https://www.evektor.cz/en/sportstar-rtc
SportStar RTC on Erinomaisilla lento-ominaisuuksilla varustettu nykyaikainen kokometallinen kaksipaikkainen lentokone jonka käyttökustannukset ovat jopa puolet edullisemmat kuin perinteisten lentokoneiden kkäyttökustannuksista. Tämä kone on vasteenotettava vaihtoehto esimerkiksi lentokouluille lupakirjoihin ja niiden ylläpitoon.
Esimerkki lasiohjaamo paneeli
- 10.6" PFD - Primary Näyttö (GDU 460)
- 10.6" MFD – Secondary näyttö (GDU 460)
- 2 ADAHRS – Erilliset gyroyksiköt (GSU 25)
- Avainmagnetokytkin (GMU 22)
- EMS (GEA 24)
- OAT ulkolämpötila sensori (GTP 59)
- GPS antennit, Synteettinen näyttö, Backup patteri
- Back-up mitterit Ilmanopeus + Korkeus (dia 2 ¼")
- COMM Garmin GTR225A + Transponderi GTX328 (mode S) + ACK A-30
- Kompassi SIRS
|
Dimensions |
|
|
Length |
19.62 ft (5.98 m) |
|
Height |
8.14 ft (2.48 m) |
|
Wing span |
28.40 ft (8.65 m) |
|
Cabin width |
3.87 ft (1.18 m) |
|
Baggage compartment volume |
10.06 cu.ft (285 l) |
|
Weights & Quantities |
|
|
Empty weight |
756 lb (343 kg) |
|
Maximum take-off weight |
1 320 lb (600 kg) |
|
Maximum baggage |
55 lb (25 kg) |
|
Design load factors |
+6 / -3g |
|
Operation load factors |
+4 / -2g |
|
Performance |
|
|
Engine |
Rotax 912ULS |
|
Never exceed speed |
146 kts (270 km/h) |
|
Maximum level speed |
115 kts (213 km/h) |
|
Cruising speed (75% of MCP) |
92 kts (171 km/h) |
|
Stalling speed |
42 kts (78 km/h) |
|
Rate of climb |
876 fpm (4.5 m/s) |
|
Service ceiling |
15 500 ft (4720 m) |
|
Take-off run (concrete RWY) |
420 ft (128 m) |
|
Take-off distance over 50 ft obstacle (concrete RWY) |
1 200 ft (365 m) |
|
Landing run (concrete RWY) |
555 ft (169 m) |
|
Range |
700 nm (1 300 km) |
Specification
|
Dimensions |
|
|
Length |
19.62 ft (5.98 m) |
|
Height |
8.14 ft (2.48 m) |
|
Wing span |
28.40 ft (8.65 m) |
|
Cabin width |
3.87 ft (1.18 m) |
|
Baggage compartment volume |
10.06 cu.ft (285 l) |
|
Weights & Quantities |
|
|
Empty weight |
756 lb (343 kg) |
|
Maximum take-off weight |
1 320 lb (600 kg) |
|
Maximum baggage |
55 lb (25 kg) |
|
Design load factors |
+6 / -3g |
|
Operation load factors |
+4 / -2g |
|
Performance |
|
|
Engine |
Rotax 912ULS |
|
Never exceed speed |
146 kts (270 km/h) |
|
Maximum level speed |
115 kts (213 km/h) |
|
Cruising speed (75% of MCP) |
92 kts (171 km/h) |
|
Stalling speed |
42 kts (78 km/h) |
|
Rate of climb |
876 fpm (4.5 m/s) |
|
Service ceiling |
15 500 ft (4720 m) |
|
Take-off run (concrete RWY) |
420 ft (128 m) |
|
Take-off distance over 50 ft obstacle (concrete RWY) |
1 200 ft (365 m) |
|
Landing run (concrete RWY) |
555 ft (169 m) |
|
Range |
700 nm (1 300 km) |
Powerplant
|
Engine |
Bombardier Rotax 912ULS |
|
No. of cylindres |
4 |
|
Maximum power |
100 hp |
|
TBO |
2000 hours |
|
Fuel |
Unleaded automotive gasoline or AVGAS 100LL |
|
Propeller |
3-blade, on-ground adjustable propeller Woodcomp Klassic 1700/3/R |