HIGHLIGHTS
– FAA & EASA Certified
– Single/Dual Pilot IFR
– Air Conditioning
– Inlet Barrier Filter
– Fixed provisions for External Hoist, Snow skid, Emergency Floats & Wire strike
– EMS provisions
– Warranty: Aircraft: 2 years or 1000 hours / Engines: 3 years or 2000 hours
manufacturer
Airbus
model
H145
configuration
Corporate
condition
Used
year
2024
time
10
helicopter location
Canada
serial number
21136
listing ID
HT24496
Description
avionics
BASIC INSTRUMENTATION
Flight Display Subsystem (FDS) composed of 2 smart multifunction displays (6 x 8 inch) providing the following functions:
• Flight Navigation Display (FND) format (incl. PFD, FLI, Master list, NAV, RPM, mast moment & fuel indication
• Vehicle Monitoring System (VMS) format (incl. engine, gearbox, hydraulic, fuel, electrical system, RPM and clock indication)
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)
Stand-by instruments:
• Integrated Electronic Standby Instrument (IESI)
• Stand-by compass
• Usage Monitoring System (UMS)
• Flight Data Continuous Recorder (FDCR)
• “One hundred feet“ alert
• Directional Gyro Free Steering Mode
Warning unit:
• Engine fire warning with fuel emergency shut-off
• Warning lights
• Fire extinguishing system warning
• Cockpit Control Panel (CCP) for FDS
• Wireless Airborne Communication Server (wACS)
Engine switch panel:
• Digital engine control (FADEC)
• Radar altimeter
AVIONICS LAYOUT
• Single / Dual Pilot IFR with Dual GTN 750Xi
• Digital Voice Control System (DVCS 6500) incl. AMU6510 (Becker), pilot + copilot
• Transponder Lynx NGT9000R+ (ACSS)- Incl. ADS-B out, ADS-B in, TCAS I.
• Distance Measuring Equipment (DME) DME-4000 (Rockwell Collins)
• Marker beacon receiver MKR3300-1 (Becker)
• GPS/NAV/COM GTN 750Xi (Garmin), copilot
• GPS/NAV/COM GTN 750Xi (Garmin), pilot
• Wireless connectivity Flight Stream 510 (Garmin) 0.0 0.0
• Flight Display Subsystem (FDS), copilot 5.0 11.0
• Avionics Package SP/DP IFR GTN Series interconnection / wiring
• TCAS (Avidyne TAS620A)
Flight Display Subsystem (FDS) composed of 2 smart multifunction displays (6 x 8 inch) providing the following functions:
• Flight Navigation Display (FND) format (incl. PFD, FLI, Master list, NAV, RPM, mast moment & fuel indication
• Vehicle Monitoring System (VMS) format (incl. engine, gearbox, hydraulic, fuel, electrical system, RPM and clock indication)
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)
Stand-by instruments:
• Integrated Electronic Standby Instrument (IESI)
• Stand-by compass
• Usage Monitoring System (UMS)
• Flight Data Continuous Recorder (FDCR)
• “One hundred feet“ alert
• Directional Gyro Free Steering Mode
Warning unit:
• Engine fire warning with fuel emergency shut-off
• Warning lights
• Fire extinguishing system warning
• Cockpit Control Panel (CCP) for FDS
• Wireless Airborne Communication Server (wACS)
Engine switch panel:
• Digital engine control (FADEC)
• Radar altimeter
AVIONICS LAYOUT
• Single / Dual Pilot IFR with Dual GTN 750Xi
• Digital Voice Control System (DVCS 6500) incl. AMU6510 (Becker), pilot + copilot
• Transponder Lynx NGT9000R+ (ACSS)- Incl. ADS-B out, ADS-B in, TCAS I.
• Distance Measuring Equipment (DME) DME-4000 (Rockwell Collins)
• Marker beacon receiver MKR3300-1 (Becker)
• GPS/NAV/COM GTN 750Xi (Garmin), copilot
• GPS/NAV/COM GTN 750Xi (Garmin), pilot
• Wireless connectivity Flight Stream 510 (Garmin) 0.0 0.0
• Flight Display Subsystem (FDS), copilot 5.0 11.0
• Avionics Package SP/DP IFR GTN Series interconnection / wiring
• TCAS (Avidyne TAS620A)
equipment
OPTIONAL EQUIPMENT
• Air conditioning System
• IBF- Inlet Barrier Filter
• External Hoist – Fixed provision
• Snow skid – Fixed provision
• Emergency Floats – fixed provision with landing gear extension
• Wire strike – fixed provision
• Smoked Windows
• Sun Visors
• Clamshell doors windows (left/right)
• Strobe – anticollision light
• Jettison-type cabin door
• Slide door loc (both sides)
• LARS Camera
• Rear camera (tail boom)
• Search-landing light
• Tablet Holder – USB 5VDC (co-pilot)
• Fuel flow meter
• Reinforced clamshell doors hinges
• 44 AH Battery
• Bleed air improvement kit
• 3rd Audio panel in the cabin
• Additional maintenance handle
HEMS FIXED PROVISION
• Multipurpose hardpoints
• Multipurpose fittings
• EMS ceiling rails
• Sealed cabin floor
• Air conditioning System
• IBF- Inlet Barrier Filter
• External Hoist – Fixed provision
• Snow skid – Fixed provision
• Emergency Floats – fixed provision with landing gear extension
• Wire strike – fixed provision
• Smoked Windows
• Sun Visors
• Clamshell doors windows (left/right)
• Strobe – anticollision light
• Jettison-type cabin door
• Slide door loc (both sides)
• LARS Camera
• Rear camera (tail boom)
• Search-landing light
• Tablet Holder – USB 5VDC (co-pilot)
• Fuel flow meter
• Reinforced clamshell doors hinges
• 44 AH Battery
• Bleed air improvement kit
• 3rd Audio panel in the cabin
• Additional maintenance handle
HEMS FIXED PROVISION
• Multipurpose hardpoints
• Multipurpose fittings
• EMS ceiling rails
• Sealed cabin floor
interior
INTERIOR CONFIGURATION
• 8 PAX
• EMS Provisions
• 8 PAX
• EMS Provisions
engine 1
SAFRAN Arriel 2E
Engine #1
S/N: 61286
TSN: 10
Engine #1
S/N: 61286
TSN: 10
engine 2
SAFRAN Arriel 2E
S/N: 61287
TSN: 10
S/N: 61287
TSN: 10




