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Albatros L 100

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L 100

General information
Type	Sports plane
Manufacturer	Albatros Flugzeugwerke
Number built	1
History
First flight	1930

TheAlbatros L 100 was a lightaircraft built inGermany to compete in the Europarundflug air race. It was a low-wing bracedmonoplane of conventionaltaildragger configuration.

Specifications (L 100)

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General characteristics

Crew: one pilot
Capacity: 2 passengers
Length: 8.45 m (27 ft 9 in)
Wingspan: 12.15 m (39 ft 10 in)
Wing area: 20.0 m² (215 sq ft)
Empty weight: 455 kg (1,000 lb)
Gross weight: 805 kg (1,775 lb)
Powerplant: 1 ×Argus As 8 , 60 kW (80 hp)

Performance

Maximum speed: 147 km/h (92 mph, 80 kn)
Range: 800 km (500 mi, 430 nmi)
Service ceiling: 3,200 m (10,500 ft)

References

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Wikimedia Commons has media related toAlbatros L 100.

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

Albatros aircraft

Early aircraft

MilitaryIdflieg
designations

B type unarmed reconnaissance biplanes	B.I B.II B.III
C type armed reconnaissance biplanes	C.I C.I (OAW) C.II C.II (OAW) 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 typeDoppeldecker 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 typeDreidecker triplane fighters	Dr.I Dr.II
G typeGrossflugzeug 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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