
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