Lioré et Olivier LeO 25
|Manufacturer||Lioré et Olivier|
The Lioré et Olivier LeO 25 was a bomber aircraft produced in France in the late 1920s.
Design and development
The LeO 25 was a development of the LeO 20 and retained much of that aircraft's structure, adding a new tail and liquid-cooled engines. The prototype was delivered to the Aéronautique Militaire amongst a batch of LeO 20s in 1928 for evaluation. This was redesignated LeO 252 in 1929 after an engine change, and a second, generally similar machine was purchased by Romania.
In 1931, the LeO 252 remaining in France was fitted with wooden floats and handed over to the Aéronavale, forming the pattern for the majority of LeO 25s which would be produced as seaplanes. The only other members of the family to be built with wheeled undercarriage were three LeO 253s purchased by Brazil in 1931, and which would see service in the Constitutionalist Revolution the following year, and the sole LeO 255 which would later be fitted with floats. This latter machine was equipped with supercharged engines and was used to set a number of height-with-load records for seaplanes.
The only versions produced in quantity were the LeO H-257bis and LeO H-258, which together represented orders for 86 units from the Aéronavale. Entering service in June 1935, they flew neutrality patrols during the Spanish Civil War and some remained in service at the outbreak of the Second World War. These surviving aircraft flew convoy escort and anti-submarine patrols in September 1939 before being used as tactical bombers against land targets during the Blitzkrieg, suffering heavy losses. Fifty-three remained on strength with Vichy forces in August 1940, and these were used for secondary roles such as training and target towing until 1944.
- LeO 25 - landplane night bomber with Hispano-Suiza 12Hb engines (1 prototype)
- LeO 252 - landplane bomber with Hispano-Suiza 12Mbr engines (1 built, one converted from LeO 25)
- LeO 253 - landplane bomber similar to LeO 252 (3 built)
- LeO H-254 - dedicated seaplane version of LeO 252 (2 built)
- LeO H-255 - record-setting version of LeO H-254 with supercharged Hispano-Suiza 12Xbrs engines (1 built)
- LeO H-256 - version of H-254 with extended wingspan (1 built)
- LeO H-257 - modified version for Aéronavale with Gnome-Rhône 14Kbrs engines and enclosed cockpit for pilot (1 built)
- LeO H-258 - interim version similar to H-257bis but with Hispano-Suiza 12Nbr engines, supplied to Aéronavale while H-257bis production was being undertaken (26 built)
- LeO 259 - version with Hispano-Suiza 12Ydrs / Hispano-Suiza 12Yfrs engines (1 built)
- Brazilian Air Force - 3 × LeO 253
- Armée de l'Air
- Royal Romanian Air Force - 1 × LeO 252
Specifications (LeO H-257bis)
- Crew: 5
- Length: 17.54 m (57 ft 7 in)
- Wingspan: 25.5 m (83 ft 8 in)
- Height: 6.8 m (22 ft 4 in)
- Wing area: 133.5 m2 (1,437 sq ft)
- Empty weight: 5,300 kg (11,684 lb)
- Gross weight: 9,560 kg (21,076 lb)
- Powerplant: 1 × Gnome-Rhône 14Knrs 14-cyl. air-cooled radial piston engine, 650 kW (870 hp)
- Powerplant: 1 × Gnome-Rhône 14Kors 14-cyl. air-cooled radial piston engine, 650 kW (870 hp) (opposite rotation to 14Knrs)
- Maximum speed: 230 km/h (143 mph; 124 kn)
- Range: 1,500 km (932 mi; 810 nmi)
- Service ceiling: 8,000 m (26,000 ft)
- Related lists
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 579.
- World Aircraft Information Files File 900 Sheet 08. London: Bright Star Publishing.
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 580.
|Wikimedia Commons has media related to Lioré et Olivier LeO 25.|
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
- World Aircraft Information Files. London: Bright Star Publishing.