- AEA Red Wing
Infobox Aircraft
name=AEA Red Wing
caption=
type=Early experimental aircraft
manufacturer=Aerial Experiment Association
designer=Thomas Selfridge
first flight=12 March 1908
introduced=
retired=
status=Destroyed on first flight
primary user=Aerial Experiment Association
more users=
produced=
number built=
unit cost=
variants with their own articles=The Red Wing (or Aerodrome #1) was an early aircraft designed byThomas Selfridge and built by theAerial Experiment Association in 1908. It was named for the bright red color of its silk wings - chosen to achieve the best result with the photography techniques of the day.On
12 March 1908 Frederick W. Baldwin piloted the aircraft off the frozenKeuka Lake nearHammondsport, New York in what would be the first public demonstration of a powered aircraft flight in the United States as well as the first flight by a Canadian pilot. "Selfridge Aerodrome Sails Steadily for 319 Feet. At 25 to 30 miles an Hour." "Washington Post ",13 May 1908 .]Contemporary accounts described the flight as the "First Public Trip of Heavier-than-air Car in America." Reports entitled "Views of an Expert" stated that Professor
Alexander Graham Bell 's new machine, the Red Wing, built from plans by Lieutenant Selfridge, was "shown to be practicable by flight overKeuka Lake ,Hammondsport, New York ,12 March 1908 by F. W. Baldwin, the engineer in charge of its construction."The aircraft covered 319 ft (97 m) at a height of around 20 ft (6 m) before crashing 20 seconds after takeoff. A portion of the tail gave way, bringing the test to an end. The Red Wing was damaged beyond repair.
pecifications (Red Wing)
aircraft specifications
plane or copter?=plane
jet or prop?=propcrew=1
length main=26 ft
length alt=8.0 m
span main=43 ft 4 in
span alt=13.21 m
height main= ft in
height alt= m
area main= ft²
area alt= m²
empty weight main= lb
empty weight alt= kg
loaded weight main=
loaded weight alt=
max takeoff weight main=
max takeoff weight alt=number of props=1
engine (prop)=Curtiss
type of prop=air-cooledV8 engine
power main=40 hp
power alt=30 kWrange main=319 ft
range alt=97 m
loading main=
loading alt=
power/mass main=
power/mass alt=References
;Notes;Bibliography
* [http://www.aerofiles.com/_ab.html "Aerofiles"] . Retrieved:19 May 2005 .ee also
aircontent
lists=
*List of experimental aircraft
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