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Albatros
/ Albatros AL 101
Albatros AL 101
The Albatros Al-101 was a 1930s German trainer aircraft.
It was a parasol wing monoplane of conventional configuration, the pilot and instructor sat in separate open cockpits.
Variants
L-101
Prototype aircraft,
L-101s
First serial modification with Argus As 8a engine,
Al-101d
Basic serial modification with Argus As 8a engine,
Al-101w
Float version of Al 101D.
Specifications
Crew
2
Length
8.5 m (27 ft 11 in)
Wingspan
12.5 m (41 ft 0 in)
Height
2.7 m (8 ft 10 in)
Wing area
20 m2 (220 sq ft)
Empty weight
515 kg (1,135 lb)
Gross weight
830 kg (1,830 lb)
Powerplant
1 × Argus As 8a, inverted 4-cyl air cooled inline piston engine,
73 kW (98 hp)
Performance
Maximum speed
171 km/h (106 mph, 92 kn)
Range
670 km (420 mi, 360 nmi)
Service ceiling
3,600 m (11,800 ft)
Rate of climb
4.2 m/s (830 ft/min)
Landing speed
70 km/h (43 mph).
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