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Extra Flugzeugproduktions-und VertriebsSingle-engine piston · Germany, Hünxe, Nordrhein-Westfalen

2023 New Extra Aircraft 330 LX

Price
On request
Year
2023
Total time
1 hours
Location
Germany

Specifications

General

Registration
TBA
Total time
1
Seats
2
Condition
New
Type
Airplane (Single Engine Piston)
Sale
aircraft for sale

Description

Airframe
Carbon fibre wing assembly with integral tank
Powerplant and propeller
Lycoming AEIO-580-B1A, 315 hp, 6 cylinder engine
Cockpit
Manually adj. rudder pedals with differential toebrakes
Systems
Two fuel pumps (1 engine-driven, 1 electric)
Standard panel equipment
Airspeed indicator (kts)
Aircraft dimensions
wingspan 26,3 ft / 8,0 m
Weights
typ. equipped empty weight 1.455 lbs / 660 kg
Airspeeds
never exceed speed (Vne) 220 kts
FUEL
total capacity 49,9 gal / 189 ltr

Description

  • Carbon composite empennage structure
  • Fuselage assembly, 1.7734 steel
  • Steerable, lightweight tailwheel
  • Fiberglass landing gear spring
  • Two-seat bubble canopy
  • Carbon pushrods
  • Titanium firewall
  • Muehlbauer, MTV 9-B-C/C198-25, 3-blade propeller
  • Two fuel pumps (1 engine-driven, 1 electric)
  • Gomolzig, 6-in-1 exhaust system
  • Single oil cooler system
  • Electric starter
  • Contour moulded composite seat, adjustable
  • Front and rear seat Hooker safety harness with ratchet
  • Forward rudder pedals with differential toebrakes
  • Adjustable composite rear seat, contour moulded
  • fixed composite front seat, contour moulded
  • 2 front and 2 rear bezel-operated air vents
  • Strobe / navigation lights at wing tips
  • Electric stall warning system
  • Pitot static system drain
  • Trickle charger socket
  • 65 Amp alternator
  • 12V battery
  • 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
  • length 22,8 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
  • 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
  • manoeuvring 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
  • usable fuel 49,4 gal / 187 ltr
  • usable fuel – acro tanks only 17,7 gal / 67 ltr

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