- Albatros L 68
__NOTOC__ Infobox Aircraft
name=L 68 Alauda
caption=
type=Trainer
manufacturer=Albatros Flugzeugwerke
designer=
first flight=
introduced=
retired=
status=
primary user=
more users=
produced=
number built=18
variants with their own articles=The Albatros L 68 Alauda was a two-seat German
trainer aircraft of the 1920s. It was a single-enginebiplane of conventional configuration that seated the pilot and instructor in tandem, opencockpit s. The wings were of unequal span and had a pronounced stagger.Variants
* L 68 - original production version with
Siemens-Halske Sh 11 engine (3 built)
* L 68a - longer wingspan and Sh 12 engine (3 built)
* L 68c - main production version based on L 68a (10 built)
* L 68d -Siemens-Halske Sh.III engine (1 built)
* L 68e -Armstrong Siddeley Lynx engine (1 built)pecifications (L 68c)
aerospecs
met or eng?= metcrew=two, pilot and instructor
capacity=
length m=6.30
length ft=20
length in=8
span m=10.10
span ft=33
span in=2
dia m=
dia ft=
dia in=
height m=2.56
height ft=8
height in=5
wing area sqm=24.4
wing area sqft=263
rot area sqm=
rot area sqft=
aspect ratio=
empty weight kg=650
empty weight lb=1,430
gross weight kg=950
gross weight lb=2,090eng1 number=1
eng1 type=Siemens-Halske Sh 12
eng1 kw= 80
eng1 hp= 110
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=140
max speed mph=90
range km=360
range miles=220
endurance h=
endurance min=
ceiling m=4,200
ceiling ft=13,800
glide ratio=
climb rate ms=1.4
climb rate ftmin=270
sink rate ms=
sink rate ftmin=armament1=
armament2=
armament3=
armament4=
armament5=
armament6=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_68.html German Aircraft between 1919-1945]ee also
aircontent
related=
similar aircraft=
sequence=
L 65 -
L 66 -
L 67 -L 68 -
L 69 -
L 70 -
L 71lists=
see also=
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