Evektor Harmony LSA

evektor harmony lsa

https://www.evektor.cz/en/harmony-lsa 

Hermony LSA on FAA hyväksytty S-LSA lentokone Evektorilta. Kone on erinomainen harraste ja koulukone. Uudistettu siivenkärki, suurennettu peräsin ja ohjaamotila muiden innovaatioden kanssa tuovat lisämukavuuksia ja ominaisuuksia. Kone tunnetaan kestävänä ja ajattomana ja sopii erinomaisesti Suomeen kun uudet MTOM 600kg määräyset astivat voimaan mahdollisesti jo tänä vuonna, mutta viimeistään 2019 keväällä.

 

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