2002 Socata Trinidad TB-21GT N713TB Colusa, CA (O08) SN Airframe Total Time: 1191

Transcription

1 Airframe Total Time: 1191 Engine Lycoming TIO 540 AB1AD Serial: L A TBO: 2000 TTSN: 1191 Compressions: Propeller Hartzell 3-Blade Propeller HC-C3YR-RF Serial: OY4739B TTSN: 1189 Maintenance No known damage history Annual Inspection due June 2016 IFR Certification due April 2016 Additional Features Keith Air Conditioning 4 Place Oxygen System Panel Mount USB Charging Outlet Sun Visors Shades for all Windows Page " 1 of " 7

2 Avionics Garmin GNS-500 with Synthetic Vision and Jeppesen Charts Garmin GTN-750 Multi-Function Display Garmin GTN-650 GPS/Nav/Comm System Garmin GDL-69 XM Weather Data Link Garmin GMA 35 Digital Remote Audio Panel Garmin GTS 800 Traffic Advisory/Alert System Garmin GTX 330 Mode S Transponder Bendix/King KT76C Transponder Bendix/King KFC 225 Auto Pilot with Altitude Preselect and Vertical Speed Full Co Pilot Instruments including Sandel 3308 Electronic HSI JP Instruments EDM 930 Engine Analyzer which displays: - RPM, manifold pressure and percent power. - Engine parameters including oil pressure, oil temperature, and fuel pressure - Engine analysis with cylinder head temperature, exhaust temperature, and turbo inlet temperature. - Fuel computer with fuel level, fuel flow, and integration with GPS for computed fuel function. - Complete data recorder for all parameters with easy cockpit download. Artex ME 406 ELT Page " 2 of " 7

3 2002 Socata Trinidad TB-21GT N713TB Interior The interior is original and is in Excellent Condition. Page " 3 of " 7

4 Exterior The exterior paint is original and in Excellent Condition. Page " 4 of " 7

5 Page " 5 of " 7

6 Performance This aircraft performance section has been assembled by the pilot of N713TB and are the real world numbers observed while flying. Cruise Performance at 75% power: 16,000ft: 174kts at 18gph 12,000ft: 162kts 9,000ft: 156kts 5,000ft: 149kts Cruise Performance at 65% power: 16,000ft: 168kts 12,000ft: 160kts 9,000ft: 153kts 5,000ft: 144kts Weights and Capacities Max Gross: 3,086 Useful Load: 917 Empty Weight: 2,169 Useable Fuel: 86 gal (516lbs) Comparative Analysis by Kenny Price The Trinidad far exceeds the comfort of any single engine airplane that I have ever flown. The seats are very comfortable, the legroom is more than suffice and with the width of the cockpit front seat area being 50 inches and the height at 44 inches, it is a delight to be in such luxury. The Beech A36 Bonanza has 7 inches less room for the front seat cockpit area and is an inch lower for headroom and with Maximum fuel, it s useful load drops to 761 lbs., 156 pounds less than the Trinidad. The Cirrus SR22 GTS has over an inch less room for the front cockpit area, and the performance speeds and Maximum payload are very similar. There is no comparison of the value that a Trinidad owner gets compared to the price of a Cirrus. The Cessna Turbo 210 has nine inches less width at the front cockpit seats and 3 inches less head room than the Trinidad. The Cessna s useful load is 870 pounds with full fuel where the Trinidad has a 917 pound capacity with full tanks. I realize that the Cessna and Beechcraft have much more fuel capacity but point being, the Trinidad s comparable performance and uncompromised comfort shows that it is an aircraft that has all of the assets that a good cross country aircraft needs. Page " 6 of " 7

7 Chase Aviation Company is proud to be the EXCLUSIVE sales Agent for this aircraft and its owner. More information can be obtained by visiting our website at Chase Aviation Company, LLC 6060 S. Aviation Ave Suite 106 North Charleston, SC Office: Fax: Located at the Charleston Int l Airport (KCHS) Page " 7 of " 7