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Eurocopter

Eurocopter

EC135 T2+

Specification may change without prior notice. Aircraft and component maintenance life remaining and technical data subject to verification prior to purchase or lease.

Key Features

  • Low Total Time
  • Passenger Configuration with EMS Provisions
  • Night Vision Goggle Compatible External Lighting
  • Single/Dual Pilot IFR
  • Air Conditioning
  • 40Ah battery upgrade
  • 200 Amp starter generator upgrade

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General Information

  • Year of Manufacture: 2011
  • Manufacturer: Eurocopter Deutschland GmbH
  • Model: EC135 T2+
  • Total Flight Time: 1,285:31 hrs
  • Total Landings: 1,988
  • C of A / ARC: Non-Expiring / Aug 03, 2017
  • MTOW: 2,910 kg
  • Empty Weight : 1,851.48 Kg
  • Condition: Excellent condition, no damage history

Major Components

  • Engines: Turbomeca Arrius 2B2
  • Engine No.1: TT 1,285:31 hrs, TTO 2,714:29 hrs, CT 757.89 cyc, PT 1,680.72 cyc
  • Engine No.2: TT 1,285:31 hrs, TTO 2,714:29 hrs, CT 742.85 cyc, PT 1,677.11 cyc
  • Main Gearbox: TT 1,285:31 hrs, TTO 3,714:29 hrs
  • TR Gearbox: TT 1,285:31 hrs, TTO 3,714:29 hrs
  • Main Rotor Blades: TT 1,285:31 hrs,
  • Tail Rotor Blades: TT 1,285:31 hrs, TTSLL 10,714:29 hrs
  • MR Servo No.1: TT 1,285:31 hrs, TTO 6,214:29 hrs
  • MR Servo No.2: TT 1,285:31 hrs, TTO 6,214:29 hrs
  • MR Servo No.3: TT 1,285:31 hrs, TTO 6,214:29 hrs
  • Rotor Mast Hub: TT 1,285:31 hrs, TTSLL 12,714:29 hrs

Mission Configuration

  • Configuration: Utility 5 passengers + 2 crew
  • Emergency Floatation gear - provisions
  • External loud speaker with siren - provisions
  • Tactical radio - provisions
  • NVG compatible cockpit layout
  • NVG compatible cockpit and cargo compartment lighting
  • NVG compatible external lighting
  • NVG formation lights
  • 400W NVG compatible searchlight
  • External loudspeaker with siren
  • High back seats with fixed height headrests
  • 4 point crew and passenger harnesses

Installed & Miscellaneous Equipment

  • ARTEX C406-N HM ELT with NAV option
  • Heated co-pilot static system
  • Digital Automatic Flight Control System (DAFCS)
  • Upper, lower and skid Wire Strike Protection System (WSPS)
  • Dual windshield wipers with wire strike deflector
  • Engine chip detector ‘fuzz burner’
  • Engine compressor washing facility
  • Sliding window vents in sliding cabin doors
  • Keith bleed air heating system
  • 40Ah battery upgrade
  • 200 Amp starter generator upgrade
  • Pilot and co-pilot illuminated chart holder
  • Self-sealing engine fuel supply tank
  • Fuel flow meter installation
  • High wind tie down kit
  • Engine sand filter fixed provisions
  • Boarding step illumination
  • Washable cockpit, cabin and cargo compartment floor covering
  • Sliding door open door restraint with mid and max positions
  • Jettisonable cockpit doors
  • 12 volt electrical outlet
  • Reinforced rear cross tube
  • Track & balance accelerometers
  • Dual controls
  • Stability Augmentation System (SAS)
  • Rotor brake

Avionics

  • VHF Comm: Bendix / King KTR 908
  • VOR / LOC / GS Nav: Bendix / King KNR 634A
  • ADF: Chelton DF-431B
  • ATC Transponder Mode ‘S’: Bendix / King MST 67A
  • Stability Augmentation System Computer: SFIM SAS 2000
  • Auto-Pilot Module: SFIM APM 2000
  • Auto-Pilot Flight Control: SFIM APMS 2010
  • Fixed Emergency Location Transmitter: ARTEX C406-N HM
  • AHRU: SFIM 420-00332-460
  • DME: Chelton CDM-451
  • GPS Receiver: FreeFlight TNL 2101 I/O +
  • ADU: Thales ADU 3200
  • Radio Altimeter: Bendix / King KRA 405B
  • Smart Mulftifunction Display: Thales SMD-45H
  • Instrument Control Panel: Thales ICP NVG
  • Flight control Display Unit: Thales FCDM
  • Caution and Advisory Display: Thales CAD

Scheduled Maintenance Inspections

  • 500 Hour Inspection: 69:57 hrs remaining
  • 12 Month Inspection: 4.5 mths remaining
  • 1,000 Hour / 36 Month Inspection: 185:53 hrs / 4.2 mths remaining