SAI KZ II
Template:Short description Template:Infobox aircraft
The SAI KZ II was a sport aircraft built in Denmark in 1937, produced in three major versions before and after the Second World War.
Design and development
In its original form, designated the Kupé (Danish: "Coupé") it was a low-wing cantilever monoplane of conventional design with fixed tailwheel undercarriage and two seats side by side under an enclosed canopy. The fuselage structure was of steel tube, skinned in plywood and fabric, and the wings were wooden with plywood covering and could be folded back along the fuselage for transport and storage.
This was followed by the aerobatic KZ II Sport with a revised fuselage design, placing the two seats in separate open cockpits in tandem, and a dedicated military trainer version along the same lines, the KZ II Træner ("Trainer"). This latter type was first produced in 1946, as a step towards rebuilding Denmark's air force after the war. They remained in service until 1955, when nine examples were sold into private hands.
In 2008, an example of each variant (including the sole extant KZ II Sport) is preserved in the Danmarks Flymuseum.
Variants
- KZ II Kupé - original version with side-by-side seating under an enclosed canopy and de Havilland Gipsy Minor or Cirrus Minor engine (14 built)
- KZ II Sport - aerobatic version with tandem seating in open cockpits and Template:Cvt Hirth 504A engine (16 built)
- KZ II Træner - military trainer version similar to KZ II Sport with de Havilland Gipsy Major engine (15 built)
Operators
- Danish Navy - ordered 4 × KZ II Sport, but these were confiscated by Germany before delivery
- Danish Air Force - 15 × KZ II Træner operated between 1946 and 1955
Specifications (KZ II Træner)
Data from Jane's.[1]
General characteristics
- Crew: 2Template:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convert
- Fuel capacity: 110 L (29 US gal; 24 imp gal) in two tanks in the wing centre-sectionTemplate:Aircraft specs/convertTemplate:Aircraft specs/engTemplate:Aircraft specs/engTemplate:Aircraft specs/engTemplate:Aircraft specs/lengthTemplate:Aircraft specs/convert
- Propellers: 2-bladed wooden fixed-pitch airscrewTemplate:Aircraft specs/length
PerformanceTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/rangeTemplate:Aircraft specs/rangeTemplate:Aircraft specs/rangeTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convert
- Power/mass: Template:Cvt (normal); Template:Cvt (aerobatic)
- Take-off run: Template:Cvt
- Landing run: Template:Cvt
See also
Related lists
References
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- Page Module:Citation/CS1/styles.css has no content.Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 563.
- Page Module:Citation/CS1/styles.css has no content.Simpson, R. W. (1995). Airlife's General Aviation. Shrewsbury: Airlife Publishing. pp. 348–49.
- Danmarks Flymuseum page on the KZ II Kupé (in Danish)
- Danmarks Flymuseum page on the KZ II Sport (in Danish)
- Danmarks Flymuseum page on the KZ II Træner (in Danish)
- Уголок неба
- Specific
- ^ Page Module:Citation/CS1/styles.css has no content.Grey, C.G.; Bridgman, Leonard, eds. (1947). Jane's all the World's Aircraft 1947. London: Sampson Low, Marston & company, ltd. pp. 110c–111c.
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