PropertyValue
rdf:type
rdfs:label
  • ANBO I
rdfs:comment
  • {| |} The ANBO I was a single-seat aircraft developed in Lithuania as a trainer for the Army. It was a low-wing, braced monoplane of conventional tailwheel configuration. The fuselage structure was of fabric-covered welded steel tube, and the wing structure was of fabric-covered wood. The first flight took place in 1925. Ten years later the aircraft was sold to Lithuanian Aviation Museum in Kaunas where it is exhibited today.
owl:sameAs
empty weight kg
  • 190
dcterms:subject
dbkwik:military/property/wikiPageUsesTemplate
ceiling ft
  • 13800
climb rate ftmin
  • 550
met or eng?
  • met
eng1 type
  • Anzani radial engine
gross weight kg
  • 300
length in
  • 10
Type
  • Prototype trainer aircraft
eng1 kW
  • 26
wing area sqft
  • 123
span m
  • 10
climb rate ms
  • 2.800000
Manufacturer
max speed kmh
  • 142
empty weight lb
  • 420
ceiling m
  • 4200
length m
  • 5.750000
max speed mph
  • 89
length ft
  • 18
First Flight
  • 1925-07-14
span ft
  • 32
gross weight lb
  • 660
span in
  • 10
wing area sqm
  • 11.400000
Retired
  • 1935
Crew
  • one pilot
Number Built
  • 1
eng1 hp
  • 35
Designer
eng1 number
  • 1
abstract
  • {| |} The ANBO I was a single-seat aircraft developed in Lithuania as a trainer for the Army. It was a low-wing, braced monoplane of conventional tailwheel configuration. The fuselage structure was of fabric-covered welded steel tube, and the wing structure was of fabric-covered wood. The first flight took place in 1925. Ten years later the aircraft was sold to Lithuanian Aviation Museum in Kaunas where it is exhibited today.