Description
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 hoursSpecifications
Year2024
ManufacturerAIRBUS
ModelH145D3
Serial Number21136
ConditionUsed
Total Time10
Engine 1 NotesSafran Arriel 2E
S/N: 61286
TSN: 10
Engine 2 NotesSafran Arriel 2E
S/N: 61287
TSN: 10
Avionics/RadiosBASIC 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)
Additional EquipmentOPTIONAL 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
Interior NotesINTERIOR CONFIGURATION
• 8 PAX
• EMS Provisions
Year2024|
ManufacturerAIRBUS|
ModelH145D3|
Serial Number21136|
ConditionUsed|
Total Time10|
Engine 1 NotesSafran Arriel 2E
S/N: 61286
TSN: 10|
Engine 2 NotesSafran Arriel 2E
S/N: 61287
TSN: 10|
Avionics/RadiosBASIC 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)|
Additional EquipmentOPTIONAL 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|
Interior NotesINTERIOR CONFIGURATION
• 8 PAX
• EMS Provisions|
