N700CZ - 2004 DAHER TBM 700C2
Aircraft Summary
General
Year
2004
Manufacturer
DAHER
Model
TBM 700C2
Serial Number
301
Condition
Used
Registration #
N700CZ
Description
Compliant seats and cabin luggage restraint including 4 points harnesses on front seats and 3 points safety belts on other seats
All seats with folding armrests and headrests
Heavy duty main wheels and tires
Ice protection:
Pneumatically deiced wing and tail unit, with ice light
Heated engine air intake lip
Pilot controlled engine inertial separator
Electrically heated propeller blades
Electrically heated pitot tubes
Electrically deiced stall warning sensor
Left-hand and right hand electrically heated windshields
Fuel Equipment:
One Structural Fuel Tank per Wing
Engine driven fuel pump
Stand-by Electrical Fuel Pump
Fuel Tank Selector with Automatic Sequencer Unit
Capacitance Gauging with Low-Level Warning
Miscellaneous:
Parking protection kid
Cabin cover
Options:
RVSM equipped
Right hand map reading tablet
Custom Painting and Decoration
Miscellaneous:
Ni-Cad battery (replacement of lead battery)
Thommen needle chronometer (replacement of digital chronometer)
Pulse light anticollision system
4 Bose X headsets connected and hardwired to battery
Engine time hourmeter (replacement of flight time hourmeter)
CD player kabinet with 4 Bose X headsets
One Owner and Pilot Since New, Replaced w/ CJ3, RVSM Equipped.
Airframe
Total Time
770.0
Airframe Notes
Metal Structure and Skin Paneling
Anti-Corrosion Protection Treatment
Pitch control through elevators with trim
Yaw control through rudder with trim
Electrical Flaps with Integrated Track and Dissymmetry Detektor and sensor
Bank Control through Ailerons and Spoilers with trim on left aileron
Retractable Gear with Electro Hydraulic actuation
Hydraulic Disc Brakes
Pressurized 6 seats cabin and baggage compartment
Large Access Door with Retractable Stairway
Front storage Compartment (not Pressurized) with External access Door
Rear baggage Compartment (not Pressurized) with External access Door
Emergency Exit
Rear Fuselage Servicing Door
Tie-Down Attachments
Jacking Points
Airframe pneumatic de-icing equipment
Easy Maintenance Access Doors
Engine Program
Engine Program Notes
PT6 A64 Pratt and Whitney Canada turboprop engine developing 1583 Shp thermodynamic, rated at 700 Shp
Electrically de-iced four bladed Hartzell constant speed propeller with overspeed limiter, full feathering and reverse
Polished aluminum spinner cone
Oil cooler
Inertial separation anti-icing air inlet
Dual exhaust
Servicing doors in cowlings
Avionics
Avionics/Radios
Left hand and center panels:
GMA 340 stereo audio panel with music input and marker beacon
1 Bose X pilot headset, stereo with noise attenuator
EHSI/EADI EFIS 40 2 tubes with symbol generator, KVG 350, KCS 305 with heading comparator alarm, turn and bank indication
GNS 530 VHF (FM immune) COM (25 kHz and 8,33 kHz spacing) /VOR-ILS/GPS
GNS 530 VHF (FM immune) COM (25 kHz and 8,33 kHz spacing) /VOR-ILS/GPS with GI 106 A VOR/ILS indicator
KMD 850 Multi-Function Display
KMH 880 Traffic Alert System (TAS) and Terrain Awareness Warning System (TAWS) displayed on MFD
WX 500 Stormscope displayed on MFD KMD 850
KNI 582 RMI Indicator Connected to Heading No. 2
KN 63 DME with Output to the EHSI and KDI 574
KEA 346 Encoding Drum Altimeter Connected to Transponder Nr. 1
Tri-band ELT with aircraft identification
KFC 325 3 Axis Digital Auto Pilot with Pre-Select Altitude and Yaw Damper
Stand-by Vacuum Artificial Horizon
Right hand panel:
KRA 405 B Radar Altimeter connected to EHSI
KR 87 SC+ADF
KDI 574 DME Indicator
RDR 2000 Radar. Connected to MFD KMD 850
GTX 330 Mode S Transponder (Nr. 1)
UI 35 000 ft Encoding Altimeter connected to Transpoter Nr. 2
GTX 327 Mode C Transpoter (Nr. 2)
Electrical Artificial Horizon
Vertical Speed Indicator
Airspeed Indicator
KCS 55 A heading n and KI 525 A HSI indicator, Connected to NAV 2
2nd Bose X stereo headset, with noise attenuator
Additional Equipment
Additional Equipment
Electrical Equipment:
Lead Acid Battery 24V-40A/h
Starter Generator 28V -200Amp (rated at 180 Amp)
Standby generator 28 V-70 Amp (rated at 57 Amp)
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
Ground Clearance Energy Saving system
Left-hand and right-hand map light
Left-hand and right-hand electrical heated windshields
Instruments:
Integral Instrument Panel with Spare Locations for Options
Airspeed Indicator
Vertical Speed Indicator
Magnetic Compass
Torque Indicator
Propeller Tachometer
Turbine Temperature Indicator (ITT)
OAT Indicator
Airframe De-Icing Control Panel
Inertial separator control
Parking brake control
Flaps Position Indicator
Trim Position Indicator (Elevator, Rudder and Ailerons)
Voltmeter and Ammeter
Electric Generator Control and Monitoring on Overhead Panel
Advisory Panel with Master Caution, Master Warning and Aural Warnings
Fuel management panel
Cabin temperature gauge
Cabin altitude and differential pressure indicator
Climb rate of climb indicator
Heated stall warning system
Flight time hourmeter
Instrument panel lighting
Interior
Interior Notes
Pressurized Cabin (p =6.2 PSI)
Carpeting floor and Alcantara Upholstery
Sound-Proofing and Thermal Insulation
Air Conditioning (R 134)
Cabin ventilation
Individual Vents and Lightings
Sun Visors and Curtains
Fully Adjustable Pilots Seats (Height, Depth and backrest)
All Seats with Adjustable Backrests
Ashtrays
Front and rear 24 V outputs
Storable working table
Air Way Charts Cabinet
Refreshment Cabinet
Gaseous Oxygen System
Baggage Compartment with Straps and Net
Coat-Rack
Halon cabin extinguisher
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