2001 4 7 01 2001 7 3 01 2001 4 8 01 2001 7 4 01 2001 4 9 01 2001 7 5 01 2001 4 10 01 2001 7 6 01 2001 7 7 01 2001 5 5 0 01 2001 7 8 10 2001 5 1 01 2001 7 9 01 2001...

Page 6: ...tion Limitations 2 an approved section Emergency procedures 3 an approved section Normal procedures 4 an approved section Performance 5 a partly approved section Weight and balance equipment list 6 a...

Page 7: ...R Date of Issue 01 2001 Revision Document No EV2000RLPEN SECTION 1 1 GENERAL 1 1 Introduction 1 2 Certification basis 1 3 Warnings cautions and notes 1 4 Descriptive data 1 4 1 Aircraft description 1...

Page 8: ...ent operation of the EV 97 EUROSTAR model 2000 version R ultra light aeroplane It also contains supplemental data supplied by the aeroplane manufacturer 1 2 Certification basis This aircraft type has...

Page 9: ...e flight manual WARNING Means that the non observation of the corresponding procedure leads to an immediate or important degradation of the flight safety CAUTION Means that the non observation of the...

Page 10: ...EUROSTAR model 2000 version R is a single engine all metal low wing monoplane of semimonocoque construction with two side by side seats The aeroplane is equipped with a fixed tricycle undercarriage w...

Page 11: ...21 m2 2 26 ft 2 Flap area 0 52 m2 5 60 ft 2 Fuselage length 5 98 m 19 62 ft width 1 04 m 3 41 ft height 2 34 m 7 67 ft Horizontal tail unit span 2 5 m 8 20 ft area 1 95 m2 20 99 ft 2 elevator area 0 8...

Page 12: ...rs si io on n R R Date of Issue 01 2001 Revision Document No EV2000RLPEN 1 5 Three view drawing 8 1 m 26 57 ft 2 5 m 8 2 ft 2 34 m 7 7 ft 19 62 ft 5 98 m 2 25 m 7 38 ft 0 94 m 3 1 ft 4 42 ft 1 35 m 1...

Page 13: ...2 2 Airspeed 2 3 Airspeed indicator markings 2 4 Powerplant 2 5 Powerplant instrument markings 2 6 Miscellaneous instrument markings 2 7 Weight 2 8 Centre of gravity 2 9 Approved manoeuvres 2 10 Manoe...

Page 14: ...nd their operational significance are shown below IAS Speed km h kts Remarks VNE Never exceed speed 270 146 Do not exceed this speed in any operation VA Manoeuvring speed 160 86 Do not make full or ab...

Page 15: ...cance are shown below IAS value or range Marking km h kts Significance White arc 58 125 31 67 Positive Flap Operating Range Green arc 75 190 40 103 Normal Operating Range Yellow arc 190 270 103 146 Ma...

Page 16: ...um 60 C 140 F 60 C 140 F Cylinder head temperature Maximum 150 C 302 F 135 C 275 F Minimum 50 C 122 F 50 C 122 F Maximum 140 C 284 F 130 C 266 F Oil temperature Optimum 90 C 110 C 194 230 F 90 C 110 C...

Page 17: ...unction Minimum Limit red line Normal Operating green arc Caution Range yellow arc Maximum Range red line Engine speed RPM 1400 1400 5500 5500 5800 5800 Exhaust Gases Temperature EGT 880 C R 912 UL 10...

Page 18: ...0 0 v ve er rs si io on n R R Date of Issue 01 2001 Revision Document No EV2000RLPEN 2 6 Miscellaneous instrument markings Fuel gauge A fuel reserve of 11 litre 2 90 USgals is indicated by yellow pilo...

Page 19: ...0 kg 992 lbs Max weight of fuel 47 kg 104 lbs Max baggage weight 15 kg 33 lbs 2 8 Centre of gravity Empty aircraft C G position standard 18 2 MAC Operating C G range 20 34 MAC 2 9 Approved manoeuvres...

Page 20: ...DBOOK 2 7 EURO STAR EV 97 M MO OD DE EL L 2 20 00 00 0 v ve er rs si io on n R R Date of Issue 01 2001 Revision Document No EV2000RLPEN 2 10 Manoeuvring load factors I N F O M A I O N O N R R T I N F...

Page 21: ...see 6 2 WARNING Abide with max take off weight 450 kg 992 lb 2 12 Kinds of operation There are permitted day VFR flights only WARNING IFR flights and flights under icing conditions are PROHIBITED Ins...

Page 22: ...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 NOTE Use only fuel suitable f...

Page 23: ...O STAR EV 97 M MO OD DE EL L 2 20 00 00 0 v ve er rs si io on n R R Date of Issue 01 2001 Revision Document No EV2000RLPEN 2 15 Other limitations No smoking onboard the aeroplane I N F O M A I O N O N...

Page 24: ...conditions 5800 5500 1400 ENGINE SPEED Max Take off max 5 min Max Continuous Idling 5800 5500 1400 rpm rpm rpm Aerobatics and intentional spins are prohibited AIRSPEED IAS Never exceed Manoeuvring Ma...

Page 25: ...OPERATING HANDBOOK 2 12 EURO STAR EV 97 M MO OD DE EL L 2 20 00 00 0 v ve er rs si io on n R R Date of Issue 01 2001 Revision Document No EV2000RLPEN I N F O M A I O N O N R R T I N F O M A I O N O N...

Page 26: ...failure during take off 3 2 3 Engine failure in flight 3 3 In Flight start 3 4 Smoke and fire 3 4 1 Fire on ground 3 4 2 Fire during take off 3 4 3 Fire in flight 3 5 Glide 3 6 Landing emergencies 3...

Page 27: ...red and applied as necessary to correct the problem 3 2 Engine failure 3 2 1 Engine failure during take off run 1 Throttle decrease to idling 2 Ignition switch off 3 Brake 3 2 2 Engine failure during...

Page 28: ...below 50 m 160 ft land in flight direction over 50 m 160 ft choose landing area 3 Wind evaluate direction and velocity 4 Landing area choose free area without obstacles 5 Flaps extend if necessary 6 F...

Page 29: ...1 3 power 9 Ignition box switch to BOTH and activate starter If the engine cannot be started increase the flight speed to 200 km h 110 kts 124 mph so that air flow can rotate the propeller thus enabli...

Page 30: ...e if it is in your power or call for a fire brigade 3 4 3 Fire in flight 1 Fuel cock shut off 2 Throttle full 3 Master switch switch off 4 Ignition switch off after using up fuel in carburettors and e...

Page 31: ...3 Instruments within permitted limits 3 6 Landing emergencies 3 6 1 Emergency landing 1 Emergency landings are generally carried out in the case of engine failure and the engine cannot be re started...

Page 32: ...ncreased idling with fully extended flaps 6 Reduce power to idle run when fly over the runway threshold and touch down at the very beginning of the chosen area 7 After stopping the aeroplane switch of...

Page 33: ...information The aircraft has no tendency to spontaneously enter into an uncontrollable spin if normal piloting techniques are used This standard procedure can be used to recover from an intentional s...

Page 34: ...g Carburettor icing mostly occurs when entering into an area of ice formation The carburettor icing shows itself through a decrease in engine power and an increase of engine temperatures To recover th...

Page 35: ...l procedures 4 4 1 Before entering cockpit 4 4 2 After entering cockpit 4 4 3 Before engine starting and Engine starting 4 4 4 Engine warm up Engine check 4 4 5 Taxiing 4 4 6 Before take off 4 4 7 Tak...

Page 36: ...nd in section 9 4 2 Assembly and disassembly For assembly and disassembly procedures refer to the Technical Description Operating and Maintenance Manual for the Ultra light Aeroplane EV 97 EUROSTAR mo...

Page 37: ...ment of position lights if installed 3 Aileron Surface condition Attachment Play Free movement 4 Flap Surface condition Attachment Play 5 Rear part of fuselage Surface condition 6 Vertical tail unit S...

Page 38: ...long time Avoid excessive pressure on a blade tip and trailing edge 15 Propeller Propeller attachment Blades Hub Spinner condition Other checks according to propeller manufacturer instructions 16 Coc...

Page 39: ...4 4 2 After entering cockpit 1 Rudder pedals free movement check 2 Brakes check of function 3 Control stick free movement check 4 Trim check of lever movement 5 Flaps check of function 6 Engine contro...

Page 40: ...ng set throttle to idling 12 Oil pressure within 10 sec min pressure 13 Choke push to shut 14 Engine warm according to 4 4 4 CAUTION The starter should be activated for a maximum of 10 sec followed by...

Page 41: ...fference between circuits R and L should be 115 rpm Set max power for verification of max speed with given propeller and engine parameters temperatures and pressures Check acceleration from idling to...

Page 42: ...s switched on 11 Instruments COMM FLYdat within limits 12 Safety harness secured and tightened 13 Cockpit locked 4 4 7 Take off By gradually increasing power set the aircraft into motion The direction...

Page 43: ...ul within permitted limits of airspeeds configurations and C G range The aircraft is very easy to both control and manoeuvre For more details about horizontal flight regimes refer to the Section 5 par...

Page 44: ...EURO STAR EV 97 M MO OD DE EL L 2 20 00 00 0 v ve er rs si io on n R R Date of Issue 01 2001 Revision Document No EV2000RLPEN 5 Landing area check runway area base leg area I N F O M A I O N O N R R...

Page 45: ...ed 110 km h 60 kts 68 mph 2 Flaps Landing position 3 Trim adjust 4 Throttle as necessary 5 Propeller in case of constant speed prop check setting of control overswitch to MANUAL position 6 Instruments...

Page 46: ...r switch switch off 8 Fuel cock shut off CAUTION Rapid engine cooling should be avoided during operation This happens above all during aircraft descent taxiing low engine rpm or at engine shutdown imm...

Page 47: ...data 5 2 1 Airspeed indicator system calibration 5 2 2 Stall speeds 5 2 3 Take off performance 5 2 4 Landing distances 5 2 5 Climb performance 5 3 Additional information 5 3 1 Cruise 5 3 2 Endurance...

Page 48: ...n approved additional information The data in the charts has been computed from actual flight tests with the aircraft and engine in good conditions and using average piloting techniques If not stated...

Page 49: ...vSO 60 67 35 38 70 76 40 43 vS1 vS1 75 80 45 47 80 85 50 52 90 94 55 57 100 103 60 61 110 112 67 67 vFE 120 121 70 70 vFE 125 126 75 75 130 130 80 79 140 139 86 84 vA 150 148 90 88 vA 160 157 95 93 17...

Page 50: ...excessive loss 57 64 LANDING Idling of altitude during 64 71 1st Position MCP recovery 52 60 LANDING Idling 60 67 2nd position MCP 50 58 Stall Flap setting Power setting Warning speed Stalling speed...

Page 51: ...mperature of 15 C 59 F RWY Take off run distance Take off distance over 15 m 50 ft obstacle m ft m ft CONCRETE 145 475 280 919 GRASS 155 509 300 984 5 2 4 Landing distances Landing distances stated in...

Page 52: ...ce EV 97 EUROSTAR Rate of climb engine Rotax 912 UL 80hp propeller V 230C fixed wooden two blade 18 40 0 0 0 5 1 0 1 5 2 0 2 5 3 0 3 5 4 0 4 5 5 0 80 85 90 95 100 105 110 115 120 125 130 135 140 145 1...

Page 53: ...peller V 230C 18 40 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 3200 3300 3400 3500 3600 3700 3800 3900 4000 4100 4200 4300 4400 4500 4600 4700 4800 4900 5000 5100 5200 5300 5400 5500 5...

Page 54: ...speed RPM 4000 4200 4500 4800 5000 5200 5500 5750 IAS km h 126 135 149 164 173 183 198 210 TAS km h 126 135 148 161 169 178 191 202 IAS km h 122 131 145 159 168 177 191 203 TAS km h 126 134 147 160 1...

Page 55: ...reserve 11 litres 2 9 Usgals indicated by yellow warning lamp Altitude 500 m ISA Engine speed rpm 4000 4200 4500 4800 5000 5200 5500 Fuel consumption l h 12 2 13 7 16 3 19 0 20 8 22 7 25 5 IAS km h 12...

Page 56: ...Balked landing climb EV 97 EUROSTAR Balked landing climb engine Rotax 912 UL 80hp propeller V 230C fixed wooden two blade 18 40 0 0 0 5 1 0 1 5 2 0 2 5 3 0 3 5 4 0 4 5 65 70 75 80 85 90 95 100 105 11...

Page 57: ...wind performance Max permitted cross wind velocity for take off and landing 5 m s 10 kts Max permitted head wind velocity for take off and landing 12 m s 23 kts 5 3 6 Ceiling Service ceiling 5000 m 16...

Page 58: ...EL L 2 20 00 00 0 v ve er rs si io on n R R Date of Issue 01 2001 Revision Document No EV2000RLPEN SECTION 6 6 WEIGHT AND BALANCE 6 1 Introduction 6 2 Weight and balance record Permitted payload rang...

Page 59: ...n contains the payload range within which the aircraft may be safely operated Procedures for weighing the aircraft and the calculation method for establishing the permitted payload range are contained...

Page 60: ...1 49 litre 12 9 USgalls 35 kg 77 lbs 1 65 litre 17 2 USgalls 47 kg 104 lbs max 15 kg 33 lbs 1 2 8 kg 17 lbs No baggage max 15 kg 33 lbs 1 2 8 kg 17 lbs No baggage max 15 kg 33 lbs 1 2 8 kg 17 lbs No...

Page 61: ...2 Airframe 7 2 1 Fuselage 7 2 2 Wing 7 2 3 Horizontal tail unit HTU 7 2 4 Vertical tail unit VTU 7 3 Controls in the cockpit 7 4 Instrument panel 7 5 Landing gear 7 6 Seats and safety harness 7 7 Bag...

Page 62: ...is an integral part of the fuselage In the middle section of the fuselage there is a two man cockpit which is accessible by unfolding the one part perspex overlap canopy The engine section in the nos...

Page 63: ...vision Document No EV2000RLPEN 7 2 4 Vertical tail unit VTU The trapezoidal fin section of the VTU is mounted to the rear section of the fuselage The rudder is attached on the fin by two hinges The fr...

Page 64: ...NDBOOK 7 3 EURO STAR EV 97 M MO OD DE EL L 2 20 00 00 0 v ve er rs si io on n R R Date of Issue 01 2001 Revision Document No EV2000RLPEN 7 3 Controls in the cockpit I N F O M A I O N O N R R T I N F O...

Page 65: ...0 v ve er rs si io on n R R Date of Issue 01 2001 Revision Document No EV2000RLPEN 7 4 Instrument panel The aeroplane EV 97 EUROSTAR model 2000 version R S N XXXXXXXXXX is equipped with the following...

Page 66: ...leg is welded from steel tubes and its suspension is made from rubber rope The nose wheel steering system is connected to the rudder control The wheels may be equipped with aerodynamic fiberglass cove...

Page 67: ...sible for the canopy to be tilted forward For easier manipulation the weight of the canopy is counterbalanced by two gas struts which allow it to open effortlessly On the lower frame there are handles...

Page 68: ...x 912 is 4 stroke 4 cylinder horizontally opposed spark ignition engine with one central camshaft push rod OHV Liquid cooled cylinder heads ram air cooled cylinders Dry sump forced lubrication Dual br...

Page 69: ...ponding quantity in litres is shown in the table 6 2 and on placard LOAD LIMITS in the cockpit 7 11 Electrical system The electric system is single wire type with the negative connected to the chassis...

Page 70: ...rough flexible plastic hoses Keep the system clear to assure its right function Both the dynamic and static hose systems are equipped with dirt pockets The dirt pockets are located inside the cockpit...

Page 71: ...on n R R Date of Issue 01 2001 Revision Document No EV2000RLPEN 7 13 Miscellaneous equipment Besides the instruments stated in par 7 14 the EV 97 EUROSTAR model 2000 version R aeroplane S N XXXXXXX i...

Page 72: ...version R S N XXXXXXX is additionally equipped with the following instruments NOTE Refer to the documentation supplied with non standard instruments for operating instructions Engine instruments The...

Page 73: ...LPEN SECTION 8 8 Aeroplane handling servicing and maintenance 8 1 Introduction 8 2 Aircraft inspection periods 8 3 Aircraft alterations or repairs 8 4 Ground handling Road transport 8 4 1 Towing 8 4 2...

Page 74: ...mends that maintenance checks and periodic inspections should be carried out in the following periods at least a after the first 25 2 flight hours b after every 50 3 flight hours c after every 100 5 f...

Page 75: ...roots A tow bar may be used to tow the aeroplane a long distance CAUTION Avoid excessive pressure at the aeroplane airframe especially at the wing tips elevator rudder trim etc CAUTION Handle the pro...

Page 76: ...akers and Master switch switched off Switch box switched off 2 Block the control stick up e g by means of safety harness or connect the control stick with rudder pedals by means of a suitable rope 3 S...

Page 77: ...k the rear part of the aircraft handle the fuselage near the auxiliary tail skid lift it upward and support To lift the wings push from underneath the wings only at the main spar Avoid lifting the win...

Page 78: ...ter and an adequate quantity of a detergents Use either a soft clean cloth sponge or deerskin Then use suitable polishers to clean the canopy CAUTION Never clean the canopy under dry conditions and ne...

Page 79: ...E EL L 2 20 00 00 0 v ve er rs si io on n R R Date of Issue 01 2001 Revision Document No EV2000RLPEN SECTION 9 9 Supplements 9 1 Introduction 9 2 List of inserted supplements 9 3 Supplements inserted...

Page 80: ...N 9 1 Introduction This section contains the appropriate supplements necessary to safely and efficiently operate the aircraft when equipped with various optional systems and equipment not provided wit...

Page 81: ...ANDBOOK 9 2 EURO STAR EV 97 M MO OD DE EL L 2 20 00 00 0 v ve er rs si io on n R R Date of Issue 01 2001 Revision Document No EV2000RLPEN 9 3 Supplements inserted I N F O M A I O N O N R R T I N F O M...

Page 82: ...S OPERATING HANDBOOK 0 EURO STAR EV 97 M MO OD DE EL L 2 20 00 00 0 v ve er rs si io on n R R Date of Issue 01 2001 Revision Document No EV2000RLPEN I N F O M A I O N O N R R T I N F O M A I O N O N...

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