PropertyValue
rdf:type
rdfs:label
  • SAI KZ X
rdfs:comment
  • {| |} The SAI KZ X was a light aircraft produced in Denmark for army co-operation duties in the early 1950s. It was a strut-braced, high-wing monoplane of conventional design with fixed tailwheel undercarriage and was derived from the KZ VII. Deliveries to the Danish Army commenced in 1952, but by the summer of that year, two had already crashed.
owl:sameAs
empty weight kg
  • 529
dcterms:subject
dbkwik:military/property/wikiPageUsesTemplate
range km
  • 800
ceiling ft
  • 14400
met or eng?
  • met
range miles
  • 500
eng1 type
gross weight kg
  • 860
length in
  • 4
primary user
Type
  • Observation aircraft
eng1 kW
  • 108
wing area sqft
  • 140
height m
  • 2.200000
Height in
  • 3
span m
  • 9.410000
Manufacturer
max speed kmh
  • 215
empty weight lb
  • 1160
Capacity
  • 3
ceiling m
  • 4400
length m
  • 6.500000
max speed mph
  • 134
National Origin
  • Denmark
length ft
  • 21
Height ft
  • 7
First Flight
  • 1951-09-29
span ft
  • 30
gross weight lb
  • 1890
span in
  • 11
wing area sqm
  • 13
Crew
  • One, pilot
Number Built
  • 12
eng1 hp
  • 145
eng1 number
  • 1
abstract
  • {| |} The SAI KZ X was a light aircraft produced in Denmark for army co-operation duties in the early 1950s. It was a strut-braced, high-wing monoplane of conventional design with fixed tailwheel undercarriage and was derived from the KZ VII. Deliveries to the Danish Army commenced in 1952, but by the summer of that year, two had already crashed. The investigations of these crashes were conducted with technical assistance from Britain's Royal Aircraft Establishment, but no underlying defect in the aircraft design was uncovered and the KZ X was returned to service. However, when two more crashes took place in 1954, the type was withdrawn from service. Most KZ Xs were scrapped, with the only surviving example now in the Danmarks Flymuseum