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2015 TBM 900 N900CY SN 1068

  • Max range
    1,730 nm
  • Max cruise speed
    330 kts
  • Max passengers
    6 persons
  • Max payload
    1,400 lbs
  • Takeoff field length
    2,380 ft

Airframe:

Metal structure and skin paneling

Carbon fiber engine cowling and winglets

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

Pilot Access Door

Large access doorwith retractable stairway

Emergency exit

Front storage compartment (not pressurized)with lockable access door

Easy maintenance access doors

Wing Tie-down attachments

Gaseous oxygen system for 6 seats and quick downing masks for pilot & copilot

Capability for CDPL VHF antenna° Custompaint scheme

 

Engine:

PT6 A66D Pratt & Whitney Canada turboprop engine developing 1825 SHP thermodynamic, flat rated at 850 SHPpropeller with overspeed limiter, full feathering and reverse

Oil cooler

Anti-icing air inlet with inertial separator without operational limitation

Dual polished exhaust system aerodynamically optimized

Service access doors in cowlings

Dual engine Chip detector displayed on GDU 1500

 

Propeller:

Full composite electrically de-iced five bladed HARTZELL constant speed

Polished aluminumspinner cone

 

Controls:

Dual flight controls, control wheel with 7 integrated functions, leather covered.(Electric pitch, rudder trim, Transp, Change freq COM1, on pilot control wheel)
Elevator, rudder and aileron electric trim

Electrical pre-select flaps with integrated asymmetrydetection system

Central console including:-single lever power controlwith low bleed idle inhibition -electric flap control-fuel selector-manual pitch trim-ailerons electric trim -manual overridecontrol

Adjustable rudder pedals

Landing gear handle

Dual toe brakes -Parking brake

Landing gear emergency extension handle

Automatic environment and pressurization control system with max diff mode

Alternate static source control

Alternate ram air source control

 

Fuel Equipment:

One structural fuel tank per wing

Engine driven fuel pump

Standby electrical fuel pump and low pressure switch/ indication

Fuel tank selector with automatic fuel tank sequencer unit

Capacitive fuel gauges with low fuel level warning system

 

Ice protection:

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

 

Electrical Equipment:

New automatic starter generator transition during start

Lead acid battery 24V-42 A.h° Starter generator 28V-300 Amp

Standby generator 28 V-100 Amp° Electrical power control center

Circuit breakers

Anticollision strobe lights -Led Beacon on ground(Winglets &tail)

Navigation lights -Taxiing and landing LED lights

Ground power plug -Ground clearance energy saver

Tri-band ELT with GPS connection

14 V port + 2 USB port on copilot side

 

Instruments & Standard avionics:

G1000 Equipped Nxi° 2 GMA 1347CDualdigital audio controller with integrated marker beacon
receiver, intercom and public address capability on outer side for pilot and co-pilot

2 GDU 1040A, 10” PFD display with three axis flight dynamics, air speed,altitude, vertical speed, HSI w/ perspective modes,turn, bank side slip, NAV/COM frequencies indication and AP annunciation

1 GDU 1500 15” multi-function display with engine (w/ optimum TRQ setting display), pressurization, electrical, fuel, flaps and trims indication, Crew Alerting System (CAS), checklist, aircraft synoptics and super large 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 GTX33 Mode S transponderwith Extended Squitter (ES)

1 GCU 475 remote FMS control panel conveniently located on the central console

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

Digital Backup instrumentation altitude, airspeed and altimeter indicator

Airframe de-icing control panel

Inertial separator control

Parking brake control

Landing gear control panel

Electric generation controls and monitoring on overhead panel

Advisory panel displayed on GDU 1500 master caution warning & alertswarning and aural warning

Cabin temperature control (dual zone, with overridecapability)

Heated stall warning system

Digital chronometer displayed on GDU 1040s

Flight time hourmeter

Instrument panel lighting, CB dedicated switch lightning

2 Bose Headsets

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