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

2023 New Extra Aircraft 330 LT

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
Fuselage assembly, 1.7734 steel
Powerplant and propeller
Lycoming AEIO-580-B1A, 315 hp, 6 cylinder engine
Cockpit
Fixed composite front seat, contour moulded
Systems
Electric stall warning system
Standard panel equipment
Airspeed indicator (kts)
Aircraft dimensions
wingspan 26,3 ft / 8,0 m
Weights
typ. equipped empty weight 1.493 lbs / 677 kg
Airspeeds
never exceed speed (Vne) 220 kts
FUEL
total capacity 58,4 gal / 221 ltr

Description

  • Carbon fibre wing assembly with integral tank
  • Carbon / glass hybrid composite empennage structure
  • Fiberglass landing gear spring
  • Choice of steerable, lightweight tailwheel or soft tailwheel
  • Two-seat bubble canopy
  • 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
  • Adjustable composite rear seat, contour moulded
  • Forward rudder pedals with differential toebrakes
  • Front and rear seat Hooker safety harness with ratchet
  • 2 front and 2 rear bezel-operated air vents
  • Moulded control stick handle
  • Pitot static system drain
  • 65 Amp alternator
  • 12V battery
  • LED nav lights
  • Cowling light, strobe lights
  • Electric trim system
  • Smoke system (optional)
  • Altimeter (ft, inHg/hPa)
  • Mechanical accelerometer
  • Magnetic compass

Aspen pfd

Aspen mfd

  • GARMIN GNS 430W
  • XPDR GARMIN GTX 328 mode S
  • EI MVP-50P engine monitor
  • Intercom syst. NAT AA83
  • ARTEX 406MHz ELT (optional)
  • length 23,0 ft / 7,01 m
  • height 8,6 ft / 2,6 m
  • wing area 116,7 ft2/ 10,84 m2
  • 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) 60 kts
  • stall speed at 2.095 lbs / 950 kg (Vs) 65 kts
  • usable fuel 55,2 gal / 209 ltr
  • usable fuel – acro tanks only 17,7 gal / 67 ltr

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