1985 Westwind II

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The Westwind II is a light business jet that was produced by Israel Aircraft Industries (IAI) from 1984 to 1999. It is a twin-engine, low-wing aircraft with seating for up to seven passengers. The Westwind II is powered by two Garrett TFE731-2 turbofan engines, which provide a maximum cruise speed of 482 knots and a maximum range of 1,700 nautical miles. The aircraft is capable of operating at altitudes up to 45,000 feet. The Westwind II was designed to be a comfortable, cost-effective business jet and was used by both private and charter operators. It was also used by government agencies and military organizations around the world. The Westwind II was succeeded by the Westwind 1124 in 1999.


  • Total Time: 7283
  • Collins Proline with 8.33 Spacing and FM Immunity
  • Collins Five Tube EFIS 85A
  • Collins FDS-85A
  • Collins VHF 20C Coms
  • Collins VIR-30A Navs
  • Collins DME 42
  • Collins RMI 36
  • Collins TRD-90 Transponders
  • Collins LAT 50 Radar ALT
  • Collins ADF -60
  • Colling WXR-250A Color Radar
  • Colllins ADS-80 Central Air Data System
  • Fairchild A 100 CVR
  • Agrus 5000 Moving Map
  • King KLN900 GPS
  • Ryan TS-9900 TCAD
  • Single Univeral UNS1F TAWS
  • Additional Equipment:
  • RVSM Certified
  • High Reliance Engine Mods
  • Grumman FIDA 58 Thrust Reversers
  • Keith Freon Air
  • Single Point Refueling
  • Artex ELT with 406 MHz and FMS Interface
  • KGS SPS206 200VA Inverter with Two Cablin Outlets
  • Teledyne Angle of Attack

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