Glasair I

Infobox Aircraft
name= Glasair I


caption=
type=amateur-built kit airplane
manufacturer=Glasair Aviation
designer=
first flight= 1979
introduced=1980
produced=
number built=
unit cost=
variants with their own articles=

The Glasair I, originally built as the prototype Glasair TD taildragger, is a high-performance homebuilt aircraft built of fiberglass. Created by Tom Hamilton as a fast, two-seat kitplane, the Glasair TD first flew in 1979. Hamilton formed Stoddard-Hamilton Aircraft that year to produce and market the kit, which was the first pre-molded composite aircraft available to builders.

pecifications

aircraft specifications

plane or copter?=plane
jet or prop?=prop
crew=2
capacity=
length main= ft in
length alt= m
span main= ft in
span alt= m
height main= ft in
height alt= m
area main= ft
area alt= m
airfoil=
empty weight main= 999lb
empty weight alt= 454 kg
loaded weight main= 1,700lb
loaded weight alt= 773 kg
useful load main= lb
useful load alt= kg
max takeoff weight main= 1,700lb
max takeoff weight alt= 773 kg
more general=
engine (prop)=
type of prop=
number of props=
power main= hp
power alt= kW
power original=
max speed main= mph
max speed alt= km/h
cruise speed main= mph
cruise speed alt= km/h
never exceed speed main= mph
never exceed speed alt= km/h
stall speed main= mph
stall speed alt= km/h
range main= mi
range alt= km
ceiling main= ft
ceiling alt= m
climb rate main= ft/min
climb rate alt= m/s
loading main= lb/ft²
loading alt= kg/m²
thrust/weight=
power/mass main= hp/lb
power/mass alt= kW/kg
more performance=
armament=
avionics=

References