Albatros L 60

__NOTOC__ Infobox Aircraft
name=L 60


caption=
type=Utility aircraft
manufacturer=Albatros Flugzeugwerke
designer=
first flight=1923
introduced=
retired=
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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.

pecifications (L 60)

aerospecs
met or eng?= met

crew=one pilot
capacity=1 passenger
length m=5.40
length ft=17
length in=9
span m=10.30
span ft=33
span in=9
dia m=
dia ft=
dia in=
height m=2.65
height ft=8
height in=8
wing area sqm=10.0
wing area sqft=108
rot area sqm=
rot area sqft=
aspect ratio=
empty weight kg=369
empty weight lb=814
gross weight kg=600
gross weight lb=1,323

eng1 number=1
eng1 type=Siemens-Halske Sh 5
eng1 kw= 60
eng1 hp= 80
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=

max speed kmh=165
max speed mph=100
range km=400
range miles=250
endurance h=
endurance min=
ceiling m=3,000
ceiling ft=9,800
glide ratio=
climb rate ms=2.1
climb rate ftmin=410
sink rate ms=
sink rate ftmin=

armament1=
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References

* cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation
year=1989 |publisher=Studio Editions |location=London |pages=55
* [http://www.histaviation.com/Albatros_L_60.html German Aircraft between 1919-1945]

ee also

aircontent

related=

similar aircraft=

sequence=
L 57 -
L 58 -
L 59 - L 60 -
L 65 -
L 66 -
L 67

lists=

see also=