Advanced Aviation Cobra

Advanced Aviation Cobra

Infobox Aircraft
infoboxwidth=20
name=Cobra


caption=
type=Homebuilt ultralight aircraft
manufacturer=Advanced Aviation
designer=
first flight=1980s
introduced=
retired=
status=
primary user=Individual civilians
more users=
produced=
number built=
unit cost=
variants with their own articles=
The Advanced Aviation Cobra was a U.S. ultralight aircraft of extremely minimalist design marketed for homebuilding. The pilot is seated in an open framework suspended beneath a fabric-covered wing on which the engine (adapted from a snowmobile) and pusher propeller are also mounted. Early Cobras (Model A) had spoilers for roll control, while the Model B had traditional full three-axis control using ailerons. A two-seat training version, known as the King Cobra was also available.

pecifications (Model B)

aircraft specifications

plane or copter?=plane
jet or prop?=prop

crew=1
length main= ft in
length alt= m
span main=35 ft 0 in
span alt=10.7 m
height main= ft in
height alt= m
area main=162 ft²
area alt=15 m²
empty weight main=218 lb
empty weight alt=99 kg
loaded weight main=
loaded weight alt=
max takeoff weight main=468 lb
max takeoff weight alt=212 kg

number of props=1
engine (prop)=
type of prop=430 Cuyuna
power main=52 hp
power alt=39 kW

max speed main=75 mph
max speed alt=65 knots, 120 km/h
range main= mi
range alt= nm, km
ceiling main= ft
ceiling alt= m
climb rate main= ft/min
climb rate alt= m/s
loading main=
loading alt=
power/mass main=
power/mass alt=

ee also

aircontent

lists=
* List of ultralight aircraft


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