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2015 TBM 900 N900CY SN 1068

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 door with retractable stairway
Emergency exit
Front storage compartment (not pressurized)
with lockable access door
Easy maintenance access doors
Wing Tie-down attachments
Jacking points
Gaseous oxygen system for 6 seats and quick downing masks for pilot & copilot
Capability for CDPL VHF antenna
Custom paint scheme


PT6 A66D Pratt & Whitney Canada turboprop engine
developing 1825 SHP thermodynamic, flat rated at 850 SHP
propeller 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

Full composite electrically de-iced five bladed HARTZELL constant speed
Polished aluminum spinner cone


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 asymmetry detection system


Central console including:
– single lever power control with low bleed idle inhibition – electric flap control – fuel selector – manual pitch trim – ailerons electric trim
– manual override control

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

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