Albatros Al 101

Al 101

Manufacturer: Albatros Flugzeugwerke
First flight: 1930
Number built: 71

The Albatros Al 101 was a German trainer aircraft of the 1930s. It was a parasol-wing monoplane of conventional configuration, and seated the pilot and instructor in separate, open cockpits.

Variants

L 101
L 101W - two examples built as floatplanes
L 101C
L 101D

Specifications (Al 101D)

General characteristics

Crew: two, pilot and instructor
Length: 8.45 m (27 ft 9 in)
Wingspan: 12.35 m (40 ft 6 in)
Height: 2.7 m (8 ft 10 in)
Wing area: 20.0 m² (215 ft²)
Empty weight: 475 kg (1,047 lb)
Loaded weight: 795 kg (1,753 lb)
Powerplant: 1x— Argus As 8 4-cylinder, water-cooled, inverted inline engine, 80 kW (110 hp)

Performance

Maximum speed: 170 km/h (110 mph)
Range: 670 km (420 mi)
Service ceiling: 3,600 m (11,800 ft)
Rate of climb: 4.2 m/s (830 ft/min)

Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. pp. 56.
German Aircraft between 1919-1945

Albatros Al 101 Pictures and Albatros Al 101 for Sale.

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Source: WikiPedia