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This aircraft is currently registered in Canada. It is located in British-Columbia and was U.S Registered. A FAA designated DAR has reviewed the aircraft and  there are no issues  for re-registration  in the US .


Year 2003
Reference Number 7899
Airframe Time 661
Engine S.M.O.H. 390 hours, Lycoming IO-540-A1DS 260HP, EMS-220 engine monitor
Propeller S.P.O.H. NEW, MT-PROPELLER/205-58, S/N XB-25275
Avionics Dual Dynon Skyview 10" EFIS/EMS avionics system
Garmin GMA240 intercom
Garmin GNS480 WAAS GPS/NAV/COM radio
Certified IFR enroute/approach with current database
GNS480 flight plan can be displayed on Skyview map and HSI, and control autopilot LNAV & VNAV
Bendix King KLX-135 GPS/COM radio
Bendix King KT-76A mode C transponder
ACK E-04 406Mhz ELT with GPS input
2 x 10" EFIS displays
Equipment Clamar 2200 composite amphib floats with gear advisory
Registered gross weight 2350lb, empty weight 1720 lb
Extended fuel tanks with monitored transfer pumps
Custom designed landing gear audio/visual advisory
Electric trim on each stick
Pulse light
Vertical card magnetic compass mounted on windscreen
Dual USB 2A power ports on panel (iPad compatible)
Remarks Shoulder harnesses
Extended baggage
Door clips
Glove box, sized to hold sectional charts
Originally built in Troutdale, OR 2003 by A&P
All builders logs
Avionics: 2 x BAT320 1 hour system backup battery
ADAHRS-200 airdata/attitude/heading primary module
ADAHRS-201 second module for redundancy
ARINC429 data interface to GNS480
SV42 roll and pitch autopilot servos
Heated pitot with AOA
Was previously US Registered
No Damage History
Glastar on Floats operating limitations from Glastar Service Letter 4:
Vx 65 kts
Vy 78 kts
Vs 52 kts
Vso 46 kts
Vfe 75 kts
Va 105 kts
Vno 133 kts
Vne 149 kts
Max Gross Weight 2350 lb
Basic Empty Weight 1720 lb
Cruise Speed @60% power = 100 kts
Fuel Consumption @60% power = 10.5 gph
Exterior White with wine trim
Interior Grey cloth/leather seats
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Specifications are Subject to Verification Upon Inspection and/or Prior Sale