Aircraft Sales


	SPECIFICATIONS
	Airframe:	Year: 1991 TTSN: 2888.6
	Engine:	P&W PT6A-66D TTSN: 2898 Cycles: 1730 HSI: 1975 Prop TT: 2888.6 (Prop Overhaul completed at 1770 hrs)
	Avionics:	KFC-275 Fully Coupled Autopilot with Remote Annunciator GMA-340 Audio Panel with Six Place Intercom, split comm., and PA function GNS-530W GPS/Comm (2) (both upgraded to WAAS in 2007) KI-825 Electronic HSI (2004) KR-87 ADF GTX-330 Transponder (new 2007) (TIS displayed on MX20) KN-63 DME with KDI-572 Indicator KAS-297C Altitude PreSelect KI-229 RMI Co-pilot A/S, Horizon, Altimeter, VS Co-pilot Electric Trims and PTT on yoke Co-pilot KCS-55A Compass System with HSI Indicator and KA-51B Slaving Control RDS-82 Vertical Profile Four Color Stabilized Radar WX-500 Stormscope with Display on GNS-530s, MX20 and KI-825 HSI MX20 Multifunction Display (moving map, traffic, terrain, stormscope, radar, Jepp charts, Wx) Ryan 9900BX TCAD (displayed on both GNS-530s) (2004) Garmin GAD-42 Roll Steering Adapter (2004) Shadin Air Data Computer (2004) Garmin Class B TWAS (terrain) (2004) WSI Wx cockpit weather system (nexrad, tops, METARs, TAFs (inc. Canada)) (2007) JeppView (displaying charts on MX20) (2004) Shadin Micro-flo Fuel Flow Indicator (2004) RVSM upgrade by Socata (04/2005) 2 Noise-canceling Headsets (one Bose, one David Clark)
	Interior:	Grey Leather with Green Accent and Charcoal Wool Carpet
	Additional Equipment:	Airborne Hourmeter (Hobbs) Astrotech Chronomenter Accordion Style Window Shades Fire Extinguisher Parking Kit and factory Towbar Dual Cabin Door Support Cables w/ dampener for lower door Refreshment and Storage Cabinet (pilot and copilot side) New copilot and pilot windshields (2005) All new leather interior (headliner to carpet; fore to aft) (2001)
	Exterior:	White over Green with Silver and Charcoal Accent. New paint (2005)
	Remarks:	No damage history This aircraft has all mandatory ADs and SBs complied with: Optional SB14261 (CT turbine blade upgrade) (05/2004) All ten year structural inspection items 03/(2006) All 1200 hour items (bonding inspection, ultrasound of composites, etc.) (03/2006) 14 year O2 canisters replaced (03/2006) #3 bearing seal replaced to correct coking problem (12/2006) Optional P&WC SIL PT6A-128 (fuel control unit bellows upgrade) (12/2006) Seven year gear overhaul (03/2008) The engine was inspected at the P&WC factory in 02/2008 after a minor FOD damage repair by P&WC. The engine was rebalanced and tested in their test cell. The test cell runs were all normal and the vibration surveys came out well within limits. The vibration surveys were better than those obtained after the #3 bearing seal replacement and the fuel control unit upgrade in 12/2006! This is possibly the best maintained, most upgraded, lightest (568 full fuel useful load), tightest (early model), smoothest (newly rebalanced engine) TBM700-A model available. Outstanding “transition” aircraft for those looking forward to VLJ and/or G1000 aircraft. Non-EFIS, but has E-HSI (therefore, lighter, less maintenance expense and no encroachment on nose baggage compartment space with EFIS avionics).
For more information: Brian Jones Northwest Aircraft / Million Air - SLC 1-800-752-5382 - Toll Free 801-550-8444 - Mobile bjones@maslc.com

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