Endast för information och utbildning – ej för operativt bruk !

1.   GENERAL

1.1   Introduction

1.2   Certification basis

1.3   Warnings, cautions and notes

1.4   Descriptive data

1.4.1   Aircraft description

1.4.2   Technical data

1.5   Three-view drawing

 

---

1.1  Introduction

The aeroplane Flight Manual has been prepared to provide pilots and instructors with information for the safe and efficient operation of the EV-97 „EUROSTAR“ model 2003 ultra-light aeroplane.

It also contains supplemental data supplied by the aeroplane manufacturer.

1.2  Certification basis

This aircraft type has been approved by the responsible airworthiness authorities listed below :

                                CZECH REPUBLIC

                                Type Certificate No.:   ULL – 03/98/”b” 00

Date of approval:   13.10.2000

Approved by:   Light Aircraft Association
 of Czech Republic

                               Certificate of Airworthiness:   “P”

1.3  Warnings, cautions and notes

The following definitions apply to warnings, cautions and notes in the 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 corresponding procedure leads to a minor or                                   possible long term degradation of the flight safety.

                                 NOTE

Draws attention to any special item not directly related to safety, but which is important or unusual.

1.4  Descriptive data

1.4.1  Aircraft description

EV-97 „EUROSTAR“ model 2003 is an aircraft intended especially for recreational and touring flying, with a limitation to non-aerobatic operation.

The EV-97 „EUROSTAR“ model 2003 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 with a controllable nose wheel.

The powerplant is composed of the ROTAX 912S (100 hp), four cylinder, four stroke engine and the two blade V 230C , fixed wooden propeller (standard powerplant).

Alternatively it is possible to upgrade to other propellers according to consumer 's request.

1.4.2  Technical data

Wing

span   ...................................... 8.1   m    26.57   ft

area   ...................................... 9.84   m 2    105.92   ft 2

MAC   ..................................... 1.25   m    4.10   ft

loading   .................................. 45.7   kg/m 2    9.37   lb/ft 2

Aileron

area   ...................................... 0.21   m 2    2.26   ft 2

Flap

area   ...................................... 0.52   m 2    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   m 2    20.99   ft 2

elevator area   ........................... 0.8   m 2    8.60   ft 2

Vertical tail unit

height   .................................... 1.24   m    4.07   ft

area   ....................................... 1.0   m 2    10.76   ft 2

rudder area   ............................. 0.4   m 2    4.30   ft 2

Landing gear

wheel track   ............................. 1.6   m    5.25   ft

wheel base   ............................. 1.35   m    4.42   ft

main wheel diameter   ................ 350   ..... mm    14   in

nose wheel diameter   ................ 350   ..... mm    14   in

1.5  Three-view drawing