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2009 EADS/SOCATA TBM 850

Seller: Avex | Seller Information
State: California
Country: United States of America
Price Call for Pricing
Views: 1856
Year: 2009
Aircraft Type: EADS/SOCATA
Location: Camarillo, California
Condition: New
Registration Number: Call
Total Time: New
Engine Specification: PT6 A66D Pratt & Whitney Canada turboprop engine
developing 1825 SHP thermodynamic, flat rated at 850 SHP
Electrically de-iced four bladed Hartzell constant speed
propeller with overspeed limiter, full feathering and reverse
Polished aluminium spinner cone
Oil cooler
Anti-icing air inlet with inertial separator
Dual exhaust system
Service access doors in cowlings
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 hourmeter
Instrument panel lighting
Backup instrumentation with pneumatic attitude,
airspeed and altimeter indicators
Interior/Exterior: Interior: Choose your own

Exterior: Optional Paint Schemes and Colors
Additional Equipment: Metal structure and skin panelling
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
Large access door with retractable stairway
Emergency exit
Front storage compartment (not pressurized)
with lockable access door
Rear fuselage servicing door
Easy maintenance access doors
Tie-down attachments
Jacking points
Standard painting and decoration
Gaseous oxygen system with quick downing pilot
and co-pilot oxygen masks
Description:
Dual flight controls
Electric pitch and rudder trim on pilot control wheel
Elevator, rudder and aileron electric trim
Electrical pre-select flaps with integrated
asymmetry detection system
Central console including:
- power control
- propeller pitch control
- condition lever
- manual control override
- electric flap control
- fuel selector
- manual pitch trim
- ailerons electric trim
Adjustable rudder pedals
Landing gear handle
Dual toe brakes
Parking brake
Landing gear emergency extension handle
Environment and pressurization control system
Alternate static source control
Alternate ram air source control

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

 

 

 

 

 

 

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