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Eurocopter

Eurocopter

EC135 P2+

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: 2013
  • Manufacturer: Eurocopter Deutschland GmbH
  • Model: EC135P2+
  • Total Flight Time: 1,407:03 hrs
  • Total Landings: 2,304
  • C of A / ARC: Non-Expiring / Jul 15, 2018
  • MTOW: 2,950 kg
  • Empty Weight : 1,951.5 kg
  • Condition: Excellent condition, no damage history

Major Components

  • Engines: Pratt & Whitney Canada PW206B2
  • Engine No.1: TT 1,407:03 hrs, TTO 2,592:57 hrs, CT 1,184 cyc, PT 1,379 cyc
  • Engine No.2: TT 1,407:03 hrs, TTO 2,592:57 hrs, CT 1,169 cyc, PT 1,378 cyc
  • Main Gearbox: TT 1,407:03 hrs, TTO 3,592:57 hrs
  • TR Gearbox: TT 1,407:03 hrs, TTO 3,592:57 hrs
  • Main Rotor Blades: TT 1,407:03 hrs
  • Tail Rotor Blades: TT 1,407:03 hrs, TTSLL 10,592:57 hrs
  • MR Servo No.1: TT 1,407:03 hrs, TTO 6,092:57 hrs
  • MR Servo No.2: TT 1,407:03 hrs, TTO 6,092:57 hrs
  • MR Servo No.3: TT 1,407:03 hrs, TTO 6,092:57 hrs
  • Rotor Mast Hub: TT 1,407:03 hrs, TTSLL 12,592:57 hrs

Mission Configuration

  • Configuration: Utility 5 passengers + 2 crew
  • Emergency Floatation gear - provisions
  • External loud speaker with siren - provisions
  • Tactical radio - provisions
  • NVG compatible external lighting
  • High back seats with fixed height headrests
  • 4 point crew / 3 point passenger with lap strap and diagonal shoulder harnesses
  • External loudspeaker with siren

Installed & Miscellaneous Equipment

  • TCAD - fixed provisions
  • KANNAD AP-H Integra (ER) ELT
  • Weather radar - fixed provisions
  • CVFDR - fixed provisions
  • 450W searchlight
  • Heated co-pilot static system
  • Digital Automatic Flight Control System (DAFCS)
  • Dual windshield wipers
  • Engine chip detector ‘fuzz burner’
  • Engine compressor washing facility
  • Sliding window vents in cockpit doors
  • Removable tinted sun shades
  • Removable floor panels - floor protector not installed
  • Push-out cabin windows
  • Enlarged cabin footstep
  • Pilot’s illuminated chart holder
  • Fuel flow meter installation
  • Sliding door open door restraint with mid and max positions
  • Reinforced rear cross tube
  • Track & balance accelerometers
  • Dual controls
  • Stability Augmentation System (SAS)
  • Rotor brake
  • Keith bleed air heating system
  • Air conditioning
  • 40Ah battery upgrade
  • 200 Amp starter generator upgrade
  • Sound proofing kit

Avionics

  • VHF Comm / NAV / VOR / LOC / GPS: Garmin GNS 430W
  • VHF Comm / NAV / VOR / LOC / GPS / TAWS: Garmin GNS 530W T
  • ATC Transponder Mode ‘S’: Garmin GTX 330
  • Stability Augmentation System Computer: SFIM SAS 2000
  • Auto-Pilot Module: SFIM APM 2000
  • Auto-Pilot Flight Control: SFIM APMS 2000
  • Fixed Emergency Location Transmitter: Kannad AP-H Integra (ER)
  • AHRU: Sagem 261500123-0460
  • DME: Collins DME 4000
  • Marker: Bendix / King KR 21
  • 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: 64:48 hrs remaining
  • 12 Month Inspection: 12 months remaining
  • 1,000 Hour / 36 Month Inspection: 577:26 hrs / 16 mths remaining