RECHERCHE
MON COMPTE
Details de l'annonce
INFORMATIONS VENDEUR :
REFERENCE
EA2010072186
TYPE
CONSTRUCTEUR
MODELE
VERSION
NUMERO DE SERIE
NUMERO D'ENREGISTREMENT
ANNEE
2008
TTAF
100
ANNEE INTERIEUR
NOMBRE DE PLACES
2+8
PAYS
PRIX
DESCRIPTION
Eurocopter EC 145
The EC145 combines Eurocopter’s latest technical developments. The EC145’s hingeless rotor system with its monolithic titanium hub is fully proven. In addition to environmental and economical aspects, the rotor system together with high time between overhaul (TBO) gearbox and airframe components allow for low maintenance costs, in addition to high in-service time of the helicopter due to the low level of scheduled maintenance required.
The EC145 is equipped with two powerful and reliable Turbomeca Arriel 1E2 engines which, in combination with its lifting system, provide outstanding performance and vital power reserves even in one-engine-inoperative scenarios. Twin-engine reliability is complemented by a fully separated fuel system, a tandem hydraulic system, dual electrical system and redundant lubrication for the main transmission. Further positive safety aspects of the EC145 are design elements like energy absorbing fuselage and seats, as well as crash-resis
The EC145 combines Eurocopter’s latest technical developments. The EC145’s hingeless rotor system with its monolithic titanium hub is fully proven. In addition to environmental and economical aspects, the rotor system together with high time between overhaul (TBO) gearbox and airframe components allow for low maintenance costs, in addition to high in-service time of the helicopter due to the low level of scheduled maintenance required.
The EC145 is equipped with two powerful and reliable Turbomeca Arriel 1E2 engines which, in combination with its lifting system, provide outstanding performance and vital power reserves even in one-engine-inoperative scenarios. Twin-engine reliability is complemented by a fully separated fuel system, a tandem hydraulic system, dual electrical system and redundant lubrication for the main transmission. Further positive safety aspects of the EC145 are design elements like energy absorbing fuselage and seats, as well as crash-resis
AVIONICS
* GARMIN GNS 430 (Avionics Solution B1 Package):
* MEGHAS FCDS Dual (4x SMD45)
* GPS/NAV/COM system GNS 430, pilot/copilot (2nd
* system VOR/ILS)
* Audio/Comm control system (pilot & co-pilot)
* IC amplifier IC 3100 -4-01 (Becker)
* Marker beacon receiver/lights KR 21 (Honeywell)
* Distance Measuring Equip. DMS-44A (Chelton/
* Wulfsberg)
* Transponder (mode S) GTX 330 (Garmin)
* Avionics solution B1 interconnection wiring
* HF Communication System KHF990
* Cabin Loud Speaker
* Radar altimeter KRA 405B (Honeywell)
* AFCS
* Usage Monitoring System (UMS)
* CVFDR
* AHRS (Free Steering Mode)
* ADF System DFS 43A (Chelton/Wulfsberg)
* ADF Control Unit CD 432B (Chelton/Wulfsberg)
* SAR Weather Radar RDR 1600 + Radar Radome
* Video Radar Unit
* 7” Co-pilot instrument Panel with Glareshield
* MEGHAS Sensor Kit
* 10 x Headsets (DAVID CLARK)
* MEGHAS FCDS Dual (4x SMD45)
* GPS/NAV/COM system GNS 430, pilot/copilot (2nd
* system VOR/ILS)
* Audio/Comm control system (pilot & co-pilot)
* IC amplifier IC 3100 -4-01 (Becker)
* Marker beacon receiver/lights KR 21 (Honeywell)
* Distance Measuring Equip. DMS-44A (Chelton/
* Wulfsberg)
* Transponder (mode S) GTX 330 (Garmin)
* Avionics solution B1 interconnection wiring
* HF Communication System KHF990
* Cabin Loud Speaker
* Radar altimeter KRA 405B (Honeywell)
* AFCS
* Usage Monitoring System (UMS)
* CVFDR
* AHRS (Free Steering Mode)
* ADF System DFS 43A (Chelton/Wulfsberg)
* ADF Control Unit CD 432B (Chelton/Wulfsberg)
* SAR Weather Radar RDR 1600 + Radar Radome
* Video Radar Unit
* 7” Co-pilot instrument Panel with Glareshield
* MEGHAS Sensor Kit
* 10 x Headsets (DAVID CLARK)
INTERIEUR
EXTERIEUR
PERFORMANCES
* Eurocopter Warranty 1000 hours // 2 years
* We offer the Aircraft: “As is” Ex-Works Asia Pacific
* We offer the Aircraft: “As is” Ex-Works Asia Pacific
SPECIFICATIONS
MTOW: 3,585 kg
MAX RANGE WITH STANDARD FUEL TANK:713 km
STANDARD CONFIGURATION:1/2+9 pax
PRODUCTION YEAR:2008
TSN:100 hours
MISSION:CORPORATE / OFFSHORE
AVAILABILITY:IMMEDIATE
MAX RANGE WITH STANDARD FUEL TANK:713 km
STANDARD CONFIGURATION:1/2+9 pax
PRODUCTION YEAR:2008
TSN:100 hours
MISSION:CORPORATE / OFFSHORE
AVAILABILITY:IMMEDIATE
EQUIPEMENT ADDITIONNEL
* Air Conditioning System
* Additional electrical unit interface (mission equipment)
* Battery type ?Saft? ULM, 40Ah, 24V
* AC system
* Tinted sun shades (cockpit windshield roof section)
* Illuminated Chart Holder for Pilot Side
* Additional Circuit Breaker Panel
* Additional Electrical Unit for 400/200W light
* Push Out Cabin Windows
* Copilot flight controls
* Engine compressor washing device & Fuzz Burner
* Helicopter Emergency Egress Lighting (HEEL)
* Emergency Floats, FP & RP
* Underwater Locator Beacon (ULB)
* Voice Alert Generator (NAT)
* ELT C406-N HM (Artex)
* IBF Sand Filler Kit
* Auxiliary Fuel Tank FP & RP
* Fuel Management System
* SPIFR Kit
* FCDS
* Rotor Brake
* Basic Sound Proofing Kit
* Comfort Improvement Kit
* Height adjustable pilot & co-pilot seats
* Leather upholstery (all seats)
* Variable Tie-Down Net
* Landing & search
* Additional electrical unit interface (mission equipment)
* Battery type ?Saft? ULM, 40Ah, 24V
* AC system
* Tinted sun shades (cockpit windshield roof section)
* Illuminated Chart Holder for Pilot Side
* Additional Circuit Breaker Panel
* Additional Electrical Unit for 400/200W light
* Push Out Cabin Windows
* Copilot flight controls
* Engine compressor washing device & Fuzz Burner
* Helicopter Emergency Egress Lighting (HEEL)
* Emergency Floats, FP & RP
* Underwater Locator Beacon (ULB)
* Voice Alert Generator (NAT)
* ELT C406-N HM (Artex)
* IBF Sand Filler Kit
* Auxiliary Fuel Tank FP & RP
* Fuel Management System
* SPIFR Kit
* FCDS
* Rotor Brake
* Basic Sound Proofing Kit
* Comfort Improvement Kit
* Height adjustable pilot & co-pilot seats
* Leather upholstery (all seats)
* Variable Tie-Down Net
* Landing & search
PUBLICITE
