N25GJ - 2010 DAHER TBM 850

2010

DAHER

TBM 850

547

Used

N25GJ

IFR

EBAW

N25GJ has had only two owners and has been meticulously maintained at the Daher factory in France. Fresh annual and C+ inspection. Hartzell 5-blade propeller • Low Time: 1,190 AFTT • Brand new Hartzell 5 blade Propeller • G1000 with Synthetic vision • PT6-66D Engine • Cruise at 320 Knots • Trend Monitored Since New • Log Books Available Airframe Metal structure and skin paneling Anti-corrosion protection treatment Electrical pre-select flaps with integrated track and dissymmetry detector Bank control through ailerons and spoilers with trim on left aileron Retractable gear with electro hydraulic control Hydraulic disc brakes Large cabin and baggage compartment Large access door with retractable stairway Front storage compartment (not pressurized) with external door Emergency exit Rear fuselage servicing door Tie-down attachments Jacking points Painting and decoration High-speed pneumatic de-icing equipment Easy maintenance access doors Engine(s) PRATT & WHITNEY PT6-66D Electrical starter/generator Oil cooler Inertial separation anti-icing air inlet Dual exhaust Servicing doors in cowlings Prop Specs NEW 5-bladed Hartzell Avionics/Radios G1000 Flight Deck includes: • Airspeed Indicator displayed on GDU 1040s • Vertical speed indicator displayed on GDU 1040s • Magnetic compass • Torque indicator displayed on GDU 1500 • Propeller tachometer displayed on GDU 1500 • Turbine temperature indicator (ITT) displayed on GDU 1500 • Gas generator tachometer displayed on GDU 1500 • Oil pressure and temperature indicator displayed on GDU 1500 • OAT Indicator displayed on GDU 1040s • Airframe de-icing control panel • Inertial separator control • Parking brake control • Landing gear position monitoring panel • Flap position indicator displayed on GDU 1500 • Trim position indicator (elevator, rudder and ailerons) displayed on GDU 1500 • Voltmeter and ammeter displayed on GDU 1500 • Electric generation controls and monitoring on overhead panel • Advisory panel with master caution, master also displayed on GDU 1500 warning and aural warning • Fuel management panel displayed on GDU 1500 • Cabin temperature control • Cabin altitude and differential pressure indicator displayed on GDU 1500 • Cabin rate of climb indicator displayed on GDU 1500 • Heated stall warning system • Digital chronometer displayed on GDU 1040s • Flight time hour meter • Instrument panel lighting • Backup instrumentation with pneumatic attitude, airspeed and altimeter indicators Instrument Panel: Integral instrument panel w/ spare locations for options Airspeed Indicator Sensitive altimeter Vertical speed indicator Electrical turn and bank indicator Magnetic compass Digital Chronometer Gas generator tachometer Propeller tachometer Fuel management panel Data Computer Oil pressure indicator Torque indicator Turbine temperature indicator (ITT) OAT Indicator Landing gear control and monitoring panel Flaps position indicator Trim position indicator (elevator, rudder and ailerons) Voltmeter and ammeter Electric generator control and monitoring on overhead panel Instrument panel lighting Advisory panel with master caution, master warning and aural warnings Environment and pressurization control system Airframe de-icing control panel Stall warning system Alternate static Additional Equipment Electrical Equipment: Lead Acid battery 24V-43A/h Starter generator 28V Auxiliary generator High safety electrical power center for regulation and switching Circuit breakers Anti-collision strobe lights Navigation lights Taxiing and landing lights Ice detector light Ground power plug receptacle Ground clearance energy saver Controls: Dual flight controls Electrical pitch and rudder trim (LH and RH) Adjustable rudder and nose wheel steering pedals Central console including: -Power control -Propeller pitch control -Condition lever -Manual control override -Electric flaps control -Fuel selector control -Ailerons electric trim Dual toe brakes Parking brake Miscellaneous: Map reading tablet Refreshment cabinet LH Hour meter airborne Pulse light anti-collision system Supplementary Gaseous Oxygen Fuel Equipment: One structural fuel tank per wing Constantly operating mechanical fuel pump Stand-by electrical fuel pump Fuel tank selector with automatic sequencer unit Capacitance gauging with low-level warning

1190.0

PT6-66D

New Hartzell 5-blade prop installed in October 2017 in replacement of the original Hartzell 4-blade prop that had a strike.

ADF Garmin transponder 33DES (Diversity) GSR56

2010

2010

6