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2017 Daher TBM 930

Serial: 1189

About this Daher TBM 930 Specs

  • PriceCall for Price
  • Reg No.N930FY
  • Serial1189
  • Airframe545
  • Engines545

This nearly new TBM 930 offers the Garmin G3000 Integrated Avionics Suite, Warranty and Mx thru 9/2022, 545 Hours Total Time, Pilot Door, Winglets, 1730 Nautical Mile Range and Fully Automatic Pressurization System.

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Highlights

Engines

PT6 A66D Pratt & Whitney Engine turboprop engine developing
1825 SHP thermodynamic, flat rated at 850 SHP.

Interior

Elite configurable Interior. Socata TBM Black Diamond Edition
with Black Onyx Leather seats, Flat Black Metal Vents and Lights
with Carbon Fiber Table and upper Accent package. Six genuine
leather seats with adjustable backrests and folding arm rests.
Leather upper cabin side panels in Polynesian Pearl, leather
covered lower cabin side panels in River Stone.

Exterior

Socata White upper fuselage and wings, Estangnous Silver
lower fuselage, Monaco Blue and Canabas Silver striping.

Additional features

• RVSM Data Package
• GTX 33 Mode S Transponder (#2) with Extended Squitter
• GRA 55 Radar Altimeter Displayed on PFD’s
• TAWS-B, Class B TAWS Worldwide Database
• GTS 820 Traffic Advisory System (TAS) Displayed on MFD
and PFD Inset Map
• KN 63 DME Displayed on PFD’s
• Electric Pitch and Rudder Trims on Co-pilot Control Wheel
• Co-pilot Side Map Light and Approach plate Holder
• WX 500 Stormscope Displayable on all Screens
• GWX70 Digital Four Color Weather Radar – 10”

Avionics

  • Garmin G3000 Avionics System
  • 1 GMA 36 Audio controller with integrated marker beacon receiver, intercom and public address capability
  • 2 Bose Headsets
  • 2 GDU 1200W, 12’’ PFD displays Primary Flight displays
  • 1 GDU 1200W, 12” MFD Multi-Function Display with engine, pressurization, electrical, fuel, flaps and trims indication, Crew Alerting System (CAS), aircraft synoptics and navigation mapping system.
  • 2 GIA 63W Nav/Com/ILS/WAAS GPS
  • 2 GEA 71 Engine and airframe interface unit
  • 2 GRS 77 Attitude and Heading Reference System (AHRS)
  • 2 GMU 44 triaxial magnetometer
  • 2 GDC 74B digital air-data computers w/ dual probe system
  • 1 GTX345 (ADS-B) Mode S Extended Squitter transponder (#1)
  • 2 GTC580 Tactile Controllers conveniently located on the reclined section of the panel
  • 1 GMC 710 autopilot mode controller located in upper central panel
  • 4 GSA 81 torque flight servos (yaw, pitch, pitch trim and roll)
  • 1 GTA 82 adapter for yaw auto trim device
  • 1 MD302 Back up Attitude, Airspeed, Altitude digital display 2 screens instrument
  • AOA Angle of Attack Sensor, Computer, and integrated display in PFD.
  • ESP Electronic Stability Protection with AOA connection for Underspeed Protection
  • Stick shaker
  • FDR Flight Data Recorder unit with integrity message to the avionics
  • Voice Warning System
  • GDL 69 A SXM datalink weather information and XM audio infotainment (US Coverage Only)
  • Chart view option for GDUs
  • Synthetic Vision Technology to be displayed on both of PFD GDU1200W
  • GSR56 datalink with satphone through headsets and WX weather information (worldwide coverage - subscription required)