This Sharp Daher TBM 960 only has 600 Hours Total Time Airframe and Engine. Full Remaining Maintenance and Warranty program through July 2027. Highlights include HomeSafe™ Autoland, Autothrottle, Automatic Ice Detection and Activation, All LED Lighting, Electronic Tinted Window Shades and Pilot Door. Contact Steve Davis for more information. sdavis@elliottjets.com or 515-865-2790.
600 Hours Since New
600 Hours Since New
PT6E- 66XT Pratt & Whitney Engine turboprop engine developing 1844 HP thermodynamic, flat rated to 895 HP.
Six genuine black leather heated seats with adjustable backrests, folding armrests and intermediate seats with forward or backward accommodation with multiple installation configuration. Interior colors consist of black lower side panels and carpet, white sand upper side panels and flat black metal finishes.
Signal White Upper, Coronado Blue Lower with Payolle Blue and Tallon Silver Accents.
• 600 Hours Total Time Airframe and Engine
• 5-Blade Hartzell Propeller
• 5,000 Hour Engine TBO
• FADEC Engine and Prop
• HomeSafe™ Autoland
• Autothrottle
• Automatic Ice Detection and Activation
• Garmin WX 8000 Fully Automated Airborne Radar
• Pilot Door
• GDL 60 for Automated WIFI and cellular data base updates
• Electronic tinted window shades
• 300 Amp Starter Generator – 100 Amp Standby Alternator
• All LED Lighting
• 330-knot Cruise
• 31,000-ft. Reached in 18 Minutes, 45 Seconds
• Full remaining Maintenance and Warranty program through July 2027
Garmin G3000
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
1 GTX 345 Mode S Extended Squitter transponder (#1) ADS-B In & out, 1 GTX 335 Extended Squitter Mode S ADS-B out(#2)
2 GTC 580 Tactile Controllers conveniently located on the reclined section of the p
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)
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