CIVIL AVIATION AUTHORITY SAFETY AND AIRSPACE REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM-67 ISSUE: 5

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1 TYPE: EV-97 teameurostar UK (1) MANUFACTURER: Light Sport Aviation Ltd, Wycombe Air Park, Hangar 1, Booker, Marlow, Buckinghamshire, SL7 3DP (2) UK IMPORTER: N/A (3) CERTIFICATION: BCAR Section S Issue 2 dated August 1999 (4) DEFINITION OF BASIC STANDARD: Build Standard Sheet included in Procedure P.01, Control and Storage of Drawings (5) COMPLIANCE WITH THE MICROLIGHT DEFINITION (a) MTOW 450 kg (b) No. Seats 2 (c) Maximum Wing Loading (d) Vso (e) Permitted range of pilot weights (f) Typical Empty Weight (ZFW) (g) ZFW kg crew + 1 hr fuel (14 litres / 10 kg) (h) ZFW + 86 kg pilot + full fuel (62 litres / 44.6 kg) (i) Max ZFW at initial permit issue 45.7 kg/m² 40 mph CAS kg total 265 kg 447 kg 396 kg 268 kg TADS BM-67 Issue 5 1 of 11

2 (6) POWER PLANTS Designation EV-97 teameurostar UK Engine Type Rotax 912 UL Rotax 912 UL Rotax 912 UL Reduction Gear 2.27:1 2.27:1 2.27:1 Exhaust System Evektor Evektor Evektor Intake System Rotax (K & N) Filter Rotax (K & N) Filter Rotax (K & N) Filter Propeller Type Propeller Dia x Pitch VZLU V230C 1625 mm dia. radius GT-2/166/145 (Also identified as GT- 2/166/VSR-FW101SRTC) 1660 mm x 1450 mm Kievprop 273/ mm dia 350 mm radius Noise Type Cert No. 175M 175M 175M AAN approving configuration (7) MANDATORY LIMITATIONS: (a) Max Take-Off Weight (b) CG Limits (c) CG datum (d) Cockpit Loadings (e) Never Exceed Speed (f) Manoeuvring Speed Aft limit FWD Limit Min Max 450 kg 425 mm aft of datum 250 mm aft of datum Wing Leading Edge Total 55 kg 172 kg 146 mph IAS 100 mph IAS (g) Permitted Manoeuvres Maximum bank angle 60º Non Aerobatic Normal acceleration limits, +4g / -2g (h) Fuel Contents (Max Usable) 62 litres TADS BM-67 Issue 5 2 of 11

3 (i) Power Plant See Table Engine Max RPM Max Continuous RPM MAX CHT MAX EGT Fuel Spec Engine Oil Spec Gearbox oil spec Fuel/Oil Mix Coolant Temperature Oil Pressure Rotax 912 UL 5800 for 5 minutes 5200 with VZLU or GT propeller 4800 with Kievprop propeller 150ºC (120ºC if SB/EUR/006 has been implemented) N/A 90 RON minimum unleaded to EN228 AVGAS UL 91 AVGAS 100LL (not recommended for long term use) API Class SF or SG, motor cycle oil with gear additives N/A N/A N/A 1.5 to 7 bar Oil Temperature 50ºC to 140ºC Fuel Pressure 0.15 to 0.4 bar (8) INSTRUMENTS REQUIRED: ASI Altimeter RPM CHT Compass Oil temperature 0 to 150 mph Required rpm Fuel Pressure Oil pressure Slip ball 150ºC Required 150ºC 0 1 bar 0 10 bar Required (9) CONTROL DEFLECTIONS: Elevator UP: 25º ± 1º Elevator trim tab UP: 5º ± 2º Elevator DOWN: 20º ± 1º Elevator trim tab DOWN: 25º ± 5º Ailerons UP: 20º ± 1º Rudder LEFT: 30º ± 2º Ailerons DOWN: 15º ± 1º Rudder RIGHT: 30º ± 2º TADS BM-67 Issue 5 3 of 11

4 (10) PILOT'S NOTES, MAINTENANCE MANUALS REFERENCES: 10.1 Manuals approved for use with this aircraft. (a) (b) Pilot s Operating Handbook POH/EUR/01 (including Supplement 01 when Kievprop propeller is fitted.) Maintenance Manual GEN/EUR/ The following placards are to be fitted:- (a) Flight Limitations Placard (to be visible to pilot) See Annex D. (b) Engine Limitations Placard (to be located near to engine instruments) See Annex D. (c) Fuel Limitations Placards See Annex D. (d) Switches See Annex D. TADS BM-67 Issue 5 4 of 11

5 (11) MANDATORY MODIFICATIONS / SERVICE BULLETINS / AIRWORTHINESS DIRECTIVES ETC: See Annex A for required modifications. Service Bulletin SB/EUR/005 Service Bulletin SB/EUR/001 Service Bulletin SB/EUR/002 Service Bulletin SB/EUR/003 Service Bulletin SB/EUR/004 Service Bulletin SB/EUR/006 Service Bulletin SB/EUR/007 Service Bulletin SB/EUR/008 Service Bulletin SB/EUR/009 Checking the Strength of the Lower Wing Spar Caps is classified as Essential, CAA MPD refers Coolant Overflow Bottle is classified as Recommended Trim Cable Clevis Pin Retainer is classified as Recommended Possible corrosion of Pitch Trim Cables is classified as Recommended Inspection and Rectification of Rudder Top Bearing is classified as Recommended Change of Cylinder Head Temperature Limit is classified as Recommended Rudder Stop Swages is classified as Recommended Aileron Rose Joint is classified as Recommended Inspection of Undercarriage Support for Cracks is classified as Recommended Service Bulletin SB/EUR/010 Under-Wing Fairings is classified as Essential, CAA MPD refers (12) MINIMUM PERFORMANCE AT MAX TAKE-OFF WEIGHT Rate of Climb: Stall or Minimum Flying Speed: 800 fpm at 70 mph IAS. 36 mph IAS at MTOW / idle / full flap. TADS BM-67 Issue 5 5 of 11

6 Issue History Issue No. Reason and signatory 1 25 July 2003 Initial Issue 2 9 March 2005 Kievprop propeller added as an alternative, see paras 6 & 10.1 and Annex D (b). Max Continuous RPM values added to para 7 (I). Service Bulletin SB/EUR/001 added to para March 2005 Para 6, pitch angle of Kievprop corrected to 28º. 4 7 April 2011 Para 7 (I), alternative max CHT added. Para 11, Service Bulletins SB/EUR/002, 003, 004 and 006 added. Annex D (b), alternative max CHT added May 2014 Company name and address changed. Items 1 to 8 added to Annex B - Approved Optional Modifications. AVGAS UL 91 Fuel Specification added to paragraph 7 (I) and Annex D (c). Service Bulletins SB/EUR/007, 008, 009 and 010 added to paragraph 11. Illustration of Aircraft Photograph, changed. N J Davis TADS BM-67 Issue 5 6 of 11

7 Illustration of Aircraft - 3 View 3.42 ft 1.04 m ft 5.98 m 7.7 ft 2.34 m 4.42 ft 5.25 ft 1.35 m 1.6 m ft 8.1 m 8.2 ft 2.5 m 7.38 ft 2.25 m 3.1 ft 0.94 m TADS BM-67 Issue 5 7 of 11

8 Illustration of Aircraft Photograph TADS BM-67 Issue 5 8 of 11

9 None ANNEX A MANDATORY MODIFICATIONS ANNEX B - APPROVED OPTIONAL MODIFICATIONS The installation of all optional modifications is to be inspected by an inspector from an Organisation approved by the CAA for the purpose and an entry made in the appropriate logbook(s). Note that other approved modifications may exist which are not listed here. 1. VSI Initial Build Standard Option 2. Lynx Intercom System Initial Build Standard option 3. Hourmeter Modification 002 (Cosmik Aviation Ltd) 4. Cabin Heater Modification 003 (Cosmik Aviation Ltd) 5. Wheel Spats Modification 010 (Cosmik Aviation Ltd) 6. Panel Mount Radio & Intercom Modification 017 (Cosmik Aviation Ltd) 7. Transponder Modification 018 (Cosmik Aviation Ltd) 8. Throttle Relief Spring Modification 025 (Cosmik Aviation Ltd) ANNEX C - WEIGHING INFORMATION 1. CG Datum: Wing Leading Edge 2. Weighing attitude: Pilot s Canopy Edge Horizontal 3. Mainwheel moment arm: See Maintenance Manual for individual aircraft 4. Nosewheel moment arm: See Maintenance Manual for individual aircraft 5. Fuel moment arm: 920 mm aft of datum 6. Crew moment arm: 500 mm aft of datum 7. Baggage moment arm 1270 mm aft of datum 8. Crew weights: Minimum 55 kg / maximum 172 kg 9. Aft CG Limit: 425 mm aft of datum 10. Fwd CG Limit: 250 mm aft of datum TADS BM-67 Issue 5 9 of 11

10 ANNEX D EXAMPLE PLACARDS (a) Flight Limitations Placards (to be visible to pilot) AIRSPEEDS (IAS) V NE (Never exceed speed) V A (Maximum manoeuvring speed) V FE (Flaps extended max. speed) V S (Stall speed, flaps extended) 146 mph 100 mph 77 mph 36 mph Flight limited to daytime VFR non-icing conditions. Aerobatics and intentional spinning are prohibited. This microlight aeroplane has not been approved to an internationally recognised airworthiness standard. (b) Engine Limitations Placard (to be located near to engine instruments) ENGINE LIMITATIONS Maximum take-off (max. 5 minutes) 5800 rpm Max. continuous 4800 or 5200 rpm* Idle approx rpm Max. CHT 150ºC** Max. oil temp. 140ºC Min. oil temp. 50ºC Min. oil pressure 1.5 bar Max. oil pressure 7.0 bar Minimum fuel pressure 0.15 bar Maximum fuel pressure 0.4 bar * Depending on propeller fitted. ** 120ºC if SB/EUR/006 has been implemented. TADS BM-67 Issue 5 10 of 11

11 (c) Fuel Limitations Placard To be located in the cockpit FUEL and LOAD LIMITS Capacity 65 litres Unusable fuel 2.9 litres Maximum take-off weight Max. empty weight Actual empty weight Max. baggage weight Minimum Cockpit Load Cockpit Load incl. Baggage (kg) 450 kg 268 kg kg* 15 kg 55 kg Max. Fuel Load (litres)** 172 (maximum) or less Full fuel * This must match the most recent W&CG report for the aircraft. ** Typical values shown. Actual values to be entered following the most recent W&CG report for the aircraft. To be located adjacent to the fuel filler (d) Switches 90 RON minimum MOGAS unleaded to EN 228 or AVGAS UL 91 or AVGAS 100LL Prolonged use of 100LL should be avoided. All switches are to be marked with function and sense (up=on, down=off). TADS BM-67 Issue 5 11 of 11

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14 Civil Aviation Authority MANDATORY PERMIT DIRECTIVE Number: Issue date: 30 January 2014 In accordance with 22(1) of Air Navigation Order 2009 as amended the following action required by this Mandatory Permit Directive (MPD) is mandatory for applicable aircraft registered in the United Kingdom operating on a UK CAA Permit to Fly. Type Approval Holder s Name: Light Sport Aviation Ltd Type/Model Designation(s): Aerotechnik EV-97 Eurostar Aerotechnik EV-97A Eurostar Aerotechnik EV-97 Eurostar SL EV-97 teameurostar UK Title: Wing / Fuselage Fairings Inspection for Rivet Damage Manufacturer: Applicability: Reason: Light Sport Aviation Ltd Aerotechnik EV-97 Eurostar Aerotechnik EV-97A Eurostar Aerotechnik EV-97 Eurostar SL EV-97 teameurostar UK EV-97 Eurostar variants are fitted with aluminium alloy fairings between the under surface of the wing and the lower fuselage. They are attached to the wings along one side with the other, unattached, side bearing on the fuselage. Effective Date: 3 February 2014 During an aircraft inspection it was noticed that the unattached sides of the fairings were rubbing against some rivet heads and causing damage to the rivet heads. The affected rivets attach the lower fuselage longerons and failure of one or more rivets could compromise the structural integrity of the fuselage. Compliance/Action: Compliance is required as follows, unless previously accomplished: 1. Within 10 flying hours from the effective date of this MPD, carry out an inspection in accordance with Light Sport Aviation Ltd Service Bulletin SB/EUR/010 and rectify any damage found, in accordance with the Service Bulletin, within a further 10 flying hours. 2. Repeat the inspection and rectification, if necessary, in paragraph 1 at intervals not exceeding 12 months. Mandatory Permit Directive Page 1 of 2

15 Civil Aviation Authority Mandatory Permit Directive SARG Airworthiness ENSURE COMPLIANCE WITH THIS MPD IS RECORDED IN THE AIRCRAFT LOGBOOK Reference Publications: Light Sport Aviation Ltd Service Bulletin SB/EUR/010, Issue 1 dated 14 November Remarks: 1. Based on the required actions and compliance time, the CAA decided to issue this MPD with a request for comments, postponing the public consultation process until after publication. 2. Enquiries regarding this Mandatory Permit Directive should be referred to: Aircraft Certification - Airworthiness, Safety and Airspace Regulation Group, Civil Aviation Authority, Aviation House, Gatwick Airport South, West Sussex RH6 0YR. Tel: +44 (0) Fax: +44 (0) nigel.davis@caa.co.uk 3. Enquiries regarding the Service Bulletin should be referred to: Light Sport Aviation Ltd, Wycombe Air Park, Hangar 1, Booker, Marlow, Bucks, SL7 3DP. Tel: +44 (0) lsa@live.co.uk. Copies of the SB may be downloaded from: Mandatory Permit Directive Page 2 of 2

16 Civil Aviation Authority MANDATORY PERMIT DIRECTIVE Number: Issue date: 23 June 2015 In accordance with Article 22(1) of Air Navigation Order 2009, as amended, the following action required by this Mandatory Permit Directive (MPD) is mandatory for applicable aircraft registered in the United Kingdom operating on a UK CAA Permit to Fly. Type Approval Holder s Name: Light Sport Aviation Ltd Type/Model Designation(s): Aerotechnik EV-97 and 97A Eurostar Aerotechnik EV-97 Eurostar SL EV-97 teameurostar UK EV-97 Eurostar SL Microlight Title: Manufacturer: Applicability: Reason: Wing Flaps Correct Engagement of the Actuator Pins - Inspection Light Sport Aviation Ltd Aerotechnik EV-97 Eurostar Aerotechnik EV-97A Eurostar Aerotechnik EV-97 Eurostar SL EV-97 teameurostar UK EV-97 Eurostar SL Microlight An accident to a Eurostar occurred when one flap retracted during the landing approach which led to an uncontrollable roll. The cause was a wing flap actuator pin which was not properly engaged in the flap and which disengaged from the flap when the flaps were extended. Effective Date: 29 June 2015 Insufficient engagement of the wing flap actuator pins into the guides in the flap root ribs may cause wear of the guides. In extreme cases the pin or guide may fail causing a loss of flap controllability. Compliance/Action Compliance is required as follows, unless previously accomplished: 1. Within 25 flying hours from the effective date of this MPD, or at the next annual inspection, whichever comes first, carry out an inspection in accordance with Light Sport Aviation Ltd Service Bulletin SB/EUR/ If the inspection reveals the exposed length of the pin to be between 17 and 20 mm, before further flight, adjust the pin in accordance with the Service Bulletin. 3. If the inspection reveals the exposed length of the pin to be more than 20 mm, before further flight, contact Light Sport Aviation for a repair scheme and implement it. Mandatory Permit Directive Page 1 of 2

17 Civil Aviation Authority Mandatory Permit Directive SARG Airworthiness ENSURE COMPLIANCE WITH THIS MPD IS RECORDED IN THE AIRCRAFT LOGBOOK Reference Publications: Light Sport Aviation Ltd Service Bulletin SB/EUR/016, Issue 1, dated 7 May Remarks: 1. This MPD was posted on 5 June 2015 as Proposed MPD for consultation until 19 June No comments were received on the PMPD. 3. Enquiries regarding this Mandatory Permit Directive should be referred to: Airworthiness, Civil Aviation Authority, Safety and Airspace Regulation Group, Aviation House, Gatwick Airport South, West Sussex RH6 0YR. Tel: +44 (0) nigel.davis@caa.co.uk. Mandatory Permit Directive Page 2 of 2

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