PIPER PA-28

Characteristics

Airframe

Elapsed time 2870 h
Assigned life Unlimited

Engine

Model Centurion 2.0S
Elapsed time 12 h
Capacity 155 hp
Overhaul period 1500h

Propeller

Model MT Propeller MTV-6A/187-129 Three-bladed, controllable pitch
Elapsed time 12 h
Overhaul period 2000 h

Interior and painting

Seat capacity 4
Interior
  • Leather cabin (2012 year)
  • White and red (2012 year)

Avionics

Dual system Dynon Sky View
  • Two 10” multifunctional displays D1000
  • Digital horizon indicator (EFIS) with three-dimensional representation of relief, airdromes, etc. (Synthetic Vision)
  • Digital indicators – of air speed, height, altitude, climb-and-dive indicator, heading indicator (HSI) with flight plan data displaying or radio-navigation beacon (VOR), digital terrain map (GPS) with topography and air navigation
  • Dual axial autopilot, standby power supply for 30 minutes of flight
  • Dual digital gyroscopes and air data computers
  • S-mode transponder
  • GARMIN SL30 radio station providing receiving/transmission at a given frequency with simultaneous listening to another frequency
  • Dual navigation (VOR) receiver with course data representation on D1000 displays
  • KANND 406 emergency location beacon, with GPS and COSPAS/SARSAT Rescue Satellite System
  • Audio-panel suitable for mobile phone, music connection, etc.
  • Spare mechanical air speed and altitude indicators

Flight characteristics

Takeoff run 283 m
Climb rate 3,51 m/s
Flight range 1980 km
Maximum speed 250 km/h
Fuel Kerosene (TS-1), eurodiesel
Tank capacity 182 l
Consumption 16-20 l/h