New 2024 TBM 960 - The TBM 960 offers the latest cockpit technology with the Garmin G3000 avionics suite controlled by the new GTC 580 touchscreen controllers. The TBM 960 features enhancements over the 930 like Auto Throttle, Automatic Ice Detection and activation, new interior design, and Ground Suppression Garmin Radar. The TBM 960 has a maximum cruise speed of 330 knots and 1,730 nautical mile range.

Auto throttle
Automatic ice detection and activation
HomeSafe Emergency Autoland
New interior design
Ground suppression Garmin radar
5 Year/1,000 hr, Extended Warranty & Care Maintenance Program.
330-knot cruise
31,000-ft. reached in 18 minutes, 45 seconds

Airframe:
Total Time: 0

Engines:
PRATT & WHITNEY PT6A-66D
Time: 0 SNEW
TBO: 3500

Garmin G3000 Avionics System
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 PFD Primary Flight Displays
1 GDU 1250W, 12" WUXGA high resolution MFD Multi-Function Display with engine, pressurization, electrical, fuel, flaps and trims indication, 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 72B digital air-data computers w/ dual probe system
2 GTX 345 Mode S Extended Squitter transponder (#1) ADS-B In & 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
MD302 Back up Attitude, Airspeed, Altitude and heading digital display, 2 screens instrument with MD32 remote magnetometer
LPV, LNAV/VNAV (including Baro VNAV) approaches support and advisory vertical guidance for LP, LNAV and Visual approaches
ESP Electronic Stability and underspeed Protection
AOA/stall indicator and Stick shaker based on heated probe
Smooth transition from barometric VNAV to Glideslope/path
Surface Watch for airport environment awareness
Auto-Ice protection system with ice detection sensor
LVL Level button to roll level and hold altitude
EDM Emergency Descent Mode
1 Flightstream FS510 Bluetooth/Wifi allowing Tablet to Avionics secured exchange information channel
Airframe de-icing control panel
Inertial separator control
Landing gear control panel
Electric generation controls and monitoring on overhead panel
Dedicated master warning and caution for Crew Alerting System message acknowledgement
Voice Alert System
Cabin temperature control (dual zone, with over ride capability)
Heated stall warning system
Digital chronometer displayed on GDU
Digital Flight time hourmeter
Instrument panel lighting, CB dedicated switch lighting
6 Bose Headsets
Flight Data Recorder
RVSM Package
Garmin GTS 820 Traffic Advisory System
WX 500 Stormscope
Garmin GWX 70 Four Color Radar with with Turbulence detection and Ground Suppression
Garmin GDL69 XM Data link weather and XM music
Jeppesen Chart View
Synthetic Vision
GSR56 Integrated Data Link Sat Phone for Text and Talk
HomeSafe Emergency Autoland

Premium edition fittings included
6 leather heated seats with adjustable backrests, folding armrests and intermediate seats with forward or backward accommodation with multiple installation configuration
Side beam seat Polished Aluminum finish
Fully adjustable (3-axis) pilot and co-pilot seats and adjustable rudder pedals
Cabin accommodation capable of 4 seats layout includes 2 nets for luggage load
Leather upper cabin side panels, leather covered lower cabin side panels, wool carpeting
Individual fresh-air vents and reading lights
Pilot and co-pilot sun visors
Ship-powered headset jacks for each seat (Bose Lemo plugs) and on instrument panel
Baggage compartment with straps and baggage net
Halon cabin fire extinguisher
Parking protection kit Windshield cover
Environment system with engine driven air-conditioning system (VCS)
Cockpit and Cabin Cupholders
Coat Hanger
Cabin foldable tablet

Metal structure and skin panelling
Carbon fiber engine cowling and winglets
Anti-corrosion protection treatment
Retractable gear with electrohydraulic actuation
Hydraulic disc brakes
Pressurized 6 seats cabin (6.2 psi) and baggage compartment
Sound proofing and thermal insulation
Pilot Access Door
Large access door with retractable stairway
Emergency exit
Front storage compartment (not pressurized) with lockable access door
Easy maintenance access doors
Wing Tie-down attachments
Jacking points
Gaseous oxygen system for 6 seats and quick donning masks with Smart Mike for pilot & copilot
Engine
PT6 A66D Pratt & Whitney Canada turboprop engine developing 1825 SHP thermodynamic, flat rated at 850 SHP propeller with overspeed limiter, full feathering and reverse
Oil cooler
Anti-icing air inlet with inertial separator without operational limitation
Dual polished exhaust system aerodynamically optimized
Service access doors in cowlings
Dual engine Chip detector indication on flight display
Flight Data Acquisition Storage and Transmission System (FAST)
Propeller
Full composite electrically de-iced five bladed Hartzell constant speed
Polished aluminum spinner cone
Controls
Dual flight controls, leather covered. Control wheel with 8 integrated functions, (Push to talk, Autopilot, CWS (control wheel stering), electric pitch and yaw trim, Transponder ident, Comm 2 frequency Changer , Stormscope, Timer)
Elevator, rudder and aileron electric trim
Electrical pre-select flaps with integrated asymmetry detection system
Central console including: Single lever power control featuring autothrottle associated with engine smart single gauge, with bleed inhibition in low idle condition electric flap control, fuel selector, manual pitch trim, ailerons electric trim manuel override control
Adjustable rudder pedals
Landing gear handle
Dual toe brakes Parking brake
Landing gear emergency extension handle
Automatic environment and pressurization control system with max diff mode
Alternate static source control
Alternate ram air source control
Fuel equipment
One structural fuel tank per wing
Engine driven fuel pump
Standby electrical fuel pump and low pressure switch/ indication
Fuel tank selector with automatic fuel tank sequencer unit
Capacitive fuel gauges with low fuel level warning system
Ice protection
Pneumatically deiced wing and tail unit
Heated engine air intake lip
Pilot controlled engine inertial separator
Electrically heated propeller blades
Electrically heated pitot tubes
Electrically deiced stall warning sensor
Pilot & Co-pilot electrically heated windshields Ice detector light
Electrical equipment
Automatic starter generator transition during start
Lead acid battery 24V 42 A.h
Starter generator 28V 300 Amp
Standby generator 28 V 100 Amp
Electrical power control center
Circuit breakers
Anticollision strobe lights Led Beacon on ground (Winglets & tail)
Navigation lights Taxiing and landing LED lights
LED ice detection light
Ground power plug Ground clearance energy saver
Tri-band ELT with GPS connection
14 V port in passenger cabin + 7 high-power USB charging ports +115V universal port