Overview | |||
Fixed Gear Cessna 210 TCM IO-520F 285 HP Engine 6 Seats Recent Interior Upgrade Garmin Avionics Upgrade VFR |
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Price: |
$295,000 USD
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Offered By: | Dennis Thompson International Limited | ||
Registration: | ZK-VAV | ||
S/N: | 205-0570 | ||
Location: |
New Zealand![]() |
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Days Active: | 153 days ago | ||
Airframe | |||
Total Time: | 12,090 Hours | ||
Avionics | |||
(Recent Upgrade) 1. Garmin GTR-200B VHF-COM 1. Garmin AERA-660 GPS. VFR. 1. Garmin GTX-335 Transponder ADS-B In 1. Garmin GDL-50R Transponder ADSB Out 1. Artex ME-406 ELT 1. PM Engineering PM-3000 Intercom |
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Additional Equipment | |||
Recent New Windscreen JPI EDM-930 Engine Monitor Recent New Alternator Cabin Door Stewards Recent New Voltage Regulator Vortex Generators Recent New Vacuum Pump LED Lights Belly Camera Hatch L/R Fuel. 316 Ltrs CIES Magnetic Fuel Probes Upgraded Instrument Panel and New Yokes Max Gross weight: 3,300 lbs Empty weight: 1,903 lbs Usefull Load: 1,397 lbs Fuel Burn: 53 lph. Est. Take-off Distance over 50ft: 1,465 ft Landing Distance over 50ft: 1,510 ft Cruise Speed: 130 kts Stall Speed: 50 kts Full capacity: 84 usg/316 ltrs |
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Engines & Props | |||
Engine: TCM Continental IO-520F. 285 HP Upgrade. STC 9/2IE/6. 1700 Hrs. TBO. Serial No. 570994 Time Since Overhaul: 515 Hours Date of Overhaul: 10/2004 Bulk strip following prop strike @31. Hrs. T.S.O. July 2007. Time Since Top Overhaul with new Superior cylinders = 100 Hrs NB: Running on calendar condition. 1185 Hrs to run to hour TBO Propeller: McCauley D2A34C58-00 Two Blade Total Time Since New: 3,750.5 Hrs Time since O/Haul: 305 Hours. 2013 Last Cal. Inspection: 2023 Next Cal Insp. Due: Dec 2028 |
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Engine Hours: | 5,172.2 SNEW | ||
Interior & Exterior | |||
Recently upgraded by Generation Global, Nelson. Blue leather upholstery. Condition rated: 10/10. Pristine. | |||
Overall White with Blue major and Red minor accent Trim colours. Condition Rated 8/10. Tidy. | |||
Other Info | |||
Inspection Status: Last Check 7.06.24 – next BRA 7.6.26 JEM Aviation Engine upgrade from 260 HP to 285 HP. STC. |
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Aircraft Documents | |||
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