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DAHER - TBM960
Price on request
Quick Link 11501
| Year | 2026 |
|---|---|
| Aircraft location | Germany |
| Total time, airframe | Factory new |
Factory New DAHER TBM960
Advertiser status
Advertiser status: aircraft dealer/broker
Advertiser's contact information:
Frank Prochaska
Rheinland Air Service GmbH
Flughafenstr. 31
41066 Mönchengladbach
Deutschland
Phone no. +49 (0) 178 2550 246
Engine 1
Manufacturer
Pratt & Whitney
Model/Type
PT6E-66XT
Power output
1844 shp
Propeller 1
Manufacturer
Hartzell
Model/Type
RaptorTM
• 1 GMA 36B audio controller with Bluetooth audio link and integrated marker beacon receiver, intercom and public address capability
• 2 GDU 1250W, 12’’ WUXGA high-resolution Primary Flight Displays (PFDs)
• 1 GDU 1250W, 12” WUXGA high-resolution Multi-Function Display (MFD) with engine, pressurization, electrical, fuel, flaps and trim indications, Crew Alerting System (CAS), checklist capability, aircraft synoptics and navigation mapping system
• 2 GIA 64W, Nav/Com/ILS/WAAS GPS
• 2 GEA 71B, engine and airframe interface unit
• 2 GRS 79, Attitude and Heading Reference System (AHRS)
• 2 GMU 44 triaxial magnetometer
• 2 GDC 72, digital air data computers with dual probe system
• 1 GTX 345 Mode S extended squitter transponder (#1) ADS-B In and Out
• 2 GTC 580 tactile controllers, conveniently located on the reclined section of the panel
• 1 GMC 711 AT autopilot and autothrottle mode controller, located in upper central panel
• 4 GSA 81 torque flight servos (yaw, pitch, pitch trim and roll)
• 1 GSA 87 servo actuator for autothrottle
• 1 GTA 82 adapter for yaw auto trim device
• 1 Garmin 4G LTE/WiFi datalink transmitter, enabling automatic database upload and flight/engine data log uploading
• 1 MD 302 back-up attitude, airspeed, altitude and heading digital display, two-screen instrument with MD32 remote magnetometer
• Airframe de-icing control panel
• Inertial separator control
• Landing gear control panel
• Electric power generator control, with monitoring on the overhead panel
• Dedicated master warning and caution for Crew Alerting System message acknowledgement
• Voice alert system
• Cabin temperature control (dual zone, with override capability)
• Heated stall warning system
• Digital chronometer displayed on GDU
• Digital flight time hourmeter
• Instrument panel lighting; dedicated lighting for the circuit breaker panel
• Six Bose A20 headsets
• Flight data recorder
• 2 GDU 1250W, 12’’ WUXGA high-resolution Primary Flight Displays (PFDs)
• 1 GDU 1250W, 12” WUXGA high-resolution Multi-Function Display (MFD) with engine, pressurization, electrical, fuel, flaps and trim indications, Crew Alerting System (CAS), checklist capability, aircraft synoptics and navigation mapping system
• 2 GIA 64W, Nav/Com/ILS/WAAS GPS
• 2 GEA 71B, engine and airframe interface unit
• 2 GRS 79, Attitude and Heading Reference System (AHRS)
• 2 GMU 44 triaxial magnetometer
• 2 GDC 72, digital air data computers with dual probe system
• 1 GTX 345 Mode S extended squitter transponder (#1) ADS-B In and Out
• 2 GTC 580 tactile controllers, conveniently located on the reclined section of the panel
• 1 GMC 711 AT autopilot and autothrottle mode controller, located in upper central panel
• 4 GSA 81 torque flight servos (yaw, pitch, pitch trim and roll)
• 1 GSA 87 servo actuator for autothrottle
• 1 GTA 82 adapter for yaw auto trim device
• 1 Garmin 4G LTE/WiFi datalink transmitter, enabling automatic database upload and flight/engine data log uploading
• 1 MD 302 back-up attitude, airspeed, altitude and heading digital display, two-screen instrument with MD32 remote magnetometer
• Airframe de-icing control panel
• Inertial separator control
• Landing gear control panel
• Electric power generator control, with monitoring on the overhead panel
• Dedicated master warning and caution for Crew Alerting System message acknowledgement
• Voice alert system
• Cabin temperature control (dual zone, with override capability)
• Heated stall warning system
• Digital chronometer displayed on GDU
• Digital flight time hourmeter
• Instrument panel lighting; dedicated lighting for the circuit breaker panel
• Six Bose A20 headsets
• Flight data recorder
Do it yourself - Select your personal Paint Scheme to fly the most unique TBM ever designed.
With a choice among thousand possibilities, you can turn your aircraft magically visible in the sky and majestically stand out on taxi ways. Strong coating and paint quality are carefully applied to last under extreme weather conditions.
With a choice among thousand possibilities, you can turn your aircraft magically visible in the sky and majestically stand out on taxi ways. Strong coating and paint quality are carefully applied to last under extreme weather conditions.
Do it yourself - Personalize YOUR TBM960! Pick your most favourite leather designs, stitching and colours to create your personal stylish and comforable cabin ambiance.
The Daher TBM 960 give SUV-type flexibility while providing style and comfort. In just a few minutes, the rear seats can be removed and the cabin converted into a four-seat forward-facing configuration with an unrestricted baggage area. The pilot door comes standard and makes boarding easy.
• Seats and cabin design, with improved insulation, convenience side shelf, cupholders, headset holders, stowage area and ambient lighting
• Six heated seats with adjustable backrests, folding armrests and intermediate seats with forward or backward-facing positioning, with multiple installation configuration
• Configurable with four seats and two nets for luggage loading
• Seat side beam polished aluminum finish
• Fully adjustable (3-axis) pilot and co-pilot seats and adjustable rudder pedals
• Individual fresh air vents and finger-touch dimmable reading lights
• Touch screen for cabin climate control
• Pilot and co-pilot sun visors
• Powered headset jacks behind each seat (Bose Lemo plugs) and on the instrument panel
• Baggage compartment with straps and baggage net
• Halon cabin fire extinguisher
• Parking protection kit - Windshield cover
• New environmental control system with engine-driven air conditioning system (VCS)
• Cabin Cupholder in the rear armrest
• Coat Hanger
• Foldable cabin table
The Daher TBM 960 give SUV-type flexibility while providing style and comfort. In just a few minutes, the rear seats can be removed and the cabin converted into a four-seat forward-facing configuration with an unrestricted baggage area. The pilot door comes standard and makes boarding easy.
• Seats and cabin design, with improved insulation, convenience side shelf, cupholders, headset holders, stowage area and ambient lighting
• Six heated seats with adjustable backrests, folding armrests and intermediate seats with forward or backward-facing positioning, with multiple installation configuration
• Configurable with four seats and two nets for luggage loading
• Seat side beam polished aluminum finish
• Fully adjustable (3-axis) pilot and co-pilot seats and adjustable rudder pedals
• Individual fresh air vents and finger-touch dimmable reading lights
• Touch screen for cabin climate control
• Pilot and co-pilot sun visors
• Powered headset jacks behind each seat (Bose Lemo plugs) and on the instrument panel
• Baggage compartment with straps and baggage net
• Halon cabin fire extinguisher
• Parking protection kit - Windshield cover
• New environmental control system with engine-driven air conditioning system (VCS)
• Cabin Cupholder in the rear armrest
• Coat Hanger
• Foldable cabin table
TBM E-Copilot
• ESP / USP - Electronic Stability Protection and Underspeed Protection
• AOA / stall indicator and stick shaker; input from heated probe
• Smooth transition from barometric VNAV to glideslope path
• Surface Watch™ for airport environment awareness
• Automated ice protection system with ice detector
• LVL - Level button to roll level and altitude hold
• EDM - Emergency Descent Mode
• LPV, LNAV/VNAV (including Baro VNAV) approach support and advisory vertical guidance
for LP, LNAV and visual approaches
• HomeSafe™ emergency autoland function
FUEL EQUIPMENT
• Design provision for operation without fuel system icing inhibitor additive
• One structural fuel tank per wing
• Engine-driven fuel pump
• Standby electrical fuel pump and low-pressure switch / indicator
• Fuel tank selector with automatic fuel tank sequencer unit
• Capacitive fuel gauges with low fuel level warning system
ICING PROTECTION
• Pneumatically deiced wing and tail sections
• Heated engine air intake lip
• Pilot controlled engine inertial separator
• Electrically heated propeller blades
• Electrically heated pitot tubes
• Electrically deiced stall warning sensor
• Electrically heated windshields: pilot and copilot / ice detector light
ELECTRICAL EQUIPMENT
• Automatic starter generator transition during start
• Lead acid battery: 24v 42 ah
• Starter generator: 28v 300 amp
• Standby generator: 28v 100 amp
• Electrical power control
• Circuit breakers
• LED anti-collision strobe lights for ground-based operations (winglets and tail)
• Navigation lights
• LED taxi and landing lights
• LED ice detection light
• Ground power plug
• Energy saver for ATC clearance while on ground
• Tri-band ELT with GPS connection
• One high-power USB-A charging port and five dual high-power USB-A/USB-C charging ports, plus 115V universal port
• ESP / USP - Electronic Stability Protection and Underspeed Protection
• AOA / stall indicator and stick shaker; input from heated probe
• Smooth transition from barometric VNAV to glideslope path
• Surface Watch™ for airport environment awareness
• Automated ice protection system with ice detector
• LVL - Level button to roll level and altitude hold
• EDM - Emergency Descent Mode
• LPV, LNAV/VNAV (including Baro VNAV) approach support and advisory vertical guidance
for LP, LNAV and visual approaches
• HomeSafe™ emergency autoland function
FUEL EQUIPMENT
• Design provision for operation without fuel system icing inhibitor additive
• One structural fuel tank per wing
• Engine-driven fuel pump
• Standby electrical fuel pump and low-pressure switch / indicator
• Fuel tank selector with automatic fuel tank sequencer unit
• Capacitive fuel gauges with low fuel level warning system
ICING PROTECTION
• Pneumatically deiced wing and tail sections
• Heated engine air intake lip
• Pilot controlled engine inertial separator
• Electrically heated propeller blades
• Electrically heated pitot tubes
• Electrically deiced stall warning sensor
• Electrically heated windshields: pilot and copilot / ice detector light
ELECTRICAL EQUIPMENT
• Automatic starter generator transition during start
• Lead acid battery: 24v 42 ah
• Starter generator: 28v 300 amp
• Standby generator: 28v 100 amp
• Electrical power control
• Circuit breakers
• LED anti-collision strobe lights for ground-based operations (winglets and tail)
• Navigation lights
• LED taxi and landing lights
• LED ice detection light
• Ground power plug
• Energy saver for ATC clearance while on ground
• Tri-band ELT with GPS connection
• One high-power USB-A charging port and five dual high-power USB-A/USB-C charging ports, plus 115V universal port
Factory New Aircraft
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