Evektor Eurostar ES600

evektor harmony lsa

Tiedot päivitetään 2021 alussa.  Samalla ilmoitetaan ketkä ostivat Joulukuussa 2020 ensimmäisen.

 

Moottorivaihtoehtoina ovat tunnetut ja luotetut

  • Rotax 912 iS/S2 taloudelliset ruiskumoottorit,
  • Rotax 924 Turbo moottorit
  • Rotax 912 ULS keveät luotettavat perusmoottorit

Specification

Dimensions

Length

20 ft

6.11 m

Height

8ft 2 in

2.48 m

Wing span

30 ft 4 in

9.25 m

Cabin width

46.5 in

1.18 m

Baggage compartment volume

10.1 cu.ft

285 l

Wight & Quantities

Useful load

634 lb

289 kg

Max. take-off weight

1 320 lb

600 kg

Empty weight (standard a/c)

686 lb

311 kg

Max. baggage

55 lb

25 kg

Design load factors

+6 / -3g

Operation load factors

+4 / -2g

Wing tank capacity

31.7 U.S. gal

120 l

Performance

Engine

Rotax 912ULS (100 hp)

Rotax 914 UL (115 hp)

Never exceed speed

146 kts

270 km/h

146 kts

270 km/h

Max. level speed

120 kts

222 km/h

130 kts

240 km/h

Cruising speed (75% power)

97 kts

171 km/h

126 kts

233 km/h

Stall speed VS1

45 kts

83 km/h

45 kts

83 km/h

Stall speed VS0 (full flaps)

40 kts

74 km/h

40 kts

74 km/h

Rate of climb

1 020 fpm

5.2 m/s

1 300 fpm

6.6 m/s

Service ceiling

15 500 ft

4 720 m

27 000 ft

8 230 m

Take-off run (concrete RWY)

620 ft

190 m

560 ft

170 m

Landing run (concrete RWY)

590 ft

180 m

590 ft

180 m

Average fuel consumption

4.0 U.S.gal

15 l/h

5.3 U.S.gal

20 l/h

Range

700 nm

1 300 km

600 nm

1 120 km

             

–– Specification

Dimensions

Length

20 ft

6.11 m

Height

8ft 2 in

2.48 m

Wing span

30 ft 4 in

9.25 m

Cabin width

46.5 in

1.18 m

Baggage compartment volume

10.1 cu.ft

285 l

Wight & Quantities

Useful load

634 lb

289 kg

Max. take-off weight

1 320 lb

600 kg

Empty weight (standard a/c)

686 lb

311 kg

Max. baggage

55 lb

25 kg

Design load factors

+6 / -3g

Operation load factors

+4 / -2g

Wing tank capacity

31.7 U.S. gal

120 l

Performance

Engine

Rotax 912ULS (100 hp)

Rotax 914 UL (115 hp)

Never exceed speed

146 kts

270 km/h

146 kts

270 km/h

Max. level speed

120 kts

222 km/h

130 kts

240 km/h

Cruising speed (75% power)

97 kts

171 km/h

126 kts

233 km/h

Stall speed VS1

45 kts

83 km/h

45 kts

83 km/h

Stall speed VS0 (full flaps)

40 kts

74 km/h

40 kts

74 km/h

Rate of climb

1 020 fpm

5.2 m/s

1 300 fpm

6.6 m/s

Service ceiling

15 500 ft

4 720 m

27 000 ft

8 230 m

Take-off run (concrete RWY)

620 ft

190 m

560 ft

170 m

Landing run (concrete RWY)

590 ft

180 m

590 ft

180 m

Average fuel consumption

4.0 U.S.gal

15 l/h

5.3 U.S.gal

20 l/h

Range

700 nm

1 300 km

600 nm

1 120 km

             

–––– Specification

Dimensions

Length

20 ft

6.11 m

Height

8ft 2 in

2.48 m

Wing span

30 ft 4 in

9.25 m

Cabin width

46.5 in

1.18 m

Baggage compartment volume

10.1 cu.ft

285 l

Wight & Quantities

Useful load

634 lb

289 kg

Max. take-off weight

1 320 lb

600 kg

Empty weight (standard a/c)

686 lb

311 kg

Max. baggage

55 lb

25 kg

Design load factors

+6 / -3g

Operation load factors

+4 / -2g

Wing tank capacity

31.7 U.S. gal

120 l

Performance

Engine

Rotax 912ULS (100 hp)

Rotax 914 UL (115 hp)

Never exceed speed

146 kts

270 km/h

146 kts

270 km/h

Max. level speed

120 kts

222 km/h

130 kts

240 km/h

Cruising speed (75% power)

97 kts

171 km/h

126 kts

233 km/h

Stall speed VS1

45 kts

83 km/h

45 kts

83 km/h

Stall speed VS0 (full flaps)

40 kts

74 km/h

40 kts

74 km/h

Rate of climb

1 020 fpm

5.2 m/s

1 300 fpm

6.6 m/s

Service ceiling

15 500 ft

4 720 m

27 000 ft

8 230 m

Take-off run (concrete RWY)

620 ft

190 m

560 ft

170 m

Landing run (concrete RWY)

590 ft

180 m

590 ft

180 m

Average fuel consumption

4.0 U.S.gal

15 l/h

5.3 U.S.gal

20 l/h

             

Powerplant

Engine

Bombardier Rotax 912ULS

No. of cylindres

4

Maximum power

100 hp

TBO

2000 hours

Fuel

Unleaded automotive gasoline or AVGAS 100LL

Propeller

Fixed or on ground and in-flight adjustable