Lioré et Olivier LeO 21

Lioré et Olivier LeO 21

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The Lioré et Olivier LeO 21 was a 1920s French biplane airliner and later military transport based on the earlier LeO 20 night bomber.

Development

First flown in August 1929 the LeO 21 was a twin-engined biplane airliner with a fixed tailskid landing gear. It retained the basic structure of the LéO 20 night bomber but with a new wider fuselage. It had room for six passengers in a nose cabin and a further 12 passengers in the main cabin with an open cockpit for the pilot.

The second LéO 21 was fitted with two 450hp (336kW) Renault 12Ja engines and re-designated as a LeO 212, it was converted by the Wagons-Lits company as a "dining aircraft". The first LéO 21 became an avion-bar in 1929 and was re-designated LeO 211, it was later modified in 1931 with Renaul engines as the LeO 213. One aircraft was produced as the LeO 21S fitted as a 10-stretcher ambulance. The first production LeO 213 was built in 1928 and a total of eleven were built and operated on routes from Paris to London, Lyons, Marseilles and Geneva. The LeO 213 had an increased wingspan, improved sound proofing and three baggage holds. When modified for night services they were re-designated as LeO 213N. In 1934 all the surviving LeO 213s were bought by the French Air Force and were converted to transports for 14-troops on bench seats and re-designated LeO 214.

Variants

;LeO 21:Prototype;LeO 21S:Air ambulance, one built.;LeO 211:First prototype modified;LeO 212:Second prototype fitted with two 450hp (336kW) Renault 12Ja engines. ;LeO 213:Production version with Renault engines, some redesignated LéO 213N for night use.;LeO 214:Military conversions from LéO 213 for the French Air Force.

Operators

;FRA

pecifications (LeO 214)

aerospecs
ref= [Orbis 1985, page 2332]
met or eng?= met

crew=1
capacity=14 troops
length m=15.55
length ft=51
length in=0¼
span m=23.03
span ft=75
span in=6¾
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=4.50
height ft=14
height in=9¼
wing area sqm=108
wing area sqft=1162.54
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=3440
empty weight lb=7584
gross weight kg=5700
gross weight lb=12566
lift kg=
lift lb=

eng1 number=2
eng1 type=Renault 12Ja V-12 piston engines
eng1 kw= 336
eng1 hp= 450
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=190
max speed mph=118
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=560
range miles=348
endurance h=
endurance min=
ceiling m=4500
ceiling ft=14765
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
armament2=
armament3=
armament4=
armament5=
armament6=

ee also

aircontent
see also=
related=
*Lioré et Olivier LeO 20
similar aircraft=
sequence=
lists=
*List of military aircraft of France

References

*
*cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=|pages=


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