About: LAPAN XT-400

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An Entity of Type : umbel-rc:Model_airplane, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
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The LAPAN XT-400, (Lembaga Penerbangan dan Antariksa Nasional - National Institute of Aeronautics and Space), was a twin-engine STOL utility aircraft under development by the government of Indonesia in the late 1970s into the early 1980s. The programme was cancelled without the prototype having been completed or flown. It was to have provided passenger and cargo transport from rough and unprepared fields, with secondary roles as an aerial survey platform and air ambulance.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:Abstraction100002137 yago:Act100030358 yago:Activity100407535 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Event100029378 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 yago:Work100575741 yago:YagoPermanentlyLocatedEntity aircraft yago:Type105840188 yago:Undertaking100795720 yago:WikicatAbandonedCivilAircraftProjects umbel-rc:Model_airplane
rdfs:label	LAPAN XT-400 (en)
rdfs:comment	The LAPAN XT-400, (Lembaga Penerbangan dan Antariksa Nasional - National Institute of Aeronautics and Space), was a twin-engine STOL utility aircraft under development by the government of Indonesia in the late 1970s into the early 1980s. The programme was cancelled without the prototype having been completed or flown. It was to have provided passenger and cargo transport from rough and unprepared fields, with secondary roles as an aerial survey platform and air ambulance. (en)
dcterms:subject	LAPAN aircraft High-wing aircraft Abandoned civil aircraft projects Twin piston-engined tractor aircraft
Wikipage page ID	19340323 (xsd:integer)
Wikipage revision ID	969673702 (xsd:integer)
Link from a Wikipage to another Wikipage	LAPAN aircraft Britten-Norman Islander High-wing aircraft Abandoned civil aircraft projects Twin piston-engined tractor aircraft LAPAN Lycoming IO-540
sameAs	LAPAN XT-400 LAPAN XT-400 LAPAN XT-400 LAPAN XT-400
span ft	47 (xsd:integer)
span in	11 (xsd:integer)
span m	14.590000 (xsd:double)
wing area sqft	273 (xsd:integer)
wing area sqm	25.400000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Cite_book dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:primeUnits%3F_	met (en)
national origin	Indonesia (en)
capacity	seven passengers (en)
crew	one pilot (en)
height ft	14 (xsd:integer)
height in	1 (xsd:integer)
length ft	33 (xsd:integer)
manufacturer	LAPAN
status	Abandoned project (en)
type	Utility aircraft (en)
has abstract	The LAPAN XT-400, (Lembaga Penerbangan dan Antariksa Nasional - National Institute of Aeronautics and Space), was a twin-engine STOL utility aircraft under development by the government of Indonesia in the late 1970s into the early 1980s. The programme was cancelled without the prototype having been completed or flown. It was to have provided passenger and cargo transport from rough and unprepared fields, with secondary roles as an aerial survey platform and air ambulance. The design itself was that of a conventional, strut-braced, high-wing monoplane, similar in general appearance to the Britten-Norman Islander, but with an upswept rear fuselage to provide for clamshell cargo doors underneath the tail. The main units of the fixed, tricycle undercarriage were carried on short stub-wings on the lower fuselage, which also provided the attachment points for the wing struts. This arrangement allowed the fuselage to maintain a rectangular cross-section along its length without landing gear components or attachment points intruding into the cargo space. The original design was for an eight-seat aircraft, but a follow-on version with 12 seats was anticipated. Had it flown, the XT-400 would have been the first aircraft of Indonesian design to carry more than three people. Construction throughout was of metal. Work on the prototype commenced in 1977, with a first flight anticipated in 1980. This however did not transpire, and the XT-400 project was cancelled in 1981 with the prototype still unfinished. (en)
ceiling ft	15300 (xsd:integer)
ceiling m	4665 (xsd:integer)
empty weight kg	1422 (xsd:integer)
empty weight lb	3136 (xsd:integer)
eng1 hp	250 (xsd:integer)
eng1 kw	187 (xsd:integer)
eng1 name	Lycoming IO-540C (en)
eng1 number	2 (xsd:integer)
gross weight kg	2540 (xsd:integer)
gross weight lb	5600 (xsd:integer)
height m	4.300000 (xsd:double)
length in	6 (xsd:integer)
length m	10.200000 (xsd:double)
max speed kmh	273 (xsd:integer)
max speed mph	170 (xsd:integer)
range km	965 (xsd:integer)
range miles	600 (xsd:integer)
gold:hypernym	Aircraft
prov:wasDerivedFrom	wikipedia-en:LAPAN_XT-400?oldid=969673702&ns=0
page length (characters) of wiki page	3663 (xsd:nonNegativeInteger)
manufacturer	LAPAN
foaf:isPrimaryTopicOf	wikipedia-en:LAPAN_XT-400
is Link from a Wikipage to another Wikipage of	List of aircraft (La–Lh) National Institute of Aeronautics and Space Lapan XT-400
is Wikipage redirect of	Lapan XT-400
is foaf:primaryTopic of	wikipedia-en:LAPAN_XT-400

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