1. Manuals
  2. Brands
  3. EVEKTOR-AEROTECHNIK Manuals
  4. Aircrafts
  5. EV-97? EUROSTAR ?model 2000 version R
  6. Operating & maintenance manual

EVEKTOR-AEROTECHNIK EV-97 Eurostar 2000 Operating & Maintenance Manual

Hide thumbs Also See for EV-97 Eurostar 2000:
Table of Contents

Advertisement

Quick Links

Download this manual See also: Pilot Operating Handbook
EVEKTOR - AEROTECHNIK
Airport, Kunovice
686 04 Kunovice
Czech Republic
tel.: 00420 572 537 111
fax: 00420 572 537 900
EV-97
M
O
D
E
L
2
0
0
0
M
O
D
E
L
2
0
0
0
v
e
r
s
i
o
n
R
v
e
r
s
i
o
n
R
EURO
STAR

Advertisement

Table of Contents
loading
Need help?

Need help?

Do you have a question about the EV-97 Eurostar 2000 and is the answer not in the manual?

Questions and answers

Related Manuals for EVEKTOR-AEROTECHNIK EV-97 Eurostar 2000

Summary of Contents for EVEKTOR-AEROTECHNIK EV-97 Eurostar 2000

  • Page 1 EVEKTOR - AEROTECHNIK Airport, Kunovice 686 04 Kunovice Czech Republic tel.: 00420 572 537 111 fax: 00420 572 537 900 EURO EV-97 STAR...
  • Page 2 © EVEKTOR - AEROTECHNIK , 2001...
  • Page 3 EVEKTOR - AEROTECHNIK Airport, Kunovice 686 04 Kunovice Czech Republic tel.: 00420 572 537 111 fax: 00420 572 537 900 EV-97 EUROSTAR Model: model 2000 version R Serial Number: Registration: Owner: ........................................ Document No.: Date of Issue: Revision: EV2000RNOEN 01/2001...
  • Page 4 The manufacturer invites suggestions and reminders concerning this manual, and appreciates proposals for corrections. We invite you to share your experiences with us during operation of your EURO EV-97 STAR...

  • Page 5: General

    EV-97 EURO STAR 1. GENERAL Document No.: Date of Issue: Revision: EV2000RNOEN 01/2001...

  • Page 6: Record Of Revisions

    EURO EV-97 STAR Record of revisions Any revisions or amendments to this manual shall be issued in the form of bulletins with attached new pages. It is in the interests of every user to enter such revision into the table of revisions and to replace the existing page by the new one.

  • Page 7: List Of Effective

    EV-97 EURO STAR List of Effective Pages Sec. Page Date Sec. Page Date Sec. Page Date Sec. Page Date Sec. Page Date 2-27 01/2001 01/2001 01/2001 01/2001 2-28 01/2001 01/2001 01/2001 01/2001 2-30 01/2001 01/2001 01/2001 01/2001 2-31 01/2001 01/2001 01/2001 01/2001 01/2001...

  • Page 8: Table Of Contents

    EURO EV-97 STAR Contents GENERAL ............................1-1 ........................1-2 ECORD OF REVISIONS ........................1-3 IST OF FFECTIVE AGES ............................1-4 ONTENTS TECHNICAL DESCRIPTION ......................2-1 ...................... 2-2 ASIC AND GENERAL INFORMATION 2.1.1 Designation ..........................2-2 ........................2-3 ASIC TECHNICAL DATA 2.2.1 Airplane views ...........................
  • Page 9 EV-97 EURO STAR 3.6.1 Empty weight determination ....................3-22 3.6.2 Operating C.G. Range calculation ..................3-23 .......................... 3-24 ROUND HANDLING 3.7.1 Towing the airplane......................... 3-24 3.7.2 Parking the airplane ........................ 3-24 3.7.3 Tieing-Down..........................3-24 3.7.4 Jacking the airplane ........................ 3-25 ..........................
  • Page 10 EURO EV-97 STAR ....................... 5-6 IBERGLASS PARTS REPAIRS ........................... 5-6 AINT REPAIRS ................5-6 IRPLANE ASSEMBLY AND LEVELING AFTER A REPAIR ......................5-7 IRST FLIGHT AFTER A REPAIR .......................... 5-7 PARE PARTS ORDER APPENDICES ..........................6-1 .......................... 6-2 IST OF PPENDICES Date of Issue: Revision:...

  • Page 11: Technical Description

    EV-97 EURO STAR 2. TECHNICAL DESCRIPTION Document No.: Date of Issue: Revision: EV2000RNOEN 01/2001...

  • Page 12: Basic And General Information

    EURO EV-97 STAR Basic and general information is a single engine, all metal, low-wing EV-97 „EUROSTAR“ model 2000 version R monoplane of semimonocoque construction with two side-by side seats. The aircraft is equipped with fixed, tricycle landing gear. The standard powerplant consists of the four-cylinder, 4 stroke, ROTAX 912 (80 hp) engine and the two blade, wooden, V 230 C fixed prop.

  • Page 13: Basic Technical Data

    EV-97 EURO STAR Basic technical data 2.2.1 Airplane views Document No.: Date of Issue: Revision: EV2000RNOEN 01/2001...

  • Page 14: Three-View Drawing

    EURO EV-97 STAR 2.2.2 Three-view drawing 26.57 ft 8.1 m 8.2 ft 2.5 m 7.38 ft 3.1 ft 2.25 m 0.94 m Date of Issue: Revision: Document No.: 01/2001 EV2000RNOEN...

  • Page 15: Basic Dimensions

    EV-97 EURO STAR 2.2.3 Basic dimensions Wing span..............26.57 ft area ...............105.92 sq ft 9.84 m MAC ..............4.10 ft 1.25 m loading (MTOW 992 lb, 450 kg) ....9.37 lbf/sq ft 45.7 kg/m (MTOW 1058 lb, 480 kg) ....9.99 lbf/sq ft 48,8 kg/m Aileron area............2.26 sq ft 0.21 m...

  • Page 16: Weight

    EURO EV-97 STAR 2.2.4 Weight Empty weight (standard equipment) ..........606 lbs± 3% 275 kg ± 3% Maximum Take-off weight (Czech Rep., Germany..)....992 lbs 450 kg (Slovak Republic, Canada)..1058 lbs 480 kg Maximum Landing weight (Czech Rep., Germany..)....992 lbs 450 kg (Slovak Republic, Canada)..1058 lbs 480 kg Maximum fuel weight...

  • Page 17: Technical Description Of The Airplane

    EV-97 EURO STAR Technical description of the airplane 2.3.1 General airframe is of semi-monocoque construction EV-97 „EUROSTAR“ model 2000 version R formed with metal reinforcements, bulkheads and duralumin cover. Pop-rivets are used for joints and some non-supporting parts are made from fiberglass. 2.3.2 Fuselage The fuselage has a semi-monocoque construction formed with reinforcements and duralumin...

  • Page 18: Horizontal Tail Unit

    EURO EV-97 STAR 2.3.4 Horizontal tail unit The rectangular HTU consists of a stabilizer and elevator with a trim tab. The semi-monocoque construction of the HTU consists of duralumin ribs, spar and cover. The width of 8.2 ft (2.5 m) enables transport without dismantling.

  • Page 19: Landing Gear

    EV-97 EURO STAR 2.3.6 Landing gear 2.3.6.1 General description The aircraft is equipped with fixed nosewheel landing gear. The nosewheel is steerable, but as an option, can be casterable, only. Fig. EV-97 Eurostar 1 - Steerable nosewheel 2 - Main landing gear 2.3.6.2 Main landing gear 2.3.6.2.1 Description The main landing gear consists of the left and right landing gear legs.
  • Page 20 EURO EV-97 STAR 2.3.6.3.2 Main landing gear layout MAIN LEG ATTACHMENT ANGLE REINFORCEMENT MAIN LEG ATTACHMENT MAIN LEG WHEEL WITH BRAKE SCREW 4x40 ČSN 02 1781.04 MAIN LEG NUT M16x1.5 ČSN 02 1412.24 WASHER SCREW 5x10 ČSN 02 2150.01 FLIGHT DIRECTION Fig.
  • Page 21 EV-97 EURO STAR 2.3.6.3.3 Steerable nosewheel landing gear layout FUSELAGE FRAME SUSPENSION STOP NOSE WHEEL LEG RUBBER ROPE SUSPENSION FOOT PEDAL NOSE WHEEL 17 ° CONTROL ROD COTTER PIN 4x40 ČSN 02 1781.04 NUT 765 155 WHEEL AXLE WASHER 765 478 WASHER E 54-04 21 NOSE WHEEL ASSEMBLY...
  • Page 22 EURO EV-97 STAR 2.3.6.4 Auxiliary tail skid 2.3.6.4.1 Description The auxiliary tail skid is attached at the lower rear part of the fuselage and protects the aircraft from inadvertent damage during tail-down landing conditions. The tail skid is formed from composite material.
  • Page 23 EV-97 EURO STAR 2.3.6.5 Wheel brakes 2.3.6.5.1 Description Both wheels on the main landing gear are equipped with hydraulic disc brakes. The brake system consists of the brake pedals (pilot standard, co-pilot as an option), hydraulic brake master cylinders, plastic hoses, brake caliper with the hydraulic brake cylinder, brake pads and the brake disc which is bolted onto the inner part of the rim.
  • Page 24 EURO EV-97 STAR 2.3.6.5.3 Brake system layout FLIGHT DIRECTION TIGHTENING STRIP 2.5x98 BRAKE HOSE FOLYFLEX L EMPFIMASTIC PU 50 FUSELAGE FRAME CRAMP 1x8 TIGHTENING STRIP MASTER CYLINDER PIN 5x20 ONL 3331.1 WASHER 5.2 ČSN 02 1702.14 COTTER PIN 1.2x12 ČSN 02 1781.04 MASTER CYLINDER ELBOW - "KNOMI"...
  • Page 25 EV-97 EURO STAR 2.3.6.6 Wheels 2.3.6.6.1 Description All the wheels consist of a two-part casting rim with a tire and tube. The main wheels are on an axle attached to the main gear leg, fastened by the nuts. 2.3.6.6.2 Main undercarriage wheel layout WHEEL WITH BRAKE SCREW 4x40 ČSN 02 1781.04 MAIN LEG...

  • Page 26: Cockpit

    EURO EV-97 STAR 2.3.6.7 Tires Main landing gear........ SAVA 14x4 (standard) or ptional: DELI TIRE 15 x 6.00 - 6 (aircraft tire) AIR TRACK 15 x 6.00 - 6 (aircraft tire) TOST 15 x 6.00 – 6 (aircraft tire) Nose landing gear ....... SAVA 14x4 (standard) or ptional: DELI TIRE 15 x 6.00 - 6 (aircraft tire) AIR TRACK 15 x 6.00 - 6 (aircraft tire)
  • Page 27 EV-97 EURO STAR 2.3.7.2 Cockpit controls The standard cockpit control arrangement is shown in the following figure. A detailed instrument panel is shown in par. 2.3.8.3. Fig. quadrant between the seats 1- flaps control lever, 2 - elevator trim tab control lever Document No.: Date of Issue: Revision:...
  • Page 28 EURO EV-97 STAR 2.3.7.3 Cockpit canopy The semi-tear shape cockpit canopy consists of two parts. The front perspex portion can be tilted forward and is attached to a steel frame. The fixed rear portion can be made of either Al-alloy sheet or perspex.

  • Page 29: Equipment

    EV-97 EURO STAR 2.3.8 Equipment 2.3.8.1 Seats and safety harness The plane has two side-by-side seats which are fixed and covered with upholstery, each equipped with seatbelts. Adjustable rudder pedals are optional. The seatbelts are attached alongside the seat and in the middle of the bulkhead behind the baggage compartment. The seatbelts can be provided as either three or four point safety belts.

  • Page 30: Instrument Panel

    EURO EV-97 STAR 2.3.8.3 Instrument panel The following instrument panel is installed in the EV-97 “EUROSTAR” model 2000 version R airplane, S/N : (example) Date of Issue: Revision: Document No.: 2-20 01/2001 EV2000RNOEN...

  • Page 31: Avionics

    EV-97 EURO STAR 2.3.9 Avionics The following instruments are installed in airplane, EV-97 “EUROSTAR” model 2000 version R ……………….: (example) 2.3.9.1 Flight and navigation instruments 1 Airspeed indicator ....1 Altimeter ......... 1 Compass ........ 1 Variometer......1 Bank indicator ......NOTE Refer to the Manuals supplied with above listed instruments for operation.

  • Page 32: Additional Equipment

    EURO EV-97 STAR 2.3.10 Additional equipment The following optional equipment is installed in the EV-97 „EUROSTAR“ model 2000 version R airplane, S/N • Date of Issue: Revision: Document No.: 2-22 01/2001 EV2000RNOEN...
  • Page 33 EV-97 EURO STAR Intentionally left blank Document No.: Date of Issue: Revision: 2-23 EV2000RNOEN 01/2001...
  • Page 34 EURO EV-97 STAR Intentionally left blank Date of Issue: Revision: Document No.: 2-24 01/2001 EV2000RNOEN...

  • Page 35: Control System

    EV-97 EURO STAR 2.3.11 Control system 2.3.11.1 Longitudinal control system description The airplane is equipped with a classic dual control system. The elevator is controlled by a control stick, with connecting rods and arms. A control stick push/pull movement is transmitted, by a rod inside the quadrant between the seats to the elevator through a two-armed lever located underneath the baggage compartment floor cover.
  • Page 36 EURO EV-97 STAR 2.3.11.4 Flap control system description The wing flaps are controlled by a control lever in a changing gate. The lever push/pull movement is transferred to a longitudinal movement of a rod guided inside the quadrant between the seats. Then to an angular displacement of a two-armed lever welded onto a tube connecting left and right flap.
  • Page 37 EV-97 EURO STAR 2.3.11.7 Longitudinal control system layout Document No.: Date of Issue: Revision: 2-27 EV2000RNOEN 01/2001...
  • Page 38 EURO EV-97 STAR 2.3.11.7.1 Lateral control system layout Date of Issue: Revision: Document No.: 2-28 01/2001 EV2000RNOEN...
  • Page 39 EV-97 EURO STAR 2.3.11.8 Directional control system layout Document No.: Date of Issue: Revision: 2-29 EV2000RNOEN 01/2001...
  • Page 40 EURO EV-97 STAR 2.3.11.9 Flap control system layout Date of Issue: Revision: Document No.: 2-30 01/2001 EV2000RNOEN...
  • Page 41 EV-97 EURO STAR 2.3.11.10 Trim tab control system layout Document No.: Date of Issue: Revision: 2-31 EV2000RNOEN 01/2001...
  • Page 42 EURO EV-97 STAR 2.3.11.11 Nosewheel control system layout FRAME SYSTEM NOSE WHEEL LEG NUT M6 ČSN 02 1413.44 CONTROL WASHER 6 ČSN 31 3282.11 COTTER PIN 1.6x14 ČSN 02 1781.05 TIGHTENING STRIP E (2:1) WASHER 6 ČSN 31 3282.11 SCREW 6x25 ČSN 02 1413.44 NUT M6 ČSN 02 1413.44 COTTER PIN 1.6x14 ČSN 02 1781.05 Date of Issue:...

  • Page 43: Powerplant

    EV-97 EURO STAR 2.3.12 Powerplant 2.3.12.1 Brief description The standard powerplant consists of the four-cylinder, 4 stroke ROTAX 912 (A or UL version, 80 hp) engine and 2 blade, wooden, V 230 C fixed prop. The ROTAX 912 S resp. ULS (100 hp) engine may be installed as option.
  • Page 44 EURO EV-97 STAR 2.3.12.2 Engine 2.3.12.2.1 Description The Rotax 912 S is a 4-stroke, 4 cylinder, horizontally opposed, spark ignition engine and has one central camshaft-push-rods-OHV. Liquid cooled cylinder heads, ram air cooled cylinders. Dry sump forced lubrication. Dual breakerless capacitor discharge ignition. The engine is fitted with electric starter, AC generator and mechanical fuel pump.

  • Page 45: C Ontents

    EV-97 EURO STAR 2.3.12.2.2 Technical data ROTAX 912 engine is installed in the aircraft of S/N Engine Model: ROTAX 912A (or UL) ROTAX 912S (or ULS) Engine Manufacturer: Bombardier-Rotax GMBH 59.6 kW / 80 hp 73.5 kW / 100 hp Max Take-off: at 5800 rpm, max.5 min.
  • Page 46 EURO EV-97 STAR 2.3.12.3 Propeller 2.3.12.3.1 Description The standard powerplant consists of the four-cylinder, 4 stroke ROTAX 912 (80 hp) engine and V 230 C prop. The V 230 C is a fixed, wooden, 2-blade propeller with leading edge protection. The prop is attached to the propeller hub with 6 bolts.
  • Page 47 EV-97 EURO STAR 2.3.12.3.2 Propeller pitch adjustment Intentionally left blank. Document No.: Date of Issue: Revision: 2-37 EV2000RNOEN 01/2001...
  • Page 48 EURO EV-97 STAR 2.3.12.4 The FLYdat engine instrument The Rotax 912 engine parameters are monitored by the integrated digital instrument (FLYdat) (standard equipment). The following parameters are displayed: • Engine speed • Engine hours • Exhaust gases temperature • Cylinder head temperature •...
  • Page 49 EV-97 EURO STAR If analog engine instruments are installed (instead of the FLYdat instrument) then the instruments limit indicators should show the following: Function Minimum Normal Caution Maximum Limit Operating Range Range Engine speed 1400 1400-5500 5500-5800 5800 [RPM] R 912 UL 100-150 °C Cylinder 150 °C...

  • Page 50: Engine Mount

    EURO EV-97 STAR 2.3.12.5 Engine mount 2.3.12.5.1 Description The engine mount is welded from chrome-molybdenum tubes and is attached to the firewall with 4 bolts. The bed is spring-mounted with four rubber silentblocks. Fig. Engine mount 1- bed, 2 - rubber silentblock 2.3.12.5.2 Engine mount diagram Date of Issue: Revision:...
  • Page 51 EV-97 EURO STAR 2.3.12.6 Engine cowlings 2.3.12.6.1 Description There are two fiberglass cowlings (upper and lower) attached to the engine mount which cover the engine. The interior sides of the cowlings are protected with fireproof paint, exterior sides are painted with aircraft paint. The upper cowling is connected to the lower cowling with quick-closing locks and is usually removed for preflight inspections.

  • Page 52: Fuel System

    EURO EV-97 STAR 2.3.13 Fuel system 2.3.13.1 Fuel system description The standard fuel tank volume is 17.2 USGAL (65 liter). The tank is located behind the seat backrests. Fuel is pulled from the fuel tank through the fuel valve located inside the cockpit on the left-hand side, below the instrument panel.
  • Page 53 EV-97 EURO STAR 2.3.13.2 Standard fuel system layout Date of Issue: Revision: Document No.: Date of Issue: Revision: 2-43 10/2001 EV2000RNOEN 01/2001...

  • Page 54: Engine Lubrication System Scheme

    EURO EV-97 STAR 2.3.13.3 Fuel tank draining The objective is to drain any water and/or contaminates in the fuel tank. Draining procedure: 1. Place a suitable bottle or transparent cup below the draining outlet hose (near the right-hand flap root) 2.

  • Page 55: Cooling System Description

    EV-97 EURO STAR 2.3.15 Cooling system description 2.3.15.1 Cooling system description The cooling system uses two forms of cooling. The cylinder heads are liquid cooled and the cylinders ram air cooled. The radiator is located in the front of the lower engine cowling. The coolant is forced through the radiator by a water pump, driven from the crankshaft to the cylinder heads.

  • Page 56: Ventilation

    EURO EV-97 STAR 2.3.17 Ventilation 2.3.17.1 Description Canopy vent windows: • The windshield air window - turn the window to open two air holes. It is highly recommended to close the window while the aircraft is parked to prevent water seeping onto the instrument panel.

  • Page 57: Wiring

    EV-97 EURO STAR 2.3.18 Wiring 2.3.18.1 Wiring description The electric system is a single-wire type with the negative side connected to the chassis. The power source is a single-phase generator integral to the engine. A 12V/16Ah maintenancefree battery is located on the firewall. The system is protected by the main 25 Amp circuit breaker or fuse.

  • Page 58: Pitot-Static System

    EURO EV-97 STAR 2.3.19 Pitot-static system 2.3.19.1 Pitot-static system description The Pitot-static tube, located under the left wing near the aileron root, provides both dynamic and static air pressure. Pressure distribution to individual instruments is done through flexible plastic hoses. Keep the system clear to ensure its correct function.

  • Page 59: Placards

    EV-97 EURO STAR 2.3.20 Placards A new aircraft is equipped with placards supplied by the airplane manufacturer. These placards explain the purpose of controls, instruments, airspeed limits, weight limits, etc. Placards with supplemetal information such as a direction of handles are also supplied. The placards are usually attached to the appropriate instruments and controls.
  • Page 60 EURO EV-97 STAR Intentionally left blank Date of Issue: Revision: Document No.: 2-50 01/2001 EV2000RNOEN...

  • Page 61: Operation

    EV-97 EURO STAR 3. OPERATION Document No.: Date of Issue: Revision: EV2000RNOEN 01/2001...

  • Page 62: Operation Outlines

    EURO EV-97 STAR Operation outlines During operation of the it is required to have in the EV-97 „EUROSTAR“ model 2000 version R following documentation in the plane: • Airplane Technical Description, Operating, Maintenance and Repair Manual EV-97 "EUROSTAR" model 2000 version R •...

  • Page 63: Airplane Assembly

    EV-97 EURO STAR Airplane assembly 3.2.1 Wing 3.2.1.1 Wing assembly The wing assembly procedure for an aircraft not-equipped with the optional wing folding mechanism is the following (3 persons are needed to accomplish this task): 3.2.1.1.1 Necessary tools • a hammer to move the wing suspension pins •...
  • Page 64 EURO EV-97 STAR 3.2.1.2 Wing disassembly 3.2.1.2.1 Necessary tools • a hammer to tap the wing suspension pins out • a screwdriver to unscrew the wing fillet connection screws • wrenches to unscrew the rear wing suspension bolt nut • a drift made from duralumin round or other suitable material (diameter 10-12 mm) to drive out the wing suspension pins 3.2.1.2.2 Wing-from-fuselage disassembly 1.
  • Page 65 EV-97 EURO STAR 3.2.1.3 Wing folding The aircraft may be equipped with the optional wing folding mechanism. The wing folding is convenient to reduce the parking area required in a hangar and to allow transportation on a suitable trailer. The wings may be folded in 15 minutes by 2 people. 3.2.1.3.1 Wing folding mechanism scheme Fig.
  • Page 66 EURO EV-97 STAR 3.2.1.3.3 Wing folding procedure 1. Insert plastic O-ring onto right strut, secure by cotter pin. Insert the right strut into the hole provided in the rear right side of fuselage. Put the strut through the fuselage (the holes in fuselage sides are covered with spring loaded covers).
  • Page 67 EV-97 EURO STAR 3.2.1.3.4 Wing reassemble procedure 1. An assistant holds the wing tip 2. Another person removes the safety pin securing the wing on the wing rest hinge 3. The assistant removes the wing from the rest (using caution with the pitot-static tube under left wing) 4.
  • Page 68 EURO EV-97 STAR Date of Issue: Revision: Document No.: 01/2001 EV2000RNOEN...
  • Page 69 EV-97 EURO STAR Document No.: Date of Issue: Revision: EV2000RNOEN 01/2001...

  • Page 70: Horizontal Tail Unit

    EURO EV-97 STAR 3.2.2 Horizontal tail unit 3.2.2.1 HTU-from-fuselage disassembly 1. Unscrew attachment bolts of HTU-fuselage fiberglass cover. 2. Disconnect the trim tab control cables. 3. Disconnect the elevator control rod. 4. Remove the safety pins securing the castle nuts on the bolts of the stabilizer rear suspensions. Screw off the nuts and remove the washers.

  • Page 71: Vertical Tail Unit

    EV-97 EURO STAR 3.2.3 Vertical tail unit 3.2.3.1 Assembly and Disassembly of the rudder 3.2.3.1.1 Necessary tools • a wrench to tighten/remove the M5 nut 3.2.3.1.2 Rudder-from-fuselage disassembly 1. Disconnect the rudder control cables, attach the ends of the cables together to keep the cables from sliping inside the fuselage.

  • Page 72: Landing Gear

    EURO EV-97 STAR 3.2.4 Landing gear 3.2.4.1 Tire replacement 1. Support the aircraft to lift a wheel with punctured tire. Main wheel: It is recommended to support the aircraft near the main gear leg entry into the fuselage (a reinforced area) Nose wheel: a) Push the rear of the fuselage down and support the aircraft under the nosewheel leg-fuselage attachment or...
  • Page 73 EV-97 EURO STAR 3.2.4.2 Assembly and disassembly of wheel pants An airplane may be equipped with the optional aerodynamic fiberglass wheel pants. 3.2.4.2.1 Main landing gear wheel pants The main wheel pant is attached with 8 screws to the main leg from the inner side and with 1 screw from the outer side.
  • Page 74 EURO EV-97 STAR 3.2.4.3 Removal and replacement of mudguards The aircraft may be equipped with optional mudguards to prevent wing lower surface pollution. 3.2.4.3.1 Main landing gear wheel mudguard Demounting 1. Support the airplane to lift the main wheel with the mudguard to be removed 2.

  • Page 75: Cockpit Canopy

    EV-97 EURO STAR 3.2.5 Cockpit canopy 3.2.5.1 Canopy demounting The front portion of the canopy can be removed, while the rear portion is fixed. The front section of the canopy is attached to the fuselage with two screws. The weight of canopy is counter-balanced with two gas struts inside the cockpit.

  • Page 76: Leveling

    EURO EV-97 STAR Leveling Leveling is used to check the airframe alignment. First set the aircraft in a horizontal position (use boards) according to leveling points. The leveling points are the rivets on the aircraft which are (generaly) marked with red paint. The location of the points is shown in the Leveling Record.

  • Page 77: Measurement Of Control Surfaces Deflections

    EV-97 EURO STAR Measurement of control surfaces deflections 3.4.1 Required deflections The deflection of the control surfaces are specified in the Control Surfaces Deflection Record (see Appendices of this Manual) and in the following Figure. A protractor with deflecting hand is used by the airplane manufacturer to measure deflections.

  • Page 78: Aileron Deflection Measurement

    EURO EV-97 STAR 3.4.2 Aileron deflection measurement Measurement procedure: 1. Attach a protractor with a deflection hand at the aileron upper surface by means of a clamp. 2. Set the aileron in neutral position (the aileron must fit the wing profile). 3.

  • Page 79: Elevator Deflections Measurement

    EV-97 EURO STAR 3.4.4 Elevator deflections measurement The starting position to measure the elevator deflections is the neutral positions of the control stick and elevator. The neutral position of the control stick is set by the aircraft manufacturer, by means of a jig.

  • Page 80: Trim Tab Deflections Measurement

    EURO EV-97 STAR 3.4.6 Trim tab deflections measurement The trim tab deflection is measured from the neutral position. When the trim tab profile does not protrude from the elevator profile with elevator set in neutral position. Measurement procedure: 1. Attach a protractor with a deflection hand at the trim tab 2.

  • Page 81: Permissible Tolerances

    EV-97 EURO STAR Permissible Tolerances The following table indicates the permissible tolerances for critical parts of the airplane. These values should not be exceeded in operation. It is expected that an operator will take steps if excessive plays are found on/in part not listed below.

  • Page 82: Weighing The Airplane And C.g. Calculation

    EURO EV-97 STAR Weighing the airplane and C.G. calculation WARNING Never exceed the maximum takeoff weight and c.g. range for any configuration of crew, fuel and baggage as shown in the flight manual. The removal or addition of equipment may result in changes to the center of gravity and empty weight of the aircraft.

  • Page 83: Operating C.g. Range Calculation

    EV-97 EURO STAR 3.6.2 Operating C.G. Range calculation On the basis of knowledge of arms, weights of items, airplane empty weight and the C.G. position it is possible to calculate weight and C.G. position according to below given formula: Item Arm to the Datum Weight Moment...

  • Page 84: Ground Handling

    EURO EV-97 STAR Ground handling 3.7.1 Towing the airplane It is easy to tow the airplane a short distance by holding the blade root, since the empty weight of this airplane is relatively low. Suitable surfaces to hold the aircraft airframe, are the rear part of the fuselage before the fin and the wing roots.

  • Page 85: Jacking The Airplane

    EV-97 EURO STAR 3.7.4 Jacking the airplane Because the empty weight of this airplane is relatively low it is easy to lift the airplane using 2 people. First prepare two suitable jacks to support the aircraft. The aircraft should be lifted by the following parts: •...
  • Page 86 EURO EV-97 STAR Intentionally left blank Date of Issue: Revision: Document No.: 3-26 01/2001 EV2000RNOEN...

  • Page 87: Maintenance

    EV-97 EURO STAR 4. MAINTENANCE Document No.: Date of Issue: Revision: EV2000RNOEN 01/2001...

  • Page 88: Overall Maintenance Survey

    EURO EV-97 STAR Overall maintenance survey Aircraft maintenance is required to mantain its airworthiness. Periodical events are performed (periodical and pre-flight inspections) along with irregular events e.g. a repair of a damage as required. Pre-flight inspection A pre-flight inspection is performed prior to the beginning of each flight. A pre-flight inspection should be repeated prior to each flight even during the same day.

  • Page 89: Periodical Inspections

    EV-97 EURO STAR Periodical inspections 4.4.1 Periodical inspection intervals The periods for overall checks and contingent maintenance will depend on the conditions of the operation and the overall condition of the airplane. The manufacturer recommends maintenance checks and periodic inspections in the following periods: 1) after the first 25 ±...

  • Page 90: Periodical Inspections - Events

    EURO EV-97 STAR 4.4.3 Periodical inspections - events Model: S/N.: Hours flown: Date of inspection: EV -97 EUROSTAR Registration: No. of Takeoffs: Inspection Tick off performed inspection Event Carried Inspected Event description every every after the first out by: hrs. hrs.
  • Page 91 EV-97 EURO STAR Inspection Tick off performed inspection Event Carried Inspected Event description every every after the first out by: hrs. hrs. hrs. 3.7. Cooling system 3.7.1. Visually check radiator for condition and leaks 3.7.2. Visually check condition, attachment of hoses; check system for leaks 3.7.3.
  • Page 92 EURO EV-97 STAR Inspection Tick off performed inspection Event Carried Inspected Event description every every after the first out by: hrs. hrs. hrs. 4.3.4. Pitch change mechanism (if controllable pitch prop is mounted) see manufacturer instructions Check condition and function according to the prop manufacturer´s instructions LANDING GEAR NOSEWHEEL LANDING GEAR...
  • Page 93 EV-97 EURO STAR Inspection Tick off performed inspection Event Carried Inspected Event description every every after the first out by: hrs. hrs. hrs. 6.1.4. Check cloth cover which covers the leg-fuselage input hole 6.2. Wheel pants or mudguards 6.2.1. Visually check wheel pants / mudguards condition - repair damage and cracks 6.3.
  • Page 94 EURO EV-97 STAR Inspection Tick off performed inspection Event Carried Inspected Event description every every after the first out by: hrs. hrs. hrs. 7.3.2. Check flap hinge 7.3.3. Check play 7.3.4. Check condition of flap control pin and wear of the groove at the flap root 7.3.5.
  • Page 95 EV-97 EURO STAR Inspection Tick off performed inspection Event Carried Inspected Event description every every after the first out by: hrs. hrs. hrs. Check play - move the stabilizer frontward- 9.5. rearward, upward-downward - contact the airplane manufacurer if play exceeded tolerances 9.6.
  • Page 96 EV-97 EURO STAR Inspection Tick off performed inspection Event Carried Inspected Event description every every after the first out by: hrs. hrs. hrs. 11.4.6. Pitostatic system drainage, see 2.3.19 11.4.7. Lubricate per Lubricating Chart 11.5. Rudder control 11.5.1. Check stiffness of movement 11.5.2.

  • Page 97: List Of Periodical Inspections Of Rotax 912 Ul Engine

    EV-97 EURO STAR 4.4.4 List of periodical inspections of Rotax 912 UL engine Engine: Rotax 912 S/N: Hours flown: Date of inspection: Airplane: EV-97 S/N: Registration: Event description after Every every Every every every every see. Rotax Carried Inspected out by the first 912 F 100 hr.

  • Page 98: Fluids

    EURO EV-97 STAR Fluids The fluids are: fuel, engine oil, liquid coolant and brake fluid. Filling locations can be seen in the Figure below. Fuel and Brake fluid filling locations are described in 4.6.4.3 and 4.6.3.2 respectivly. Fig. Filling locations in engine compartment 1- oil tank, 2 - liquid coolant tank...

  • Page 99: Engine Oil

    EV-97 EURO STAR 4.5.1 Engine oil 4.5.1.1 Recommended brands The recommended oil brands are listed in Service Information 18 UL 97-D/E, Jan. 1998, which is enclosed with this Manual. 4.5.1.1.1 Table of oils see Engine Operator’s manual for suitable oil grades. 4.5.1.2 Oil quantity The total oil quantity in the Rotax 912 lubricating system amounts to 0.9 USGAL (3.5 liters).

  • Page 100: Coolant

    EURO EV-97 STAR 4.5.2 Coolant 4.5.2.1 Recommended types Refer to the Rotax 912 Operator’s Manual for recommended coolant types. The “BASF Glysantin Anticorrosion“, “FRIDEX G 48“ or “Glysantin Protect Plus (produced by BASF)“ is recommended by the engine manufacturer. The engine manufacturer also recommends the use of antifreeze concentrate during cold weather operation.

  • Page 101: Brake Fluid

    EV-97 EURO STAR 4.5.3 Brake fluid 4.5.3.1 Recommended types Only brake fluid of J 1703c classification should be used for hydraulic brake system (type for middle hard or hard operation). Czech Rep. Foreign • Syntol HD 205 • ATE Blau •...

  • Page 102: Fuel

    EURO EV-97 STAR 4.5.4 Fuel 4.5.4.1 Recommended brands Refer to enclosed Service Information 18 UL 97 D/E, Issue Jan. 1998 for recommended fuel brands. 4.5.4.2 Fuel quantity The standard aircraft is equipped with a 17.2USGAL (65 liters) fuel tank. An additional fuel tank optional. Keep the maximum permitted take-off weight in mind when adding fuel to a larger tank.
  • Page 103 EV-97 EURO STAR A gasoline can and a funnel with a flexible end may be used to fill the fuel tank or a device described below may be constructed. It consists of a gasoline can and tire-pump. A gasoline can funnel is set on the gasoline can - a tire valve is brazed on the funnel and a hose on the tire-pump (compressor) is connected to the valve.

  • Page 104: Lubrication

    EURO EV-97 STAR Lubrication 4.6.1 Lubrication fundamentals There are some generally inaccessible joints and control system parts inside the wings and fuselage, which have been cleaned and lubricated during airplane assembly. Lubrication of these will be performed during a periodic inspection. There are some parts, e.g.

  • Page 105: Lubricating Points

    EV-97 EURO STAR 4.6.2.2 Lubricating points after the Every Every Unit Lubricating point Lubricant first 50 hrs. 100 hrs 25 hrs. Prop • Adjustable props acc. to Prop Manual • Engine oil change acc. to Engine Manual • carburetor control cable at inlet into the bowden (in engine compartment) •...

  • Page 106: Mechanism Adjustments

    EURO EV-97 STAR Mechanism adjustments 4.7.1 Torque moments Strengh class Metric thread 1,67 kg.m 0,17 3,45 kg.m 0,35 4,31 4,90 5,39 5,88 6,86 7,84 8,33 9,80 13,72 16,67 kg.m 0,44 0,50 0,55 0,60 0,70 0,80 0,85 1,00 1,40 1,70 5,88 7,84 8,82 9,80...

  • Page 107: Necessary Maintenance Tools

    EV-97 EURO STAR Necessary maintenance tools No special tools are needed for the maintenance. EV-97 „EUROSTAR“ model 2000 version R Tools used for automobile maintenance are suitable. If the aircraft is equipped with the wing folding mechanism, the following additional tools are supplied with that aircraft: assembly lever, rests for folded wings and others as required.

  • Page 108: Brake System Efficiency Adjustment

    EURO EV-97 STAR 4.10 Brake system efficiency adjustment 4.10.1 Brake pad replacement Brake pad replacement is only performed when a pad is worn-out. CAUTION Due to the possibility of brake fluid leaking, it is advisable not to loosen the hose cup nut during brake pad removal.

  • Page 109: Bleeding

    EV-97 EURO STAR 4.10.2 Bleeding It is important to thoroughly bleed the brake system. Otherwise the system function may be unreliable and the brakes may fail. There are two main reasons for air entering the brake system: 1. Disconnected or loose hoses 2.

  • Page 110: Control Surfaces Deflection Setting

    EURO EV-97 STAR 4.11 Control surfaces deflection setting Control surface deflections of a new aircraft are set by the manufacturer. Deflections are adjusted to values specified in the Control Surfaces Deflection Record enclosed in this Manual. A neutral position of the control surfaces and controls is used as a base for adjustment of deflections.

  • Page 111: Rudder Deflection Adjustment

    EV-97 EURO STAR 4.11.4 Rudder deflection adjustment The rudder deflections are set by the aircraft manufacturer and can not be adjusted. 4.11.5 Trim tab adjustment The following may be adjusted: a) The position of the trim tab control lever may be adjusted against a groove in the quadrant between the seats.

  • Page 112: Steerable Nosewheel Landing Gear Adjustment

    EURO EV-97 STAR 4.12 Steerable nosewheel landing gear adjustment A steerable nosewheel adjustment is necessary so the airplane tracks during straight taxiing with engine idling (to eliminate prop turning moment) with rudder pedals held in neutral position (no crosswind!). Procedure: 1.

  • Page 113: Engine Idle Adjustment

    EV-97 EURO STAR 4.13 Engine idle adjustment Because the engine idle is adjusted on a running engine, use extreme caution near the propeller. The aircraft should be tied down. Use the adjustment screw on the carburetor of the Rotax 912 engine to adjust the idle.

  • Page 114: Cleaning And Care

    EURO EV-97 STAR 4.15 Cleaning and care 4.15.1 Airplane care outlines Use mild detergents to clean the exterior surfaces. Oil spots on the surfaces (except the canopy!) may be cleaned with gasoline or strong detergents such as 409. Upholstery covers can be removed from the cockpit, brushed or washed in lukewarm water with a laundry detergent.

  • Page 115: Engine Maintenance

    EV-97 EURO STAR 4.15.5 Engine maintenance Refer to the engine manufacturer's instructions for engine maintenance. 4.15.6 Propeller maintenance Refer to the propeller manufacturer's instructions for engine maintenance. Document No.: Date of Issue: Revision: 4-29 EV2000RNOEN 01/2001...

  • Page 116: Winter Operation

    EURO EV-97 STAR 4.15.7 Winter operation 4.15.7.1 General It is considered a winter operation, if the outside temperature falls below 41 °F (+5 °C) . 4.15.7.2 Preparing the aircraft for winter operation Aircraft airframe • Lubricate the aircraft per Lubricating Chart (100 hr. Inspection) if the last inspection was not within 6 months •...
  • Page 117 EV-97 EURO STAR Pre-heating engine and oil It is permissible to start an engine without pre-heating if the outside air temperature is not below 41 °F (+5 °C). Pre-heat the engine and oil if air temperature falls below 41 °F (+5 °C). Use suitable air heater or a dryer.
  • Page 118 EURO EV-97 STAR Intentionally left blank Date of Issue: Revision: Document No.: 4-32 01/2001 EV2000RNOEN...

  • Page 119: Repairs

    EV-97 EURO STAR 5. REPAIRS Document No.: Date of Issue: Revision: EV2000RNOEN 01/2001...

  • Page 120: Repair Guidelines

    EURO EV-97 STAR Repair guidelines Dents, cracks and loose rivets are the most frequent problems encounered during the operation of an all-metal airplane. The following guedelines should be considered during repair: 1. The Strength in any cross-section of a repaired area/part should at a minimum be the same as the strength of the original undamaged area or part.

  • Page 121: Materials Used

    EV-97 EURO STAR Materials used 5.3.1 List of skin sheets Duralumin sheets plated by aluminum are used for skins. The following thickness are used: 0.016 in 0.4 mm 0.5 mm 0.020 in 0.6 mm 0.024 in Material qualities are shown in the following table : Z 424253.61 Czech Standard Al Cu Mg 1...

  • Page 122: Skin Repair

    EURO EV-97 STAR Skin repair 1. To prevent small cracks (0.2 in, max.5 mm) from spreading, drill a hole of 0.06 in (1.5 mm), diameter at the end of the crack 2. Small holes (up to ∅ 0.16 in, 4 mm) can be repaired by a "POP"rivets 3.

  • Page 123: Riveting

    EV-97 EURO STAR 5.4.1 Riveting "POP" rivets are used in most cases. Aircraft solid rivets are used only on wing spars, the wing box inside the fuselage and on some airplane parts with high loads. These parts must be repaired only by an authorized repair station.

  • Page 124: Fiberglass Parts Repairs

    EURO EV-97 STAR Fiberglass parts repairs Cracks, permanent deformations and breaks are the most prevelant type of damage. Prior to undertaking the repair, clean the area to be repaired thoroughly, with soap and water. Remove any paint by wet or dry sanding. Superficial scars, scratches, surface abrasions, or erosion can generally be repaired by applying one or more coats of epoxy resin.

  • Page 125: First Flight After A Repair

    EV-97 EURO STAR First flight after a repair CAUTION Only qualified pilots may perform the test flight. The following information is intended for the aircraft owner. A test flight is mandatory in the following cases: After repair or replacement of fixed surfaces - wing, fin, stabilizer, or control surfaces i.e. elevator, aileron or flap.
  • Page 126 EURO EV-97 STAR Intentionally left blank Date of Issue: Revision: Document No.: 01/2001 EV2000RNOEN...

  • Page 127: Appendices

    EV-97 EURO STAR 6. APPENDICES Document No.: Date of Issue: Revision: EV2000RNOEN 01/2001...

  • Page 128: List Of Appendices

    EURO EV-97 STAR List of Appendices • Leveling Record • Control Surfaces Deflection Record • Weight and Balance Record • Flight Test Record • Spare Parts Order • Airplane Failure Card • Airplane Placards • Airplane Wiring diagrams • Service Information 18 UL 97 D/E, Issue Jan. 1998 Date of Issue: Revision: Document No.:...

  • Page 129: Weight And Balance Record

    Weight and Balance Record EV-97 Model : Registration : S/N : Configuration : Weighing Point Scale Reading Tare Net Weight [lbs] or[ kg] [lbs] or [kg] [lbs] or [kg] Nosewheel Left wheel Right wheel Total Weight [lbs] or [kg] TW = permitted empty weight TW=NW =...
  • Page 131 Control Surfaces Deflection Record EV-97 Model: Registration: S/N: Specified Real deflection deflection Distance between neutralized control stick and instrument panel Distance between control stick fully pulled and Longitudinal instrument panel control 25°±1° HTU upward deflection 20°±1° HTU downward deflection Distance between neutralized control stick and fuselage side frame Distance between control stick moved fully to the left/right and fuselage side frame...
  • Page 133 Leveling Record EV-97 Model: Registration: S/N: Vertical measurement Straight measurem Differences left / right side Point Measure Points Measure Specified values Real 1- 3 1 Points Difference Tolerance Difference 3- 5 ±0.08 in 6-17 ±2 mm 8- 7 ±0.08 in 13-18 ±2 mm ±0.2 in...
  • Page 135 Flight Test Record Page: Pages: TAKE-OFF WEIGHT 992 lbs (450 kg) S/N: Registration: Model: EV-97 Engine: R 912..S/N: Hours flown: Prop.: S/N: RESULTS: (Airspeeds are IAS) Regime Test Meteorological conditions On ground pressure QNH On ground temperature QMU Wind direction/velocity Engine check Full throttle Engine max.
  • Page 137 Spare Parts Order Please, do not complete gray-shaded areas. Date: From: EVEKTOR - AEROTECHNIK 686 04 KUNOVICE CZECH REPUBLIC Tel.: +420 572 537 111 Fax.: +420 572 537 900 1.Registration......4.Type........2.S/N........5.Tot. hours flown....3.Number of Take-offs..... 6. Date of Failure detection....Damaged part ................
  • Page 139 Airplane Failure Card Dear customer, We´d like to ask you for your cooperation in obtaining information required for systematic improvement of our planes reliability. Please, send or transmit completed card to the following address: EVEKTOR AEROTECHNIK Quality Control Department 686 04 Kunovice CZECH REPUBLIC EV-97 Airplane:...

Table of Contents

Save PDF