Экстра 300 — спортивный самолёт, моноплан, обладает практически неограниченными возможностями в аэробатике. Разработан Вальтером Экстра, немецким спортивным пилотом в 1987 году под брендом основанной им компании Extra Flugzeugbau. Силовая установка — инжекторный двигатель Лайкоминг AEIO-540 мощностью 300 л. с. (224 кВт).
Практически основной самолёт мировой серии по аэробатике Red Bull Air Race.
| AIRFRAME |
| |
- Fuselage assembly, 1.7734 steel
- carbon fiber wing assembly with integral tank
- carbon / glass hybrid composite empennage structure
- fiberglass landing gear spring
- choice of stearable, lightweight tailwheel or soft tailwheel
- two seat bubble canopy
|
|
|
| POWERPLANT AND PROPELLER |
| |
- Lycoming AEIO-540-L1B5, 300 hp, 6-cylinder engine
- Gomolzig 6-in-1 exhaust system
- single oil cooler system
- Muehlbauer, MTV 9-B-C/C200-15, 3-blade propeller
- electric starter
- two fuel pumps (1 engine-driven, 1 electric)
|
| |
|
| |
|
|
| COCKPIT |
| |
- Fixed composite front seat, contour molded
- adjustable composite rear seat, contour molded
- forward rudder pedals with differential toe brakes
- electrically adjustable rear rudder pedals with differential toe brakes
- front and rear seat Hooker safety harness with ratchet
- 2 front and 2 rear bezel-operated air vents
|
|
|
| SYSTEMS |
| |
- Electric stall warning system
- pitot static drain
- 65 amp alternator
- 12 V battery
- strobe / navigation lights at wing tips
- trickle charger socket
- optional smoke system
|
|
| |
|
|
| STANDARD PANEL EQUIPMENT |
| |
- Airspeed indicator (kts)
- altimeter (ft, inHg/hPa)
- mechanical accelerometer
- magnetic compass
- slip and skid indicator, with holder if req'd
- digital RPM indicator
- analog fuel gauges
- analog CHT/EGT, oil press./oil temp. gauges
- digital V/A indicator
- MAP/FF indicator
|
|
| AIRCRAFT DIMENSIONS |
| |
| wingspan |
26,3 ft - 8 m |
| length |
22,30 ft - 6,9 m |
| height |
8,6 ft - 2,6 m |
| wing area |
115,2 ft² - 10,7 m² |
| FAA / EASA certified load factor |
+/- 10 g |
|
|
 |
| |
|
|
| WEIGHTS |
| |
| typ. equipped empty weight |
1.480 lbs - 672 kg |
| MTOW normal category (+6/-3g) |
2.095 lbs - 950 kg |
| MTOW two-pilot acro (+8/-8g) |
1.918 lbs - 870 kg |
| MTOW single-pilot acro (+10/-10g) |
1.808 lbs - 820 kg |
|
|
| |
|
|
| AIRSPEEDS |
| |
| never exceed speed (Vne) |
220 kts |
| maneuvering speed (Va) (acro) |
158 kts |
| stall speed at 1.808 lbs / 820 kg (Vs) |
55 kts |
| stall speed at 2.095 lbs / 950 kg (Vs) |
60 kts |
|
|
| |
|
|
| FUEL |
| |
| total capacity |
49,9 gal - 189 ltr |
| usable fuel |
49,4 gal - 187 ltr |
| usable fuel - acro tanks only |
17,7 gal - 67 ltr |
|
Создание сайта