2012 Airbus EC135 P2+ P2i Turbine Helicopter For (SOLD)

HEMS configuration, SP/DP IFR, NVIS Certified, A/C TT 6454 FH / 18338 cycles (as per 5/9-22), Operated & based in Norway & Denmark, Fully covered by PbH & FMP contracts.

Type:
Helicopter (Turbine)
Manufacturer:
Eurocopter
Model:
EC135 P2+
Year:
2012
Serial Number:
1033
Reg. Number:
LN-OON
Total Time:
6,454 Hours
Seats:
4
Price:
Price upon request

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Description

General
Components & spare parts available for sale
MTOW enhanced at 2950 kg
MEGHAS Dual Flight Control Display System
Tactical radio provisions
Dual cargo hook system
Aerolite Medical interior
Flightcell DZMx cellular & Iridium satellite system, with GPS tracking solution
Flightcell external WIFI router
GSM/4G Medi-link antenna system & power, outlets in FWD cabin (16VDC 5A)
ACP51 audio panel in cabin
3rd Tetra antenna with connection in centre console for loose equipment
Dart Bearpaws
Dart skidtube & wearplates
Moving map EuroNav 7, with Iridium SAT, GSM / UMTS, & FLARM module
Flarm traffic system
IPAD holders for pilot & co-pilot

Customized Options Configuration
Airbus Helicopters Extra Options From 2012
EC135 P2+ with MTOW-enhanced at 2950 kg
Engine fire extinguishing system
Center console
Instrument panel ext. on co-pilot side
Map cases on instrument panel glare shield, co-pilot door, pilot door & centre console
Co-pilot flight controls (detachable parts)
Bleed air heating system with add. air outlets in cargo compartment
Battery (40 Ah, 24 VDC) ULM (Saft) instead of standard battery
Alternating Current (AC), 50 VA
Starter/generator (2 x 200 A, 28V DC) instead of standard generator
Reinforced rear landing gear crosstube
Dual Landing & search light (400 W/200 W)–NVG
Fixed landing light
White strobe lights
Emergency Locator Transmitter (ELT) incl. NAV option C406N HM (Artex)
Standard cockpit, cabin & cargo compartment – NVG, with separation curtain for cockpit/ cabin
Night Vision Imaging System (NVIS) certification, basic
Enhanced exterior painting instead of standard painting
Tinted sunshades for cockpit windshield roof section
Clam-shell doors with window, one-h& latching & ext. opening fastener
Sliding door max position, LH & RH
Jettisonable cockpit doors
Dual cargo hook system
Cable cutter system (WSP)
Rotor brake system
Fuel management system (fuel flow meters)
Accelerometers for track & balance system VMSII (Chadwick Helmuth)
Engine cowling heat protection, compressor wash kit
Windshield wiper system
Height adjustable pilot & co-pilot seat instead of standard seats
Extra multifunction handle on main gearbox cowling LH & RH
Emergency lights incl. boarding step illuminations
Emergency hammer

Avionic Package Dual Pilot IFR
MEGHAS dual (2xSMD45 / 1xSMD68) Flight Control Display System (FCDS)
FCDS/DAFCS GPS selection switch for GNS430AW (Garmin)
GPS/NAV/COM GNS430AW (Garmin), pilot & copilot w/COM 16w
Digital Audio Control System (NAT), incl. AMU 50, ACP53 pilot & copilot.
Transponder incl. Mode-S GTX330 – NVG (Garmin)
Distance Measuring Equipment DME-4000 (Rockwell Collins)
Marker beacon receiver & lights KR21(Honeywell) – NVG
Radar altimeter KRA 405B (Honeywell)
Dual Attitude & Heading Reference System (AHRS) & magnetometer
Dual pitot static system
3-axis Automatic Flight Control System (DAFCS)
Tactical radio system VHF-FM maritime freq. (NAT) NTX138E (radio) w/ TH250C (ctrl-pnl) & UT12-000 (tone decoder FM)
Tactical radio, Cobham dual Tetra radio system with dual control head in cockpit & cabin (Provision only, no radio’s delivered)
Wireless intercom system (Axnes), Polycon
Search & rescue weather radar RDR-1600 (Telephonics) Interfaced to EuroNav 7 & FCDS
Traffic Advisory System TAS620 (Avidyne)

Standard Helicopter Definition
Basic Instrumentation
Central Panel Display System (CPDS), consisting of:
Caution Advisory Display (CAD) with indication
of:
Caution & advisory information
Fuel quantity indication

Vehicle & Engine Multifunction Display (VEMD) with indication of:
Torque
Engine parameters N1-RPM, oil pressure, oil temperature, Turbine Outlet temperature (TOTI. engine/ FA DEC rep EEC failure & parameter code messages, self diagnoses)
First Limit Indicator (FLl) for TQ, TOT, N1
Main transmission parameters (oil pressure, oil temperature)
Dual ammeter (generator)
Ammeter (battery)
Dual voltmeter
Outside Air Temperature (OAT)
Automatic in-flight power check
Parameters of optional equipment (e.g. internal long range fuel tank)

Clock (2″)
Magnetic compass
Engine cycle counter (on flight report page)
Triple (rotor & engines) RPM-indicator (2″)
Back-up instruments: (single pilot)”
Airspeed indicator (2″)
Altimeter (2″)

Warning unit:
Engine fire warning w/fuel emergency shut-off
Warning lights
Aural warning

Main switch panel:
DC power control
Full Authority Digital Engine Control (FADEC)

Pilot static system with electrical heated pilot tube, pilot side
Static pressure crossover system
Air Dala Computer (ADC)

Power plant:
Two Pratt & Whitney PW206B2 turbine engines. These two engines are equipped with:
Fire detectors
Full Authority Digital Engine Control (FADEC)
Chip detectors with quick-disconnect plugs
Overspeed protection system
Twin-engine OEl-training mode
Oil cooling & lubricating system with thermostatic valve
Crash resistant fuel system with a flexible bladder-type
fuel main tank & supply tank (split into two sections)
Automatically controlled variable rotor speed system
Fuel tank filler flap, lockable

Transmission system:
Flat-shaped main gearbox with two stages
Chip detector system with quick-disconnect plug (main gearbox)
Redundant oil cooling & lubrication system
Main gearbox attachment with Anti-Resonance Isolation System (ARIS)
Free wheel assemblies in the engine input drives
Tail rotor drive shaft
Tail rotor gearbox with splash lubrication & oil level sight gauge
Chip detector system with quick-disconnect plug (tail rotor gearbox)

Rotor & Flight controls:
Bearingless Main Rotor system (BMR), consisting of:
Rotor head / mast in one piece
Four fiber-reinforced composite main rotor blades with anti-erosion strips, control cuff, elastomeric lead-lag dampers & special blade tip painting

Main rotor control system with dual hydraulic boost system
Electrical trim system (cyclic)
Basic provisions for an easy integration of a track & balance system
Fenestron®-type tail rotor with ten metal blades (asymmetric blade spacing) & stator
Tail rotor gearbox cover
Tail rotor control system with flex ball cable & single hydraulic booster
Yaw-SAS (Stability Augmentation System)
Mast moment system