2008 EUROCOPTER EC145
Starts from the median asking price of 22 comparable EUROCOPTER Helicopter listings ($1,086,287), then adjusts for:
- Year +1 vs comparable listings +1.5%
- Airframe time -3,449 hr vs comps +6.9%
- Modern GPS navigator (uncommon in comps) +3.0%
- Autopilot (uncommon in comps) +2.0%
Shown as a range. An estimate from asking-price comparables and FAA supply data — not an appraisal.
Overview
| Make / Model | EUROCOPTER EC145 |
|---|---|
| Type | Helicopter |
| Airframe time | 1,186 hrs |
| Avionics / GPS | Garmin GNS 430 |
| Avionics / Transponder | Garmin GTX330 |
| Airworthy | Yes |
Description
Low Hours • One Owner since new • Corporate configuration 10 seats • Airbus Center Maintained • Flat Passenger Cabin Floor • Single/Dual Pilot IFR • Pilot/Copilot Instruments • Airbus AFCS Autopilot • Air Conditioning • Bleed Air Heater • Premium Leather Interior • Wire Strike Protection • NVG Compatible/ Capable Cockpit • Two Passenger Sliding Doors • 400W Landing & Searchlight • Thales MEGHAS/ FCDS Glass Cockpit • Honeywell KRA 405B Radar Altimeter • Ryan TCAD9900BX Traffic Alert System • 2 x Garmin GNS 430 GPS/Nav/Com • Dual Controls
Modifications
Dual Controls Air Conditioning Bleed Air Heating System VEMD (Vehicle & Engine Multifunction Display) NVG-Compatible Warning Unit NVG-Compatible CAD (Crew Alerting Display) 7-inch Copilot Instrument Panel with Glare Shield Avionics compartment ventilation system Long Boarding Steps Built-in Maintenance Steps & Grips Wire Strike Protection System Two Passenger Sliding Doors Two Rear Hinged Clamshell Doors One Windshield Wiper 400W Landing & Search Light Two Fire Extinguishers Strobe Lights Tail Position Light Navigation Lights Magnetic Compass Standby Horizon Standby Altimeter Standby Airspeed Triple (rotor and engines) RPM Indicator Dual Hydraulic Boost System for Cyclic/Collective Single Hydraulic Boost System for Yaw Stability Augmentation System (SAS) for Tail Rotor High Visibility Paint Main & Tail Rotor Blades Clock
Avionics
Single/Dual Pilot IFR Airbus Avionics Solution B1 Thales MEGHAS/ FCDS Glass Cockpit NVG Compatible/Capable Cockpit 2 x SMD 45 Pilot & Copilot Primary Flight Displays (PFDs) 2 x SMD 45 Pilot & Copilot Navigation Displays (NDs) Central Panel Display System (CPDS) Honeywell KR 21 Marker Beacon Receiver and Indicator Lights 2 x Garmin GNS 430 GPS/Nav/Com Garmin GTX 330 Mode S Transponder 2 x Becker ACU 6100 Pilot & Copilot Audio/Comm Control Units Becker IC 3100 Intercom Amplifier Airbus Automatic Flight Control System (AFCS) - Autopilot 2 x APM 2001 Autopilot Modules (Duplex System) APMS 2360 Automatic Pilot System 2 x MEGHAS Instrument Control Panels (ICPs) MEGHAS Reconfiguration Unit Honeywell KRA 405B Radar Altimeter Ryan TCAD 9900BX Traffic Alert System ACR Artex C406-N HM ELT
How this aircraft compares
Where this EUROCOPTER EC145 lands versus other EUROCOPTER EC145 listings on fyiAero.
Airframe time
20th pct1,186 hours total (TTAF) · 20th percentile of 5 listings
Percentile = share of comparable listings at or below this value. Lower airframe/engine hours are generally fresher; price reflects the asking price only.
General
| Year | 2008 |
|---|---|
| Manufacturer | EUROCOPTER |
| Model | EC145 |
| Serial Number | 9198 |
| Condition | Used |
Airframe
| Total Time | 1,186 |
|---|---|
| Complete Logs | Yes |
Avionics
| Artificial Horizon | Yes |
|---|---|
| Radar Altimeter | Yes |
| Single Pilot Operation | Yes |
| Auto Pilot | Yes |
| ELT | Yes |
| Traffic Avoidance System | Yes |
| Wire Strike Protection System | Yes |
| Avionics/Radios | Single/Dual Pilot IFR Airbus Avionics Solution B1 Thales MEGHAS/ FCDS Glass Cockpit NVG Compatible/Capable Cockpit 2 x SMD 45 Pilot & Copilot Primary Flight Displays (PFDs) 2 x SMD 45 Pilot & Copilot Navigation Displays (NDs) Central Panel Display System (CPDS) Honeywell KR 21 Marker Beacon Receiver and Indicator Lights 2 x Garmin GNS 430 GPS/Nav/Com Garmin GTX 330 Mode S Transponder 2 x Becker ACU 6100 Pilot & Copilot Audio/Comm Control Units Becker IC 3100 Intercom Amplifier Airbus Automatic Flight Control System (AFCS) - Autopilot 2 x APM 2001 Autopilot Modules (Duplex System) APMS 2360 Automatic Pilot System 2 x MEGHAS Instrument Control Panels (ICPs) MEGHAS Reconfiguration Unit Honeywell KRA 405B Radar Altimeter Ryan TCAD 9900BX Traffic Alert System ACR Artex C406-N HM ELT |
Additional Equipment
| Dual Controls | Yes |
|---|---|
| A/C | Yes |
| Heater | Yes |
| Baggage Compartment | Yes |
| Additional Equipment | Dual Controls Air Conditioning Bleed Air Heating System VEMD (Vehicle & Engine Multifunction Display) NVG-Compatible Warning Unit NVG-Compatible CAD (Crew Alerting Display) 7-inch Copilot Instrument Panel with Glare Shield Avionics compartment ventilation system Long Boarding Steps Built-in Maintenance Steps & Grips Wire Strike Protection System Two Passenger Sliding Doors Two Rear Hinged Clamshell Doors One Windshield Wiper 400W Landing & Search Light Two Fire Extinguishers Strobe Lights Tail Position Light Navigation Lights Magnetic Compass Standby Horizon Standby Altimeter Standby Airspeed Triple (rotor and engines) RPM Indicator Dual Hydraulic Boost System for Cyclic/Collective Single Hydraulic Boost System for Yaw Stability Augmentation System (SAS) for Tail Rotor High Visibility Paint Main & Tail Rotor Blades Clock |
Interior
| Configuration | Corporate |
|---|---|
| Number of Seats | 10 |
| Soundproofing | Yes |
Inspection Status
| Inspection Status | All manufacturer's ADs and mandatory SBs up to date and maintained at Airbus Service Center. |
|---|---|
| Airworthy | Yes |
Rotor
| Main Rotor Blade Time Remaining | 23813 |
|---|---|
| Main Rotor Gearbox Time Remaining | 4213 |
| Anti-Torque System | Tail Rotor |
| Tail Rotor Blade Time Remaining | 8113 |
| Tail Rotor Gearbox Time Remaining | 1617 |