2024 Airbus H145D3Turbine Helicopter • Toronto, Ontario, Canada

This 2024 Airbus H145D3, serial number 21136, is a nearly new, low-time helicopter presented with only 10 total hours on both its airframe and its twin Safran Arriel 2E engines (S/N 61286 & 61287). It is certified for both FAA and EASA operations and is equipped for demanding single or dual-pilot IFR missions, with a primary configuration supporting 8 passengers and including fixed provisions for EMS (Emergency Medical Service) applications. The aircraft benefits from a comprehensive factory warranty covering the airframe for 2 years or 1000 hours and the engines for 3 years or 2000 hours.

The avionics suite is centered on a dual Garmin GTN...

Year: 2024

Make: Airbus

Series: H145

Model: H145D3

Serial #: 21136

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Specifications

Category: Turbine Helicopter

Intended Use: Emergency Medical Services, Passenger, Search and Rescue, Sightseeing, Utility

Flight Rules: IFR

Seats: 8

Hours, Logs & Inspections

Total Time: 10 hrs

Engine 1 Time: 10 hrs (TSN)

Engine 2 Time: 10 hrs (TSN)

Avionics

GPS

Garmin GTN 750Xi - GPS/NAV/COM GTN GPS/NAV/COM GTN

Comms

Garmin GTN 750Xi - GPS/NAV/COM GTN GPS/NAV/COM GTN (DME) Marker Beacon

Autopilot

Single/Dual Pilot IFR with Dual GTN 750Xi

Audio

Becker DVCS 6500 - Digital Voice Control System (DVCS incl. Pilot Copilot; 3rd Audio Panel in the Cabin

Traffic

ACSS Lynx NGT9000R+ - Transponder (ACSS) Incl. ADS-B out, ADS-B in, TCAS TCAS

ADS-B Out

ACSS Lynx NGT9000R+ - Transponder (ACSS) Incl. ADS-B out

ADS-B In

ACSS Lynx NGT9000R+ - Transponder (ACSS) Incl. ADS-B in

PFD

Flight Display Subsystem (FDS) composed of 2 smart multifunction displays (6 x 8 inch) providing Flight Navigation Display (FND) format (incl. PFD, FLI, Master list, NAV, RPM, mast moment & fuel indication)

MFD

Flight Display Subsystem (FDS) composed of 2 smart multifunction displays (6 x 8 inch) providing Vehicle Monitoring System (VMS) format (incl. engine, gearbox, hydraulic, fuel, electrical system, RPM and clock indication)

EMS/EIS

Vehicle Monitoring System (VMS) format; Vehicle Management System (VMS) including: 2 duplex Aircraft Management Computer (AMC); Reference sensors: 3 Attitude and Heading Reference Systems (AHRS), 2 Air Data sensors (electrically heated pitot tube and static port), 2 Three Axis Magnetometers (TAM); Usage Monitoring System (UMS); Flight Data Continuous Recorder (FDCR); Fuel flow meter