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H135

General Information

  • Make : Airbus Helicopters
  • Model : H135 P3
  • YOM : 2010
  • TTSN : 1740 hrs
  • Engine Type : PW206B2
  • Mission : VIP
  • Flight Rule : IFR
  • Available : Immediately
  • Location : On request
  • Asking Price : On request

Medias:

Avionics


  • AV PACK DP IFR GC G430
  • Digital Audio Control System (NAT), incl. AMU50, ACP53 pilot and copilot
  • Transponder (Mode S) GTX330 (Garmin)
  • DME Rockwell Collins
  • Marker beacon KR 21 (Honeywell)
  • GPS / NAV / COM GNS 430W, pilot and copilot (Garmin) interfaced with FCDS
  • 2” stand-by horizon AI 804 DC (Goodrich) with emergency battery
  • MEGHAS - Flight Control Display System (FCDS) - Dual (4xSMD45)
  • Radar altimeter KRA 405 B (Honeywell)
  • Fixed provisions for ANR
  • MEGHAS Sensor Kit
  • Copilot pitot static system
  • Digital Automatic Flight Control System-DAFCS
  • Fixed provisions for ANR
  • ADF control unit CDF-552 (Chelton Wulfsberg)
  • ADF receiver DF-431B (Chelton/Wulfsberg)
  • Color weather radar RDR 2000 (Honeywell)
  • Video Radar Unit (VRU)

  • Equipment & Interior


  • Inlet barrier filter system
  • Battery, type "Saft", ULM, 40 Ah, 24 V
  • Engine fire extinguishing system
  • AC system (50 VA)
  • Engine outlet heat protection
  • Starter/generator (2 x 200 A, 28V DC)
  • Flashlight copilot side
  • Rotor brake system
  • Tinted sun shades for cockpit windshield roof section
  • Reinforced rear landing gear cross tube
  • Slant panel & Center console
  • Landing & search light, 450 W
  • Avionics compartment
  • Sliding windows in sliding doors
  • Copilot flight controls
  • Windshield wiper system
  • 7" copilot instrument panel with glare shield
  • Windshield wiper system
  • Map case in copilot door
  • Fuel management system (Fuel flow meters)
  • Bleed air heating system
  • Strobe lights, white
  • Air conditioning system
  • ELT C406-N HM (Artex) incl. NAV. opt.

  • Printable version : EC135_P3.pdf