N81WD - 1987 GLASAIR GLASAIR I RG

1987

GLASAIR

GLASAIR I RG

N81WD

Used

IFR

2200.0

2

XC rocket 170 mph at 7 gph or over 200 mph Gross 2100 lbs, empty 1350 lbs, useful load 750 lbs Ive flown it at 22,000 ft. 2 place side-by-side with 100 lbs luggage capacity Turbocharged Glasair I RG

780

SMOH

Lycoming TSIO-360 180/220 hp turbo-normalized

Hartzel Scimitar constant speed 206hr SOH

Completely upgraded IFR instrument panel

IFR Garmin GNS430W with Demo Mode switch (ground use only) Garmin SL-30 Garmin 396 panel mounted w/XM weather (dont fly without it!) Grand Rapids Technology Horizon I Efis & AHRS KI-209A Nav Indicator TruTrak Sorcerer 3-axis A/P coupled with EFIS, 430, SL30. Can control from EFIS or independently TruTrak ADI backup artificial horizon, ball, bank Backup Airspeed Backup Altimeter KT76-A transponder PS Engineering PM-3000 intercom Custom annunciator panel with test and dim Precision Aviation Vertical card compass Dual com antennas Left & right stick mounted PTT switches Left stick A/P CWS/disengage Left Phono, mic & Bose jacks, Right phono, mic & aux audio jacks Cooled GNS430W & KT76A

Remote oil filter (easy to change) Plasma electronic ignition Fine wire spark plugs plus Plasma automotive HID landing light Lightweight starter 45 amp lightweight alternator All electric, no vacuum system 18AH backup battery Battery minder Thermostatic battery warmers Thermostatic Tanis engine pre-heater with cylinder heat Emergency power switch and indicator Heavy duty Grove 56-113 brakes & wheels upgrade Gear extension: Standard electric hydraulic pump Manual up/down gear control override switch Standard gravity drop emergency gear extension (They dont work very well!) Manual hydraulic hand pump gear extension (works very well) Electronics International MVP-50 Engine Analyzer with up/down hydraulic pressure, TAS, fuel flow & totalizer, alternator & battery amps & volts, 4 cylinder CHT & EGT, TIT, pressure altitude, OAT, vertical speed, airspeed, engine hrs, tach hrs, GPS coordinates, in addition to standard MP, RPM, oil T&P, etc. All downloadable for analysis Halon fire suppression system Mechanical and electrical fuel pumps Fuel Capacity: 42 gal main, 6 gal header, 17 gal aux fuel tank Approx 1600 mi range with aux tank Fill main tank from either side Transfer pump for aux tank with empty indicatior Dual stick & rudder controls Pilot side brakes Manual flaps and elevator trim 24 cu ft AL O2 tank Pulse demand O2 Controller Stramm medium wing extensions (similar) Float valve main tank fuel vents (no vent siphon leakage) Left slider door, right gull wing Fresh air vents Variable heater control with pilot/passenger damper First Place, Corinthian Class, Great American Cross Country Race 1993 Oil analyses available from May, 2006

The original has some pearl in it which hasnt been completely matched for some repainting. Optionally includes wing jacks and tail weight. Complete hangar tools, supplies, and parts negotiable.

Fresh Annual Damage history: Nose gear up landing 11/97, repaired, engine overhauled & 320-360 conversion Left main gear collapse 9/06, engine disassembled inspected, no damage. Prop trued and overhauled. Hard landing with prop strike 7/09, engine disassembled inspected, no damage, nose gear replaced, main forks replaced, new prop blades.