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Airbus Helicopter H 130 - with certified Autopilot - like new- |
[卖出]
€ 3.630.000 |
概观
| 概况 | | 类型: | 直升机 (涡轮机) | | 品牌: | Airbus | | 型号 1: | Helicopter H 130 - with certified Autopilot - like new- | | 制造年: | 2016 | | 注册号: | D-reg | | 属性: | 始终（一直）停留在机库
商用注册的
EU-OPS 1 注册的 | | 地点: | 德国, M黱chen, EDDM | | 时间总计: | 100 h | | 价格: | € 3.630.000
(~ US$ 3.861.594)[卖出] | | 净价: | US$ 3.244.590
€ 3.050.000 | | 欧盟增值税: | 是的 | | 增值税规定: | 对 (19%) | | 细节 |
| 销售者 |
Carlos de Pilar Flugzeughandel
www.carlos-de-pilar.de
Postfach 1529
82157 Gr鋐elfing
德国
电话: +49 89 8542303
传真: [+49] - (0)89 - 853176 |
| 联系销售者 |
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细节
| 概况 | | 类型: | 直升机 (涡轮机) | | 品牌: | Airbus | | 型号 1: | Helicopter H 130 - with certified Autopilot - like new- | | 制造年: | 2016 | | 注册号: | D-reg | | 属性: | 始终（一直）停留在机库
商用注册的
EU-OPS 1 注册的 | | 地点: | 德国, M黱chen, EDDM | | 时间总计: | 100 h | | 价格: | € 3.630.000
(~ US$ 3.861.594)[卖出] | | 净价: | US$ 3.244.590
€ 3.050.000 | | 欧盟增值税: | 是的 | | 增值税规定: | 对 (19%) | | 乘客数量: | 1+4 |
| 航空电子学 |  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
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| 装备 |  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 |
| 外部 | 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 |
| Inspection Status | almost brand new
on Camo
Factory Warranty
operated in AOC |
| 其他 | | IF THE PLANE IS SOLD WITHIN THE EU THE PURCHASE PRICE IS SUBJECT TO 19 % VAT |
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