I have not been able to find any clear written explanation in either old Stoddard-Hamilton Newsletters for anything from Glasair. The use of the SH-2 model designation and the more specific Glasair designation has caused much confusion in the past. Injuries: 1 Serious Flight Conducted Under: Part 91: General Aviation - Personal On January 6, 2020, at 1724 eastern standard time, an experimental amateur-built Glasair I RG, N118CV, was destroyed during a forced landing following a total loss of engine power while maneuvering in the traffic pattern at Mount Sterling-Montgomery Airport (IOB.
To differentiate within this broad family of four-cylinder Glasair models the additional designation Glasair I, Glasair II, Glasair IIS, and Glasair S-II, have been used. The The SH-2 model designation is used to cover and designate the entire broad family of Glasair models designed to use a four-cylinder aircraft engine. It was never placed in production. The SH-1 model was a tandem seat aircraft, which existed only in prototype form.
The three landing gear configurations are retractable gear (RG), fixed tricycle (FT), and tail dragger (TD). The.Three landing gear configurations are available for each of these models. Glasair Specifications and Performance. Inverted fuel and oil, Copilot brakes, slotted flaps, sloped windshield, ram air induction, extended fin and rudder, defrost/heat, cabin fan, aileron/elevator elec trim.It could not be determined whether the landing gear manufacturer or the aircraft builder had installed the bushing. 1995 kit 3301, Completed in 2001 at Jim Muldoon (Glasair Factory Tech) build assist shop. Wheel and brake performance requirements are compatible for the TSO ratings of the.GLASAIR III 199,000 ACCEPTING OFFERS Selling my beautiful Glasair III with a Reno pedigree.
The result of the Super II modifications was to give the Glasair a lot more utility, baggage weight carrying capacity and improved stability and control.)3001-XXXX are used for the Glasair III (RG only)(Ed. Note – Glasair Super IIS – This model has the longer horizontal stabilizer, the wing in the original location and the nose lengthened six inches to give more leg room and a wider C.G. These builders were given several options to pick from to make CG and stability and control improvements which included adding 12″ to the span of the horizontal stabilizer and moving the wing slightly aft (by 1.5″).)2201-XXXX are used for the Glasair SIIS (TD, FT, or RG)(Ed. Unfortunately, the II-S ended up with the CG slightly aft.
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