About: Beechcraft CT-134 Musketeer

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About: Beechcraft CT-134 Musketeer Sponge Permalink

An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

The Beechcraft CT-134 Musketeer was a military training derivative of the Musketeer built by Beechcraft for the Canadian Forces. The CT-134 was a single engine, low-wing, four-seat light aircraft with fixed landing gear and a limited aerobatic capability.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	Beechcraft CT-134 Musketeer
rdfs:comment	The Beechcraft CT-134 Musketeer was a military training derivative of the Musketeer built by Beechcraft for the Canadian Forces. The CT-134 was a single engine, low-wing, four-seat light aircraft with fixed landing gear and a limited aerobatic capability.
sameAs	dbr:Beechcraft_CT-134_Musketeer
dcterms:subject	dbkwik:resource/FUwnXua-41_8iqKSDDJhpQ== dbkwik:resource/iMlwGhmMJJV362ccAvHqRg== dbkwik:resource/bXBXYgXgObp71YEJ8-MWYA== dbkwik:resource/16CrkSnZXhGeS76iRaLr2Q==
foaf:homepage	http://www.airforce.forces.gc.ca/v2/equip/hst/musketeer-eng.asp
dbkwik:military/pr...iPageUsesTemplate	dbkwik:resource/AaGpNMKXeCEx6k1ovZIRVg== dbkwik:resource/ZbtrzLFw6TNwE1208cbZTA== dbkwik:resource/pTEKXoXwy_QJD-cbbKl3EQ== dbkwik:resource/8c65HClsHBgkxfJdWXaRHw== dbkwik:resource/cbsrEQx1xy51eXd2rIQtLg== dbkwik:resource/WFXNScnUbLW0ms-nET7UKA== dbkwik:resource/u1wPeCPbPjINuBoAqXRPqQ== dbkwik:resource/7_dwHHF8FUA3XhGjI4-8Fw==
max takeoff weight alt	1110(xsd:integer)
airfoil	NACA 63A415
climb rate main	880.0
number of props	1(xsd:integer)
length alt	7.85 m
span main	998.22
power/mass alt	8(xsd:double)
height alt	2.50 m
Introduced	1971(xsd:integer)
primary user	Canadian Forces
Type	Basic trainer
type of prop	air-cooled, 4-cylinder piston engine
loading main	16(xsd:double)
range alt	1257.0
length main	25(xsd:integer)
power alt	136.0
area main	146.0
power main	180.0
height main	8(xsd:integer)
span alt	10.00 m
range main	675.0
Manufacturer	Beech Aircraft Corporation
max speed main	124(xsd:integer)
engine (prop)	Lycoming O-360-A4G
power/mass main	13(xsd:double)
Capacity	2(xsd:integer)
climb rate alt	268(xsd:integer)
ceiling main	13000.0
National Origin	United States
empty weight main	1560.0
Developed From	dbkwik:resource/eKViKyGKbcTtyfGWjMPBSQ==
area alt	13.6
max speed alt	231.0
jet or prop?	prop
never exceed speed alt	283.0
loading alt	82(xsd:integer)
empty weight alt	707.0
plane or copter?	plane
ceiling alt	3,962 m
max takeoff weight main	2450(xsd:integer)
Retired	1992(xsd:integer)
never exceed speed main	152(xsd:integer)
Crew	Student and instructor
Number Built	48(xsd:integer)
ref	C-12-134-000/MC-000 Operating Checklist Musketeer CT 134, CFTMPC, 10 Jul 79
abstract	The Beechcraft CT-134 Musketeer was a military training derivative of the Musketeer built by Beechcraft for the Canadian Forces. The CT-134 was a single engine, low-wing, four-seat light aircraft with fixed landing gear and a limited aerobatic capability.

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