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CIVIL AVIATION AUTHORITY – SAFETY AND AIRSPACE REGULATION GROUP

MICROLIGHT TYPE APPROVAL DATA SHEET (TADS)

NO: BM-67 ISSUE: 5

TADS BM-67 Issue 5 1 of 11

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 45.7 kg/m²

(d) Vso 40 mph CAS

(e) Permitted range of pilot weights 55 – 172 kg total

(f) Typical Empty Weight (ZFW) 265 kg

(g) ZFW + 172 kg crew + 1 hr fuel (14 litres / 10 kg) 447 kg

(h) ZFW + 86 kg pilot + full fuel (62 litres / 44.6 kg) 396 kg

(i) Max ZFW at initial permit issue 268 kg



NO: BM-67 ISSUE: 5


(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 VZLU V230C

GT-2/166/145 (Also identified as GT-

2/166/VSR-FW101SRTC) Kievprop 273/1700

Propeller Dia x Pitch

1625 mm dia. 18.5º @75% radius 1660 mm x 1450 mm 1702 mm dia

28º @ 350 mm radius

Noise Type Cert No. 175M 175M 175M

AAN approving configuration 28662 28662 29076

(7) MANDATORY LIMITATIONS:

(a) Max Take-Off Weight 450 kg

(b) CG Limits Aft limit FWD Limit

425 mm aft of datum 250 mm aft of datum

(c) CG datum Wing Leading Edge

(d) Cockpit Loadings Min Max

Total 55 kg 172 kg

(e) Never Exceed Speed 146 mph IAS

(f) Manoeuvring Speed 100 mph IAS

(g) Permitted Manoeuvres Maximum bank angle 60º Non Aerobatic Normal acceleration limits, +4g / -2g

(h) Fuel Contents (Max Usable) 62 litres



NO: BM-67 ISSUE: 5


(i) Power Plant See Table

Engine Rotax 912 UL

Max RPM 5800 for 5 minutes

Max Continuous RPM 5200 with VZLU or GT propeller 4800 with Kievprop propeller

MAX CHT 150ºC (120ºC if SB/EUR/006 has been implemented)

MAX EGT N/A

Fuel Spec 90 RON minimum unleaded to EN228 AVGAS UL 91

AVGAS 100LL (not recommended for long term use)

Engine Oil Spec API Class SF or SG, motor cycle oil with gear additives

Gearbox oil spec N/A

Fuel/Oil Mix N/A

Coolant Temperature N/A

Oil Pressure 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

Fuel Pressure

Oil pressure

Slip ball

0 to 150 mph

Required 0-7000 rpm

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



NO: BM-67 ISSUE: 5


(10) PILOT'S NOTES, MAINTENANCE MANUALS REFERENCES:

10.1 Manuals approved for use with this aircraft.

(a) Pilot’s Operating Handbook POH/EUR/01 (including Supplement 01 when Kievprop propeller is fitted.)

(b) Maintenance Manual GEN/EUR/02 10.2 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.



NO: BM-67 ISSUE: 5


(11) MANDATORY MODIFICATIONS / SERVICE BULLETINS / AIRWORTHINESS DIRECTIVES ETC: See Annex A for required modifications.

Service Bulletin SB/EUR/005 Checking the Strength of the Lower Wing Spar Caps is classified as Essential, CAA MPD 2010-003 refers

Service Bulletin SB/EUR/001 Coolant Overflow Bottle is classified as Recommended

Service Bulletin SB/EUR/002 Trim Cable Clevis Pin Retainer is classified as Recommended

Service Bulletin SB/EUR/003 Possible corrosion of Pitch Trim Cables is classified as Recommended

Service Bulletin SB/EUR/004 Inspection and Rectification of Rudder Top Bearing is classified as Recommended

Service Bulletin SB/EUR/006 Change of Cylinder Head Temperature Limit is classified as Recommended

Service Bulletin SB/EUR/007 Rudder Stop Swages is classified as Recommended

Service Bulletin SB/EUR/008 Aileron Rose Joint is classified as Recommended

Service Bulletin SB/EUR/009 Inspection of Undercarriage Support for Cracks is classified as Recommended

Service Bulletin SB/EUR/010 Under-Wing Fairings is classified as Essential, CAA MPD 2014-002 refers

(12) MINIMUM PERFORMANCE AT MAX TAKE-OFF WEIGHT

Rate of Climb: 800 fpm at 70 mph IAS. Stall or Minimum Flying Speed: 36 mph IAS at MTOW / idle / full flap.



NO: BM-67 ISSUE: 5


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 11.

3 11 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.

5

13 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



NO: BM-67 ISSUE: 5


Illustration of Aircraft - 3 View

8.1 m26.57 ft

2.5 m8.2 ft

2.34 m7.7 ft

19.6

2 ft

5.98

m

2.25 m7.38 ft

0.94 m3.1 ft

4.42

ft1.

35 m

1.6

m5.

25 ft

3.42

ft1.

04 m



NO: BM-67 ISSUE: 5


Illustration of Aircraft – Photograph



NO: BM-67 ISSUE: 5


ANNEX A – MANDATORY MODIFICATIONS

None

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



NO: BM-67 ISSUE: 5


ANNEX D

EXAMPLE PLACARDS (a) Flight Limitations Placards (to be visible to pilot)

AIRSPEEDS (IAS) VNE (Never exceed speed) 146 mph VA (Maximum manoeuvring speed) 100 mph VFE (Flaps extended max. speed) 77 mph VS (Stall speed, flaps extended) 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. 1400 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.



NO: BM-67 ISSUE: 5


(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 450 kg Max. empty weight 268 kg Actual empty weight ___kg* Max. baggage weight 15 kg Minimum Cockpit Load 55 kg

Cockpit Load incl. Baggage (kg) Max. Fuel Load (litres)** 172 (maximum) 14

160 31 150 44 140 58

135 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

90 RON minimum MOGAS unleaded to EN 228 or AVGAS UL 91 or AVGAS 100LL

Prolonged use of 100LL should be avoided. (d) Switches All switches are to be marked with function and sense (up=on, down=off).

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Mandatory Permit Directive 2014-002 Page 1 of 2

Civil Aviation Authority

MANDATORY PERMIT DIRECTIVE Number: 2014-002 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: Light Sport Aviation Ltd

Applicability: Aerotechnik EV-97 Eurostar Aerotechnik EV-97A Eurostar Aerotechnik EV-97 Eurostar SL EV-97 teamEurostar UK

Reason: 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. 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.

Effective Date: 3 February 2014

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.

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 2014.

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)1293 573309. Fax: +44 (0)1293 573976. E-mail: [email protected] 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) 1494 524020. E-mail: [email protected]. Copies of the SB may be downloaded from: http://www.lightsportaviation.org.uk/



MANDATORY PERMIT DIRECTIVE Number: 2015-001 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: Wing Flaps –Correct Engagement of the Actuator Pins - Inspection

Manufacturer: Light Sport Aviation Ltd

Applicability: Aerotechnik EV-97 Eurostar Aerotechnik EV-97A Eurostar Aerotechnik EV-97 Eurostar SL EV-97 teamEurostar UK EV-97 Eurostar SL Microlight

Reason: 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. 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.

Effective Date: 29 June 2015

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/016.

2. 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.

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 2015.

Remarks: 1. This MPD was posted on 5 June 2015 as Proposed MPD 15-01 for consultation until 19 June 2015.

2. 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) 1293 573309. E-mail: [email protected].



MANDATORY PERMIT DIRECTIVE Number: 2018-006 Issue date: 8 June 2018

In accordance with 41(1) of Air Navigation Order 2016 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):

EV-97 teamEurostar UK EV-97 Eurostar SL Microlight

Title: Amendment of Inspection Requirements and Replacement of Critical Structural Items

Manufacturer: Evektor Aerotecnik

Applicability: EV-97 teamEurostar UK and EV-97 Eurostar SL Microlight

Reason: A metal-fatigue analysis performed by Evektor has identified a potentially unsafe condition relating to fatigue cracks in the lower spar cap of the main spar, and the main-spar carry-through structure in the fuselage. Additionally, service experience has identified certain items that deteriorate in service and yet were not addressed by the inspection schedules in the maintenance manuals (prior to issue 6). Therefore, the manufacturer has amended the maintenance manuals to include:

• A detailed, recurring, 1000-hour inspection, starting at 2000 hours. • Replacement of critical wing and fuselage structural components

at 4000 hours (450kg EV-97 teamEurostar UK) or 3000 hours (472.5kg EV-97 Eurostar SL Microlight).

Due to the fleet size and with aircraft either exceeding or rapidly approaching the specified new intervals, this MPD has been raised to increase awareness and mandate these inspections/replacements.

Effective Date: 8 June 2018

Civil Aviation Authority Mandatory Permit Directive SARG


Compliance/Action: FOR ALL APPLICABLE TYPES From the effective date of this MPD: -

1. Determine that the latest versions of the applicable maintenance manual are in use (refer to “Reference Publications” section below).

Within 300 flight hours or six months from the effective date of this MPD (whichever occurs first): -

1. For all applicable types that have accumulated 2000 airframe

hours or above, conduct the 1000-hour inspection as specified within the applicable aircraft maintenance manual.

2. For all applicable types whose wing main spars and/or fuselage main-spar carry-through structure have accumulated 4000 airframe hours or above (450kg EV-97 teamEurostar UK) or 3000 hours or above (472.5kg EV-97 Eurostar SL Microlight) conduct the replacement of critical items* as specified within the applicable aircraft maintenance manual.

3. Thereafter carry out the detailed inspection at 1000 hour intervals and the replacement of the critical wing and fuselage structural components at 4000 hours (450kg EV-97 teamEurostar UK) or 3000 hours (472.5kg EV-97 Eurostar SL Microlight) intervals as detailed in the aircraft maintenance manual.

4. If any cracks are found during the inspections noted above, before further flight consult Light Sport Aviation (LSA) for further instructions regarding repair/replacement of the affected structure.

* Replacement of critical wing and fuselage structural components can only be conducted by the manufacturer.

Note: Amateur-built examples of the Eurostar are not affected by this MPD.

Civil Aviation Authority Mandatory Permit Directive SARG


ENSURE COMPLIANCE WITH THIS MPD IS RECORDED IN THE ARICRAFT LOGBOOK

Reference Publications:

EV-97 teamEurostar UK (MAUW 450kg RTF) – Maintenance Manuel, ref. GEN/EUR/02, issue 7 (or later approved issue). EV-97 Eurostar SL Microlight (MTOW 472.5kg RTF) Maintenance Manual, ref. GEN/EUR/04, issue 7 (or later approved issue).

Remarks: 1. During development of this MPD, BMAA and LAA were consulted.

2. Enquiries regarding this Mandatory Permit Directive should be referred to: GA Unit, Safety Airspace Regulation Group, Civil Aviation Authority, Aviation House, Gatwick Airport South, West Sussex RH6 0YR.

Tel: +44 (0)1293 573988 E-mail: [email protected]

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