Airbus - Helicopter h 130 - with certified autopilot - like new-, 2016

 1 avionics master switch
 1 gyro-horizon
 1 gyro-compass with
 1 Horizontal Situation Indicator
 1 turn and bank indicator
 1 VHF/VOR/LOC/GS/GPS
 1 transponder (mode S)
 1 altitude encoder
 1 Emergency Locator Transmitter
 1 ICS passenger interphone
1VHF/VORLOC/GS
Autopilot

 The EC130 T2 is certified with a pilot being on the left side
 The baseline aircraft is delivered with left side controls and capabilities for the removable dual controls (copilot controls are optional)
 Anti-Vibration Control System with 1 controller, actuators and accelerometers
 Fuselage comprising the cabin and 3 luggage holds, with floor tie-down nets and access doors
 Tail boom with stabilizer, FENESTRON type anti torque rotor, and tail skid
 Tubular skid landing gear, with replaceable skid shoes,
with long footsteps (on right and on left side), profiler on rear tube, capable of taking handling wheels
 Lifting points
 Mooring fixtures
 Single color exterior painting
 Internal paint: light grey (prevailing colour)
 Interior signs and markings: available in either French or English

COCKPIT / CABIN
 Cabin floor in light-alloy sheet-metal
 1 pilot high-back energy-absorbing seat, adjustable in reach, removable, complete with cushions, safety belts and shoulder harnesses
 6 passengers high-back energy-absorbing seats, removable, complete with cushions safety belts and shoulder harnesses:
 2 front right, including for 1 copilot (copilot controls are optional)
 4 rear row
 2 cockpit jettisonable hinged doors
 1 LH front door fitted with a sliding window
 1 RH front door compatible with 8 seat layout
 1 LH rear sliding door
 1 RH rear sliding door
 Locks on every access to cabin and luggage
 Lock on fuel cap
 Lateral and upper tinted windows (windscreen excluded)
 1 ceiling housing the cabin lighting, 7 air ventilation outlets and controls (rotor brake and fuel cut-off)
 Dynamic ventilation system
 Cabin heating
 Demisting system for front windscreens
 2 pilot document holders
 Door map case in LH and RH front doors
 Rear bulkhead and lateral rear upholstery
 1 fire-extinguisher
 1 Flight Manual: available in either French or English
 Interior harmony according to definition in force
compartments

INSTRUMENTS
 1 airspeed indicator
 1 altimeter
 1 vertical speed indicator
 1 LCD rotor and free turbine dual indicator
 1 stop watch
 1 warning panel
 1 magnetic compass
 1 heated pitot head
 1 external side slip indicator
 1 control box for light and electrical generation
 1 ICS connection to audio warning issued from VEMD
 1 cockpit imaging and flight data monitoring device
 1 LCD dual screen Vehicle and Engine Multifunction
Display (VEMD) providing the following information:
 First Limit Indicators (FLI)
 torquemeter
 exhaust gas temperature (TOT)
 gas generator tachometer (N1)
 Engine oil temperature, pressure
 Fuel quantity
 Fuel flow and estimated remaining time to fly
 Ammeter and voltmeter and battery temperature
 Outside Air Temperature (OAT)
 Enhanced usage monitoring functions
 IGE/OGE performance calculations
 engine cycles counting
 engine power check
 overlimits display
 VEMD and peripheral maintenance information
 Data downloading capability (software and connection
wire as option)
AVIONICS
 1 avionics master switch
 1 gyro-horizon
 1 gyro-compass with
 1 Horizontal Situation Indicator
 1 turn and bank indicator
 1 VHF/VOR/LOC/GS/GPS
 1 transponder (mode S)
 1 altitude encoder
 1 Emergency Locator Transmitter
 1 ICS passenger interphone
 1 VHF/VORLOC/GS
POWER PLANT
 1 Turbomeca ARRIEL 2D turbine engine complete with starting, fuel supply and dual channel digital engine control system (FADEC) and 1 back-up fuel control box that automatically controls the engine in case of a total failure of the 2 digital channels of the FADEC
 1 crashworthy fuel system including 1 tank of 540 liters (143 US gal.) total capacity
 1 twist grip on pilot side (for engine reduction in case of tail
 1 magnetic plug and 1 chip detector
 1 engine lubrication and oil cooling system
 1 fire detection system
 1 air-intake protection grids
 1 torque-measurement pick-up
rotor failure and autorotation training)
TRANSMISSION SYSTEM
 1 main gearbox, anti-vibration mounted, with oil sight gauge, chip detector, oil temperature and pressure switches, port for endoscope and self sealing valve for oil sampling and draining
 1 main gearbox oil cooling system
 1 engine to main gearbox coupling shaft
 1 main rotor high and low r.p.m. warning device
 1 tail drive carried by five anti-friction bearings
 1 tail gearbox with oil sight gauge, chip detector and port for endoscopic inspection
 1 rotor brake
ROTORS AND FLIGHT CONTROLS
 1 main rotor with 3 composite-material blades around a STARFLEX head fitted with spherical thrust bearings
 1 anti-torque rotor (FENESTRON) with 10 asymmetrical blades, integrated in vertical fin
 3 main rotor hydraulic servo units (duplex servos)
 Integrated back-up control valve on each body of each duplex servo
HYDRAULIC GENERATION
 2 independent hydraulic systems feeding the duplex servos
ELECTRICAL INSTALLATION
 One 150 A, 28 VDC starter-generator
 One 15 A.h cadmium-nickel battery
 1 ground power receptacle
 3 position lights (LED)
 1 flashing anti-collision light (LED)
 2 fixed landing lights
 2 cabin light sets, each with 2 reading lights for 2 rear
passengers and 1 dome light
 1 integrated instrument panel lighting system
 Integrated lighting in central console
 1 reading map light on upper canopy strut for pilot
 1 cockpit breaker panel
 One 28 V DC cabin power outlet
AIRBORNE KIT 1
 1 pitot head cover
 2 static port stoppers
 1 engine air-intake blanking cover
 1 exhaust pipe blank
 2 ground handling bogies
 1 cargo net and rope
 1 lifting ring
 2 upper mooring rings
 3 main-blade socks and pole
 1 document holder
 1 airborne kit stowage bag
 1 front air-intake blanking cover
 1 fuel tank bleeding
 3 ballast plates
1 Weight not included in baseline aircraft empty weight.

Appendix 2 Technical Configuration
00-10010-04-CI EC130 T2 Baseline Aircraft
"as per 130 T2 15.100.03.E, and including:
- VEMD
- NR & NTL indicator
- Control Warning Panel
- Altimeter
- Air Speed indicator
- Vertical Speed Indicator
- External side slip indicator
- Stop watch
- Magnetic Compass
- Cockpit camera"
Avionics
08-00025-03-CI VFR day and night package, included in baseline definition
06-67076-02-CI Emergency locator transmitter - Kannad INTEGRA AP-H
"2 frequencies: 121.5 MHz (VHF), 406 MHz (COSPAS-SARSAT).
The Programming Data Sheet must be filled and communicated by the customer two months at the latest before the helicopter's delivery."
08-11048-00-CI VHF/VOR/LOC/GS - Garmin GNC 255A
08-16119-00-CI Intercom system (ICS) - Garmin GMA 35
08-22061-01-CI Transponder (mode S) - Garmin GTX 33H
The mode S identification must be communicated by the customer two months at the latest before the delivery.
08-43073-00-CI VHF/VOR/LOC/GS/GPS - Garmin GTN 750H
This equipment is delivered with the original EUROPE map. Subscription for updates to be made by the customer.
08-51002-01-CI Gyro-horizon Thales H 321 EGM
08-52011-01-CI Gyro Compass Honeywell KCS 55A with Horizontal Situation Indicator Honeywell KI 525A
08-57011-01-CI Altitude encoder - Trans-cal
08-63006-01-CI Turn and Bank indicator UI 9560
- 2 -
Optional Equipment List
05-02079-00-CI Engine exhaust area black thermal painting
05-21002-00-CI Cable cutter system
05-23005-00-CI Engine flushing device without removal of cowlings
05-24005-00-CI High visibility paint scheme on main rotor blades
05-25027-01-CI Enhanced Engine Air Particle Separator
05-25029-00-CI Heavy duty blade pins
05-31025-00-CI Tinted windows for front windscreens
05-31033-00-CI Sun protected upper windows
05-32012-00-CI Pilot's windshield wiper
05-37015-00-CI Dual controls
05-42025-03-CI Enhanced Air conditioning system
05-63002-03-CI Thales Avionics 200A starter-generator instead of Skurka 150A in baseline
06-11006-00-CI Short protective skid shoes
06-26026-00-CI-STC Dual external cargo sling mirrors
06-27048-00-FP Cargo sling (1500kg) - Fixed Parts
06-27048-00-RP Cargo sling (1500kg) - Removable Parts
06-42017-00-CI Landing light adjustable in site and azimuth
06-61006-00-FP Emergency floatation gear - Fixed Parts
06-93000-00-CI Additional ballast plates in tail boom

Interior Layout
07-00021-02-CI STYLENCE Layout Harmonie Scheme :Titanium

Optional Avionics
08-18037-01-CI ICS installation compatible with Bose headset
08-21008-08-CI Radio altimeter Thales AHV16, instead of Turn and Bank indicator UI 9560
08-51015-01-CI Stand-by gyro-horizon Thales H321EGM
08-83017-00-CI VEMD data download kit
Optional Avionics Retrofit Airbus Kassel
1 2 Axis Autopilot HeliSAS
2 Garmin G 500 H
3 Garmin TAS GTS 800

Appendix 3 Paint Scheme
Exterior painting Single Colour BMW mineral grey - BMW Color Code B39
Landing gear Single Colour BMW mineral grey - BMW Color Code B39 Engine exhaust area black thermal painting

almost brand new
on Camo
Factory Warranty
operated in AOC

IF THE PLANE IS SOLD WITHIN THE EU THE PURCHASE PRICE IS SUBJECT TO 19 % VAT