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LOIRE 210

 


Technical Specifications
Type
Bomber medium four-seat with median wings and retractable landing gear
Date first flight
March 21, 1935
Wingspan
11.79 m 
Lenght
9.51 m 
Height
3.80 m 
Wing Area
20.30 m2 
Empty Weight
1440 Kg 
Max. Takeoff Weight
2100 Kg 
Cruising Speed
199 km/h. 
Maximum Speed
315 km/h at 5000m 
Climbing Speed
4 000 m en 9’ 24” 
Service ceilling
8000m 
Range
750 kms
Crew
1 Men
Motorization
1 Radial Engine Hispano-suiza 9Vbs water cooled of 720 Hp 11
Armament
4 machine-gun Darne of 7.5mm iin the wings

 


Production

21 Loire 210 have been built since the date of the first flight on March 21, 1935.

To date, out of the 21 aircraft manufactured, 10 are listed in the list below:


Historical

The rise of seaplanes onboard led to the idea of owning a floatplane able to protect French Fleet ships against enemy seaplanes.

From 1931, the future Admiral Lartigue publishes a note, in this sense. This will culminate in 1933, on an official program to provide the Naval Aeronautics with a Catapultable Fighting Seaplane. One of the technical requirements was the use of the Hispano-suiza 9V radial engine of 700cv, which is renowned for its reliability.

Four manufacturers have responded to the program: The company Dewoitine proposed a HD 502, derived from the D500, refused because maintaining the online engine of its terrestrial version. The Bernard 110 was dismissed because of the bankruptcy of the company. The Potez 453, considered unstable at takeoff at sea, was also rejected. The Romano company proposed a biplane R90, also not selected for a lack of stability at sea. The Loire Company presented the Loire 210, which, responding well to the program, won the competition.

The Loire 210 made its first flight on March 21, 1935. The aircraft is healthy and its performances are considered correct. Its piloting is easy, and it passes all the program of classic aerobatics. His catapulting is easy and his behavior at sea is good. Trials end in the fall of 1935.

The company Loire, however, studied a version equipped with a Gnome and Rhône K14 engine more powerful and diameter smaller, so more aerodynamic. The aircraft, designated Loire 211, reached 330 km / h, but was not retained by Naval Aviation.

An order for 20 aircrafs is passed on May 12, 1937. But the development of the prototypes will be long and the assembly of the series models will be several delayed to incorporate modifications. When the first aircrafts arrive finally in unit, they will be already exceeded. The Loire 210 will be delivered between November 1938 and September 1939. 21 units are built and equip squadrons HC1 (Dunkerque Strasbourg) and HC2 (Richelieu and Jean Bart) from August 1939.

The aircraft was therefore catapultable and was recovered after its mission via a crane along the ship. This recovery maneuver, long, could be particularly delicate if the sea was not calm. An original solution was tested: the ship had a wide notched ramp at the stern of the ship, which was to allow the pilot of the aircraft to land at the rear of the boat, and come and grab his floats on the carpet before being put back on board after tilting the ramp!

However, the career of Loire 210 was short. The aircraft experienced some accidents that will put an end to its use. Thus, on October 17, 1939, the Loire 210 piloted by Lieutenant (Navy) Ziegler, commander of the HC1, breaks in flight during an aerobatic session. The pilot parachutes himself and is safe and sound, but the investigation will reveal, on some other aircraft in the unit, cracks on the main spar of the wing .. The technical services decide in November 1939, the withdrawal of the service of all the Loire 210 and thus the dissolution of the Escadrille HC1.


Versions

The Loire 210 has only been produced in one version


Bibliography

No books known for this aircraft


Photos Album

 


Drawing 3 views

Links to Website
"French Air Force"