The Pazmany PL-4A is a single-seat, single-engine sport aircraft developed in the United States and first flown in 1972. It is marketed for homebuilding from plans, and 686 sets had sold by 1985. The PL-4A is a conventional, low-wing cantilever monoplane with an enclosed cabin and fixed, tailwheel undercarriage. The design features a T-tail, chosen to facilitate folding the wings. Construction throughout is of metal, using standard extruded sections for the longerons and pop rivets as the basic fastener. The standard powerplant is a Volkswagen air-cooled engine of 60 hp (45 kW) Construction time is estimated to be around 1,000–1,500 hours.
Property | Value |
---|---|
dbo:abstract |
|
dbo:designer | |
dbo:manufacturer | |
dbo:type | |
dbo:wikiPageExternalLink | |
dbo:wikiPageID |
|
dbo:wikiPageLength |
|
dbo:wikiPageRevisionID |
|
dbo:wikiPageWikiLink |
|
dbp:ceilingFt |
|
dbp:ceilingM |
|
dbp:climbRateFtmin |
|
dbp:climbRateMs |
|
dbp:crew |
|
dbp:designer | |
dbp:emptyWeightKg |
|
dbp:emptyWeightLb |
|
dbp:eng1Hp |
|
dbp:eng1Kw |
|
dbp:eng1Name |
|
dbp:eng1Number |
|
dbp:firstFlight |
|
dbp:grossWeightKg |
|
dbp:grossWeightLb |
|
dbp:heightFt |
|
dbp:heightIn |
|
dbp:heightM |
|
dbp:lengthFt |
|
dbp:lengthIn |
|
dbp:lengthM |
|
dbp:manufacturer | |
dbp:maxSpeedKmh |
|
dbp:maxSpeedMph |
|
dbp:nationalOrigin |
|
dbp:numberBuilt |
|
dbp:primeUnits?_ |
|
dbp:rangeKm |
|
dbp:rangeMiles |
|
dbp:ref |
|
dbp:spanFt |
|
dbp:spanIn |
|
dbp:spanM |
|
dbp:type | |
dbp:wikiPageUsesTemplate | |
dbp:wingAreaSqft |
|
dbp:wingAreaSqm |
|
dcterms:subject | |
gold:hypernym | |
rdf:type |
|
rdfs:comment |
|
rdfs:label |
|
owl:sameAs | |
prov:wasDerivedFrom | |
foaf:isPrimaryTopicOf | |
is dbo:wikiPageDisambiguates of | |
is dbo:wikiPageRedirects of | |
is dbo:wikiPageWikiLink of | |
is foaf:primaryTopic of |