The Comp Air CA12 is a turboprop-powered civil utility aircraft, currently under development. Comp Air is seeking certification. It is configured as a conventional, low-wing monoplane with tricycle undercarriage. The first flight was on April 14, 2007.
Attributes | Values |
---|---|
rdf:type | |
rdfs:label |
|
rdfs:comment |
|
dcterms:subject | |
Wikipage page ID |
|
Wikipage revision ID |
|
Link from a Wikipage to another Wikipage | |
Link from a Wikipage to an external page | |
sameAs | |
span ft |
|
stall speed kts |
|
wing area sqft |
|
wing loading lb/sqft |
|
dbp:wikiPageUsesTemplate | |
dbp:primeUnits%3F_ |
|
national origin | |
capacity |
|
crew |
|
length ft |
|
manufacturer | |
related |
|
type |
|
has abstract |
|
avionics |
|
climb rate ftmin |
|
climb rate note |
|
cruise speed kts |
|
empty weight lb |
|
eng1 hp |
|
eng1 name | |
eng1 number |
|
eng1 type |
|
length in |
|
max takeoff weight lb |
|
range nmi |
|
prov:wasDerivedFrom | |
page length (characters) of wiki page |
|
manufacturer | |
origin | |
foaf:isPrimaryTopicOf | |
is Link from a Wikipage to another Wikipage of | |
is Wikipage redirect of | |
is foaf:primaryTopic of |