2003 TBM 700C

2003 TBM 700C
S/N 261
CORPORATE AIRSEARCH INTERNATIONAL, INC.
Airframe:
ONLY 920 HOURS SINCE NEW
Engine: 3500 TBO
EXCELLENT HISTORY
FACTORY MAINTENANCE PERFORMED EXCLUSIVELY BY DAHER-SOCATA
SPECIFICATIONS/DESCRIPTIONS ARE PROVIDED AS INTRODUCTORY INFORMATION AND DO NOT CONSTITUTE REPRESENTATIONS OR
WARRANTIES OF CORPORATE AIRSEARCH INTERNATIONAL, INC. OR AFFILIATE COMPANIES. ACCORDINGLY, YOU SHOULD RELY ON
YOUR OWN INSPECTION OF THE AIRCRAFT. THE AIRCRAFT IS OFFERED SUBJECT TO PRIOR SALE OR REMOVAL FROM THE MARKET.
CORPORATE AIRSEARCH INTERNATIONAL, INC.
CONTACT J.P. HANLEY
PALM BEACH, FLORIDA
E–MAIL
WEBSITE
561.433.3510
[email protected]
www.caijets.com
2003 TBM 700C2 SN 261
CORPORATE AIRSEARCH INTERNATIONAL, INC.
CONTACT J.P. HANLEY
PALM BEACH, FLORIDA
E–MAIL
WEBSITE
561.433.3510
[email protected]
www.caijets.com
2003 TBM 700C2 SN 261
STATS
• Model: SOCATA TBM 700C2
• Serial number: 261
• Year of Manufacturer: 2003
• Airframe total time (AFTT): 920
• Engine TBO hours: 3,500
• Number of seats: 6
• Registration number: G-MCMC
• Flight rules: IFR
• Location: Portugal
CORPORATE AIRSEARCH INTERNATIONAL, INC.
CONTACT J.P. HANLEY
PALM BEACH, FLORIDA
E–MAIL
WEBSITE
561.433.3510
[email protected]
www.caijets.com
2003 TBM 700C2 SN 261
CORPORATE AIRSEARCH INTERNATIONAL, INC.
CONTACT J.P. HANLEY
PALM BEACH, FLORIDA
E–MAIL
WEBSITE
561.433.3510
[email protected]
www.caijets.com
2003 TBM 700C2 SN 261
AVIONICS / RADIOS
• 2-Tube Color EFIS (EHSI/EADI)
• 1 KFC 325 A/P (Auto-Pilot)
• 2 Garmin GNS 530 (IFR Com/Nav GPS)
• 1 Radar Altimeter KRA 405B
• 1 Multi-Function Display Honeywell KMD 850
• 2 Transponder Garmin GTX 327/330
• 1 Weather Radar Honeywell RDR 2000
• Honeywell IAHS including:
• KMH 880 (TAS Traffic Alert System & Terrain
Warning System)
• WX 500 Stormscope displayed on Honeywell KMD 850
• 2 Airspeed Indicator
• 2 Vertical Speed Indicator
• 1 Electrical Attitude Indicator
• 1 Vacuum Stand-By Attitude Indicator
• Engine Control Gauges
• Electric Pitch and Rudder Trim
• Gas Generator Tachometer
• Shadin ETM 700 Engine Trent Monitoring System
CORPORATE AIRSEARCH INTERNATIONAL, INC.
CONTACT J.P. HANLEY
PALM BEACH, FLORIDA
E–MAIL
WEBSITE
561.433.3510
[email protected]
www.caijets.com
2003 TBM 700C2 SN 261
GENERAL OVERVIEW
• Premium TBM 700C2 with Excellent life history
• Fully equipped and in excellent condition
(inside and out)
• Only 920 hours of airframe total time
• Excellent factory maintenance history
• Fresh A+ and 10-year inspection performed by
DAHER-SOCATA
• No damage history
• Serial number 261, built by DAHER-SOCATA factory
in France in 2003
• Only two private owners since new, aircraft acquired by
the current owner in 2006
• Equipped with Dual Garmin GNS 530W
• Additional features include
Air Conditioning, Artex 406 ELT, Garmin GMA-340
CORPORATE AIRSEARCH INTERNATIONAL, INC.
CONTACT J.P. HANLEY
PALM BEACH, FLORIDA
E–MAIL
WEBSITE
561.433.3510
[email protected]
www.caijets.com
CORPORATE AIRSEARCH INTERNATIONAL, INC.
CONTACT J.P. HANLEY
PALM BEACH, FLORIDA
E–MAIL
WEBSITE
561.433.3510
[email protected]
www.caijets.com
2003 TBM 700C2 SN 261
LOW HOURS & EXCELLENT MAINTENANCE
• 920 hours Total Time Airframe/Engine
• 2,580 hours to engine overhaul (TBO 3,500 hours).
• No damage history and complete and consecutive
logbooks
• Servicing, inspection and maintenance to EASA/UK
CAA procedures
• Excellent maintenance with annual inspections
performed exclusively by factory DAHER SOCATA in
Tarbes France, including A+ and 10-year inspection(s)
completed January 2014.
• Six place VIP interior with comfortable beige leather
seats, burr walnut panelling and contrasting
“Ultrasuede” headlining with beige carpeting.
• CAMO Continued Airworthiness Maintenance Oversight
• Professionally flown since new.
• Always hangared in Europe, United Kingdom, France
and Portugal (Aircraft’s current location).
LICENSES AND CERTIFICATIONS
• Airworthiness Review Certificate (ARC)
Valid until 28/01/2015
• UK Certificate of Registration from CAA since
April 2006
CORPORATE AIRSEARCH INTERNATIONAL, INC.
CONTACT J.P. HANLEY
PALM BEACH, FLORIDA
E–MAIL
WEBSITE
561.433.3510
[email protected]
www.caijets.com
CORPORATE AIRSEARCH INTERNATIONAL, INC.
CONTACT J.P. HANLEY
PALM BEACH, FLORIDA
E–MAIL
WEBSITE
561.433.3510
[email protected]
www.caijets.com
SOCATA 700C STANDARD DEFINITIONS *
Powerplant
Manufacturer:
Type:
Model:
Thermodynamical power:
Flat rated power:
Air intake:
Pratt & Whitney
free turbine, inverse flow
PT6A-64 turboprop
1,583 shp
700 shp
deiced, inertial separator
Propeller
Manufacturer:
Type:
Model:
Diameter:
Fuel
Total Fuel capacity:
Useable fuel:
Average fuel consumption:
Hartzell
Four-blade, all metal, reversible/feathering
HC-E4N-3/E9083S (K)
91 in.
Jet A
290.60 US gallons
281.62 US gallons
50 US gallons per hour
Oil
Type:
Total oil capacity:
Maximum consumption:
MIL-L-23699C (viscosity 5 cSt)
12.7 US quarts
0.3 US quarts an hour
Dimensions
Overall length:
Wingspan:
Height:
Horizontal tail span:
Wing area:
Wing aspect ratio:
Wheelbase:
Wheeltrack:
Turn diameter, wing tip:
34.92 feet
41.60 feet
14.29 feet
16.36 feet
193.75 square feet
8,216
12.71 feet
9.56 feet
67.3 feet
Internal Dimensions
Cabin length:
Cabin width:
Cabin height:
Maximum freight volume:
Length of freight area:
Cargo cabin floor area:
Rear access door dimensions:
Rear luggage compartment dimensions:
Rear luggage door dimensions:
Optional pilot door dimensions:
13.29 feet
3.97 feet
4.00 feet
123.6 cubic feet
10 feet
33.9 square feet
3.9 x 3.54 feet
16 x 12 x 31.5 in
15 x 10 in
3.34 x 2.56 feet
* Standard definitions provided courtesy of Daher-Socata and is for informational planning
purposes only. Some equipment listed may or may not be installed on TBM 700C2, S/N 281.
CONTACT J.P. HANLEY - [email protected] - 561-433-3510 - WWW.CAIJETS.COM
SOCATA 700C STANDARD DEFINITIONS *
Airframe
• 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, dissymmetry detector and sensor
• Bank control through ailerons and spoilers with trim on left aileron
• Retractable gear with electrohydraulic 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
• Standard painting and decoration
• Airframe pneumatic de-icing equipment
• Easy maintenance access doors
Electrical Equipment
• Lead acid battery 24 V-43 A/h
• Starter generator 28 V-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 lights
• Navigation lights
• Taxiing and landing lights
• Ice detector light
• Ground power plug
• Ground clearance energy saving system
• Left-hand and right-hand map lights
• Left-hand and right-hand electrical heated windshields
* Standard definitions provided courtesy of Daher-Socata and is for informational planning
purposes only. Some equipment listed may or may not be installed on TBM 700C2, S/N 281.
CONTACT J.P. HANLEY - [email protected] - 561-433-3510 - WWW.CAIJETS.COM
SOCATA 700C STANDARD DEFINITIONS *
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
• Landing gear position monitoring panel
• Flaps position indicator
• Trim position indicator (elevator, rudder, ailerons)
• Voltmeter and ammeter
• Electric generator control and monitoring on overhead panel
• Advisory panel with master caution, master warning and aural alerts
• Fuel management panel
• Cabin temperature gauge
• Cabin altitude and differential pressure indicator
• Climb rate of climb indicator
• Heated stall warning system
• Flight time hour meter
• Instrument panel lighting
Engine
• PT6A-64 Pratt & Whitney Canada turboprop engine developing
1583 Shp thermodynamic, flat 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
* Standard definitions provided courtesy of Daher-Socata and is for informational planning
purposes only. Some equipment listed may or may not be installed on TBM 700C2, S/N 281.
CONTACT J.P. HANLEY - [email protected] - 561-433-3510 - WWW.CAIJETS.COM
SOCATA 700C STANDARD DEFINITIONS *
Fuel Equipment
• On structural fuel tank per wing
• Engine driven fuel pump
• Standby electrical fuel pump
• Fuel tank selector with automatic sequencer unit
• Capacitance gauging with low level warning
Cabin Fittings
• Pressurized cabin (p = 6.2 psi)
• All seats with adjustable backrest
• Carpeting florr and Alcantara upholstery
• Ash-trays
• Sound proofing and thermal insulation
• Front and rear 24V outputs
• Air conditioning (R-134)
• Storable working table
• Cabin ventilation
• Airway chart cabinet
• Individual vents and lighting
• Refreshment cabinet
• Sun visors and curtains
• Gaseous Oxygen System
• Fully adjustable pilot seats
• Coat-rack
(height, depth, and backrest)
• Halon cabin extinguisher
• Baggage compartment with straps and net
• Platinum Edition including:
high comfort leather seats
wood veneered overhead panel
wood veneered baggage compartment frame
wood veneered retractable working table
black chrome or gold metallic finishing
smoked brown mirror in baggage
compartment carpet runner
cabinets with wood veneered doors, leather covered
Controls
• Dual flight controls
• Adjustable rudder and nose-wheel steering pedals
• Electrical pitch and rudder trims on
• Landing gear retraction and extension control
left-hand and right-hand control wheels
• Central console including:
Power control
• Environment and pressurization control system
• Alternate static source control
• Alternate ram air source control
Propeller pitch control
Condition lever
Manual control override
Electric flaps control
Fuel selector control
Manual pitch trim
Ailerons electric trim
* Standard definitions provided courtesy of Daher-Socata and is for informational planning
purposes only. Some equipment listed may or may not be installed on TBM 700C2, S/N 281.
CONTACT J.P. HANLEY - [email protected] - 561-433-3510 - WWW.CAIJETS.COM
SOCATA 700C STANDARD DEFINITIONS *
Ice Protection
• Pneumatically deiced wing and tail unit with ice light
• Heated engine air intake lip
• Pilot controller engine inertial separator
• Electrically heated propeller blades
• Electrically heated pitot tubes
• Electrically de-iced stall warning sensor
• Left-hand and right-hand electrically heated windshields
Loading
Basic empty weight:
4,685 lbs
Maximum zero fuel weight:
6,032 lbs
Maximum ramp weight:
7,430 lbs
Maximum takeoff weight:
7,394 lbs
Maximum payload:
1,347 lbs
Maximum payload with full fuel:
804 lbs
Maximum luggage capacity in storage areas:
297 lbs
Maximum landing weight:
7,024 lbs
Performance
Time to climb to 26,000 feet at MTOW:
18 min 45 sec
Time to climb to 31,000 ft. at MTOW:
Maximum cruise speed at 26,000 ft:
21 min
280 to 300 KTAS
Economy cruise speed at 31,000 ft:
Certified ceiling:
248 KTAS
31,000 ft
Distances
(ISA conditions at maximum take-off weight with 50 ft. obstacle clearance)
Take-off:
2,133 ft.
Landing without reverse:
2,133 ft.
Ranges
Maximum range (ISA conditions, max. take-off weight NBAA IFR Reserve)
With full fuel economical cruise speed:
1,637 Nm
With full fuel maximum cruise:
1,344 Nm
With max. passengers economical cruise speed:
330 Nm
With max. passengers maximum cruise:
294 Nm
* Standard definitions provided courtesy of Daher-Socata and is for informational planning
purposes only. Some equipment listed may or may not be installed on TBM 700C2, S/N 281.
CONTACT J.P. HANLEY - [email protected] - 561-433-3510 - WWW.CAIJETS.COM
CORPORATE AIRSEARCH INTERNATIONAL, INC.
J.P. Hanley
PRESIDENT
Corporate AirSearch International, Inc.
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t CORPORA
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E-MAIL
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