Jump to content

Albatros L 60

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by Trialpears (talk | contribs) at 16:05, 21 July 2020 (Convert Template:Aerospecs to Template:Aircraft specs per Wikipedia:Templates for discussion/Log/2019 March 20#Template:Aerospecs (via WP:JWB)). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

L 60
Role Utility aircraft
Manufacturer Albatros Flugzeugwerke
First flight 1923
Produced 3

The Albatros L 60 was a two-seat German utility aircraft of the 1920s developed from the Albatros L 59. It was a single-engine low-wing cantilever monoplane with large, spatted undercarriage.

Specifications (L 60)

General characteristics

  • Crew: one pilot
  • Capacity: 1 passenger
  • Length: 5.40 m (17 ft 9 in)
  • Wingspan: 10.30 m (33 ft 9 in)
  • Height: 2.65 m (8 ft 8 in)
  • Wing area: 10.0 m2 (108 sq ft)
  • Empty weight: 369 kg (814 lb)
  • Gross weight: 600 kg (1,323 lb)
  • Powerplant: 1 × Siemens-Halske Sh 5 , 60 kW (80 hp)

Performance

  • Maximum speed: 165 km/h (100 mph, 87 kn)
  • Range: 400 km (250 mi, 220 nmi)
  • Service ceiling: 3,000 m (9,800 ft)
  • Rate of climb: 2.1 m/s (410 ft/min)

See also

References

  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 55.
  • German Aircraft between 1919–1945