Albatros L 57

The Albatros L 57 was an early monoplane. It was a project for an airliner but was never completed, and as such never entered production. The top covering of the fuselage is swept up higher as compared to other similar planes of the era. The plane was designed to have up to six passengers.

Specifications

Engine: Mercedes D.IIIa
Length: 10.42 meters
Height: 3.55 meters
Span: 14.20 meters
Wing Area: 34.50 meters²
Weights: Empty: 1036 kilograms; Flying Weight: 1850 kilograms
Max. speed at sea level: 149 km/h
Cruising Speed at Sea Level: 120 km/h
Ceiling: 3450 meters
Range on full tank: 540 km^[1]

References

^ "Aircraft template". www.histaviation.com. Retrieved 2021-11-25.

Albatros aircraft

Early aircraft

Military Idflieg
designations

B type unarmed reconnaissance biplanes	B.I B.II B.III
C type armed reconnaissance biplanes	C.I C.II C.III C.IV C.V C.VI C.VII C.VIIII N C.IX C.X C.XI C.XII C.XIII C.XIV C.XV
D type Doppeldecker fighters	D.I D.II D.III D.IV D.V D.VI D.VII D.VIII D.IX D.X D.XI D.XII D.XIII D.XIV D.XV
Dr type Dreidecker triplane fighters	Dr.I Dr.II
G type Grossflugzeug bombers	G.I G.II G.III G.IV
J type close support	J.I J.II J.III

Company
designations

Landflugzeug (Landplanes)	LDD L.1 L.2 L.3 L.4 L.5 L.6 L.7 L.8 L.9 L.10 L.11 L.12 L.13 L.14 L.15 L.16 L.17 L.18 L.19 L.20 L.21 L.22 L.23 L.24 L.25 L.26 L.27 L.28 L.29 L.30 L.31 L.32 L.33 L.34 L.35 L.36 L.37 L.38 L.39 L.40 L.41 L.42 L.43 L.44 L.45 L.46 L.47 L.48 L.49 L.50 L.51 L.52 L.53 L.54 L.55 L.56 L.57 L.58 L.59 L.60 L.65 L.66 L.67 L.68 L.69 L.70 L.71 L.72 L.73 L.74 L.75 L.76 L.77 L.78 L.79 L.80 L.81 L.82 L.83 L.84 L.100 L.101 L.102 L.103
Wasserflugzeug (Seaplanes)	W.1 W.2 W.3 W.4 W.5 W.8 WMZ
Höhenflugzeug (High Altitude)	H.1

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Specifications

References