Ensner Mk.1       

The Ensner Mk.1 was designed and built by F.G.Ensner, a member of the Thames Valley Gliding Club. A single-seat light sailplane built at West Drayton, Middlesex, UK.

It was built to carry out full scale tests of various aerofoil sections at low speeds. It was conventional wooden construction, with circular cross-section fuselage and parallel chord wing.

It was first flown from Fairey’s Great West Aerodrome on 26 June 1932. Only one was built and no C of A was issued.

Wing span: 7.62 m / 25 ft 0 in
Length: 4.11 m / 13 ft 6 in
Empty weight: 45.36 kg / 100 lb
Max L/D: 20

ENSAE Farfelu

The Farfelu is a two-seat training glider designed and being built at Toulouse by students of ENSAE – the Ecole Nationale Superieure de I’Aeronautique et de I’Espace. Instructor and pupil sit side by side under a one-piece canopy and the monocoque fuselage, of integrally stiffened epoxy/Nomex/epoxy sandwich construction, is built in two halves, the cockpit section tapering into a slimmer rear half carrying the tail; a metal box structure provides additional strength and reinforcement at the wing attachment points. The cantilever shoulder wings have single box spars and a laminated epoxy/Nomex/epoxy sandwich skin; there are Schempp-Hirth air brakes above and below each wing. The unswept cruciform tail unit is of similar construction to the wings, and there is a fixed monowheel in a small fairing and a tail bumper. The Farfelu prototype had not flown in 1955.

Span: 52 ft 6 in
Length: 25 ft 8 in
Wing area: 181.4 sqft
Aspect ratio: 15.19
Empty weight: 617 lb
Max weight: 1,102 lb
Min sinking speed: 2.50 ft/sec
Best glide ratio: 32:1

England 1922 Glider        

A single seat glider designed by E.C. Gordon England and built by George England (1922) Ltd, Walton-on-Thames, Surry, UK. Of wooden construction, only one was built, and flown in the 1922 Itford competitions, as No.13, by the designer, but it crashed during the stormy weather on 21 October 1922.

The undercarriage was twin mainwheels plus twin tail skids. The cantilever wings had no airbrakes or flaps.

The glider may have later been used at a gliding club at the RAF Staff College, Andover.

Wingspan: 8.58m / 28 ft 2 in
Length: 5.26m / 17 ft 3 in
Wing area: 12.08 sq.m / 130 sq.ft
Aspect ratio: 6
Empty weight: 45.36 kg / 100 lb
AUW: 117.94 kg / 260 lb
Wing loading: 9.76 kg/sq.m / 2.0 lb/sq.ft

Elsnic EL 2 M Sedy VLK

The history of the two-seater glider EL-2-M began in the early 1930s. At that time, Ludvík Elsnic, Slávek Rodovský, František Pešta, Jarmila Králová (since March 15, 1939 in Rodovská), Josef Horák, Mr. Vonráček and others met in the workshops of the gliding department of the then Masaryk Aviation League in Maniny in Prague, and debated the bad situation, in which the Czech gliding was in. The fleet is minimal, a few gliders and gliders of mostly German design, made in an amateur way, mostly without any support and any interest of the official authorities. In the end, all the discussions came to a clear conclusion: if you want to fly, build a glider yourself.

The situation gradually changed when the discussants heard that Walter was preparing an auxiliary aircraft engine for gliders. Then Slávek Rodovský stated that he could use his own funds to finance the construction of a glider. The nature of the meetings at Maniny changed, and the discussions took on a working character. At the beginning, it was decided on the type of glider, and the idea became a two-seater, allowing easy installation of the auxiliary engine.

At the last meeting on September 1, 1933, it was already clear that it would be a strut parasol with a seat for the passenger at the center of gravity and with the possibility of attaching an auxiliary engine to the console above the canopy. The original design provided for the engine version as the main one. Ludvík Elsnic based his own designs on the glider, which was named EL-2M. EL as Elsnic, 2 perhaps as Elsnic’s second design in order or more likely a two-seater aircraft, M as a motor. Construction according to the first drawings began on November 1, 1933.

The financial costs of the construction were reduced by items for wood and plywood, which were largely begged for by the architect Vavrouš. However, the rest of the material had to be paid for, which was mainly the concern of Slávek Rodovský. All visitors to the workshop in Maniny shared their work. As soon as he came, he immediately got a job, maybe just gluing the ribs. The new glider grew mostly out of the enthusiasm of the people who devoted all their free time to it. Josef Tláskal watched over the workshop design, all fittings were made by Josef Horák, and Pešta, Rodovský, Králová, Vondráček and others took part in the production of small parts. Despite the dedication of all the “builders” of the new glider, the construction took longer than expected, so that only on June 15, 1934, everyone could say “done!”. It was also decided at that time to name the prototype. He received an emblem in the form of a gray wolf’s head in a (probably) blue target on both sides and the inscription “Gray Wolf” below it. The originator of the name was the main sponsor of the construction, Slávek Rodovský, it was derived from the name of his scout unit.

Rodovský also flew the new prototype himself, the very next day, June 16, 1934. The first takeoff was made by pulling behind the car using a longer rope. On June 17, the flight continued with two aero tows. The EL-2M prototype flew for about 9 hours that day. After a whole month, tests of the new glider continued, during which the performance, dexterity and flight characteristics were determined. The gray wolf belonged to the category of aircraft that were said to have “succeeded”. This is evidenced by the fact that the measured performances (such as sagging) were slightly better than calculated. In the same way, the flight characteristics fully complied with the mission of the aircraft, which, according to the test report, could be flown at almost 25 km / h without stalling, while the wings were still sensitive. He let himself be forced into a stall, and he came out of it very soon. He willingly performed partial acrobatics. Based on these tests, the EL-2M glider was approved on 13 July 1934 by the commission of the then Ministry of Public Works of the Czech Republic for normal operation. Immediately afterwards, the glider was demonstrated by MLL gliders on an air show in Terezín, where it was transported by airlift. Later, the Gray Wolf took part in other events.

From the beginning, there was great interest in the Gray Wolf among the gliding community. Requests for drawing documentation only flocked to the headquarters of the then Masaryk Aviation League (hereinafter referred to as MLL). At the same time, the price of the documentation, including the license for one copy, was not at all low at the time, reaching CZK 650. Only a set of hull drawings cost 470 CZK. The first sets of drawings were sent to interested parties at the end of November 1934.

Meanwhile, the prototype underwent a “baptism” at the first gliding race in Raná in September 1934. The gray wolf was piloted on them by the designer Ludvík Elsnic. Soon after the start of the race during one of the first landings in the wet ground, he damaged the fuselage, repaired the next day, but the whole competition was successful. On September 6, for example, the time reached 1 hour and 15 minutes. He completed some competition flights with a passenger, for example, on September 6 with Jarmila Králová, he lasted 58 minutes in the air. EL-2M Gray Wolf was finally evaluated as the second-best glider of the competition after Zlín Z-VII Akéla.

Although Slávek Rodovský performed acrobatics on the Gray Wolf, the aircraft was not registered in the “acrobatic aircraft” category. Therefore, during 1935, a new calculation was made and the wing struts were strengthened. After this modification, on May 30, 1935, the glider was recognized by the Ministry of Public Works as fully capable of acrobatics in a single-seat class. It has been adopted by MLL clubs as a welcome extension of glider capabilities.

In February 1935, a prototype of the Gray Wolf underwent its first motorization in workshops in Maniny. It was equipped with an older motorcycle air-cooled two-cylinder engine Blackburn inverted V configuration with a declared power of less than 12 kW (16 hp). The engine was installed on a canopy on a small pyramid of tubular construction with a thrust propeller on a long shaft. An aerodynamically shaped petrol tank was mounted in front of the engine in one unit. The origin of the engine is not clear, it may have been an engine from the DH-53 aircraft (delivered to the Czech Republic in the 1920s from England) or once imported for the BH-16 prototypes. But even here he proved unsatisfactory. The first test flights of the Gray Wolf prototype with a big black six on the rudder took place at Raná in the second half of February 1935, but there was no question of success. During the first flight, the long shaft twisted, the propeller flew away and damaged the fuselage. Also other flights in Kbely in the period 23.3.- 7.4.1935, the longest of which did not exceed 15 minutes, did not go without problems. The engine did not run regularly, did not deliver the expected power and the long drive shaft caused great problems. Irregularities in operation could also be caused by overcooling the engine. During the tests in Kbely, it was started either with the help of a rubber rope or by stretching on the rope behind the car. Eventually, however, Blackburn was removed and in the summer the prototype continued to fly only as a motorless. It was not until November 1935 that the engine was reinstalled, but without success. At the beginning of 1936, the prototype of the Gray Wolf was exhibited at the sports aviation exhibition at the Prague Sample Fairs with Blackburn installed, but after the exhibition, the engine was definitively removed.

At about the same time, the prototype probably received instrumentation for the first time. Until then, it flew without any instruments, by the pilot’s feel and the occasionally tied strip of fabric on the wing strut. There is speculation as to whether the equipment was in connection with the motorization of the prototype, but the existing low-quality photographs from the tests on Raná rather exclude this. It is not known what were installed, as no clear photograph or written or drawing document has yet been found to show this. Some photos of the prototype show a “pitotka” on the upper part of the bow and an unidentified “alarm clock”. There is also a short film shot of the prototype Gray Wolf behind the “brandy” at Raná from 1935, which shows a special aerodynamic cover from above on the fuselage in front of the front cockpit in the form of an opaque plate or pyramid. It can be deduced that its only purpose was to cover a set of instruments that did not fit inside the fuselage.

At the beginning of 1935, 7 EL-2Ms were flying. One of them was also item no. 5, called DINKA and built in early 1935 in Náchod.

“Gray Wolf”, which was the name used for all built two-seater EL-2M, served in MLL clubs throughout the country. At the end of April 1935, Slávek Rodovský and his prototype took part in the first national Štefánik glider races in Banská Štiavnica. He then tested the gliding terrain near Žilina, where he flew for more than three hours in two takeoffs. The first woman in the Czech Republic, Jarmila Králová, passed the “C” test on the prototype EL-2M on May 14, 1935. The same glider was at the second gliding races on Raná in July 1935 and reached the highest elevation of all competitors after the start with a rubber rope: 625m. The glider was often used for its pleasant flight characteristics to verify new gliding terrain, for example in October 1935 in the Iron Mountains, etc. It was also flown in winter, which required a considerable dose of self-denial and warm clothing as the cabin was open. The performance of Jarmila Králové with Rodovský on January 12, 1936 in Raná, when she reached the then longest flight of a two-seater two-seater in the Czech Republic in the length of 4 hours and 11 minutes, arouses respect even today. In this context, it should be noted that the normal time of all flights of Gray Wolf gliders was most often in the order of minutes at that time, and only a few individuals knew about the possibilities of thermal flying.

There was a fatal injury to the pilot of the Gray Wolf, rtm. Bedřich Chovanec which destroy the prototype. It was May 7, when the tow rope near the village of Světlá nad Sázavou broke during the aero towing from Prague to Olomouc. Both aircraft landed safely in an emergency, the tow plane was piloted by the then Sergeant František Peřina, later a famous fighter war pilot. After repairing the tow rope, both planes took off to continue the flight. During the start at a height of about 50 m, however, the left and right wing of the Gray Wolf was torn off. The hull crashed. The pilot was seriously injured and died after being transported to a hospital in Německý (now Havlíčkův Brod). The cause of the disaster was allegedly the high speed of the lift at the start and a sudden unexpected gust of wind.

The EL-2M is an all-wood two-seater glider of the “parasol” type with a canopy wing made of metal tubes, of which the visible ones are profiled either by a wooden body or are made of special tubes of teardrop-shaped cross-section. With the help of four permanent pin holders on the back of the canopy, it is possible to install an auxiliary motor with a traction or thruster propeller about above the center of gravity.

The wing is divided, with two main and three auxiliary beams. Each half of the wing consists of 23 ribs with a G 633 profile and 20 ribs (semi-ribs – only the upper part). The wing is fastened to the canopy made of metal tubes with a diameter of 20 mm by means of pins, each half is supported by a tubular profiled V-shaped strut. The plywood also covers the root part of the wing up to the third rib, and further strengthens the cover at the tenth rib, from which the aileron begins. It also strengthens the end arch of the wing. The other upholstery material is air canvas. The aileron is designed in a similar way, the plywood mainly covers and connects the second and third auxiliary beam. The plywood also forms a profiled cover of the entire tubular canopy. The hexagonal cross-section is a lattice structure with a plywood cover, consisting of twelve hull partitions. The hinges for the rudder and the height stabilizer are attached to the latter. According to the construction documentation, the diagonal reinforcements of the plywood cover are between the second and sixth fuselage bulkheads, some amateur builders applied them to the entire fuselage, which is evident from the photos. The cockpit is open, normally without a protective plate, only with the lining of the edge of the hole. In at least one case, however, there was also a version with an amateur-made and installed covered cabin of the “Kränichov” type, which is evidenced by existing photographs of the Gray Wolf operated somewhere in Slovakia (the author saw it, but did not obtain it). The rear seat is exactly in the center of gravity, which allows the glider to operate as a single-seater. Access to the rear seat is quite difficult, the passenger must stretch backwards from the front seat after opening the roof door on the top of the cockpit between the front and rear seats and after folding down the front seat backrest. The instrumentation was not a standard accessory for the Gray Wolves. If the gliders were equipped with devices, then the additional installations were always not documented and can be seen from only a few photographs. Foot and manual control is a double cable, guided by the fuselage.

The landing gear consists of a simple ash rail underlain by three rubber blocks, two of which are under the cockpit under the fourth bulkhead. At the end of the fuselage under the keel (from the eleventh to the twelfth fuselage bulkhead) it is complemented by a steel spring spur. The prototype documentation is hand-drawn variants, which Ings. At the bow of the fuselage is a sling for a rubber starting rope, it was also used for aero tows and autostartes. For some specimens it was a simple steel hook, for others it was a device similar to today.
Tail surfaces. The elevator stabilizer with a span of 3.5 m is a simple construction with one beam, covered with plywood thickness. 1.2 mm. It is attached to the fuselage by inserting the beam into the exact cutout in the twelfth fuselage bulkhead and securing with pins to the fittings on the eleventh bulkhead. It is reinforced by a pair of struts to the keel. The double-girder elevator is suspended rotatably at five points, it is covered with canvas except for the parts covered with plywood formed by two beams and the inner part of the rudder. The keel firmly connected to the fuselage is completely covered with plywood. The rudder is partially aerodynamically balanced in the upper part, covered with plywood at the front and lower part, otherwise covered with canvas.

The gray wolf was built in Bratislava, Choceň, Náchod, Butovice, Užhorod, Plzeň, Slaný, Kutná Hora, Roudnice nad Labem, Humpolec, Stará Paka, Povážská Bystrica, Přibyslav, Mladá Boleslav. Boleslav, Adamov, Olomouc, Zlín, Velká Bytča and many other places. At the turn of 1931/32, the staff of the local military crew, Staff Captain Josef Koukolík, founded the local group of the Masaryk Aviation League (MLL), which focused on aircraft modelling. Some of its members soon became interested in gliding. Emil Seige and his friend Jaroslav Hauser (since 1947 Horský) became its pioneer and also instructor. For their work and hobby, they found an extraordinary understanding with the director of the State Vocational School of Wood, Ing. Augustine Puchta, who enabled them to build gliders and gliders in a school body shop under the expert guidance of teacher Josef Hartman. The first Zögling test glider was built at the school in 1933/34. Later, it was the turn of more structurally demanding gliders, aircraft “Přerov type I, II, III” by experienced designers Jan Hrbek and Ing. Elsnice. Finally, a two-seater glider EL-2M “Gray Wolf” was built here in the school’s workshop. At least ten copies of Gray Wolf were produced in Kralupy nad Vltavou by František Kochman. In the summer of 1936, about 25 new Gray Wolves were completed, and by then at least ten were flying.

Because not everywhere were suitable conditions for downhill flying with a rubber rope, which was the most common way of gliding at the time, and aero tows were expensive for many MLL gliding departments, cars were quite commonly used for take-offs. Costs also decreased in other ways. MLL gliders in Roudnice nad Labem, for example, delivered a new Gray Wolf in 1936, agreed with the Prague Gliding Department of the ARČS and operated flying in Kbely with aero tows.

The national gliding races were held for the first time in Slovakia, near Žilina. Among other types, three EL-2Ms competed there, all in the single-seater category. They were named “Straník” with pilot Ladislav Vaníček, “Šumava” with pilot Maňák and “Pelikán” with pilot Antonín Zrna. However, in the large field of more modern gliders, they did not succeed significantly. However, this did not reduce the interest in the Gray Wolves, as the need for a two-seater school with pleasant flight characteristics continued to grow. This is evidenced, among other things, by the production plan for another twenty of these gliders, compiled by the MLL headquarters for 1937. In that year, the EL-2M gliders flew as trainers’ throughout the country. They did not take part in the competitions very much, at the fourth national sailing competition in 1937 only one flew on Straník, with the name “Chalan”, from the MLL sailing department from Velká Bytča. Pilot Klein flew for the entire race for a total of 4 hours and 9 minutes and was evaluated as the best on the school glider.

In the year of 1938, other EL-2M gliders were built. They often flew in the program “1000 pilots republic” as a kind of voluntary prelude to subsequent motor training.

“Such training was completed, for example, by the legendary Slovak RAF fighter pilot Otto Smik, who allegedly fondly remembered it during the war.”

After the mobilization in May in 1938, the races at Straník near Žilina were abandoned and from 1 May to 19 June, the 5th MLL National Trade Union Competition was announced at Rané. The proposals allowed to compete at other airports and also only on Sundays. During this competition, quite a few accidents occurred at Rané. Among other things, A. Šubrt damaged the bow of the “Gray Wolf”. On Thursday, June 16, the President of the Republic, Dr. Edvard Beneš. M.j. was presented in flight the Humpolec motorized Gray Wolf and Rodovsky acrobatics on the Gö-1 “Falcon”.

In 1938 was the second catastrophe of thr EL-2M type. On Kozák on June 26, 1938, the Železný Brod glider Karel Peroutka died when his Gray Wolf lost speed while in a turn and crashed. The third victim of flying the EL-2M was Jaroslav Koula from Kerhanice nad Orlicí on September 11, 1938, after the Gray Wolf collided with the Grünau Baby glider. Jaroslav Valenta from Prague saved himself after the collision. It was the first and last victim on Rana before World War II. The attempt to fly on the slope at Vysoká u Německého, today Havlíčkův Brod in 1938, ended after the accident. The cases described were human fault, piloting error, so it had no effect on the popularity and use of other Gray Wolves. Other clouds rolled over their flying, clouds beginning in World War II. After the occupation in March 1939, these gliders flew “freely” only in Slovakia. The gliders were taken over by the German.

It is difficult to find out how many EL-2M gliders were actually built during the occupation of the republic in 1939. There is a photograph of the glider with a clearly visible serial number 31. However, it is not clear whether the serial numbers were assigned together with the sent set of production documentation or when the completed specimen was flown. The first option is more likely to apply. Pessimistic estimates of the number of actually built specimens are close to the number of 50 pieces, realistic approx. 55 – 60. It could mean that the Gray Wolf was probably the most widespread two-seater glider in Europe before World War II.

The second motorized “gray” was a glider built by the gliding (or, as it was also called at that time – the MLL sailing department) in Moravian Ostrava. There they used a new Walter Atom engine from 1935, a four-stroke flat air-cooled two-cylinder with an output of 18.5 to 21 kW (25 to 28 hp) at 2600 to 3000 rpm, a dry weight of 40 kg, a displacement of 1.1 liters and compression ratio 5.2: 1. It was reportedly installed with a thruster, but the photo shows an engine on a tubular pyramid above a canopy of a wing with a propeller. It was mainly used for training students of gliding who have already passed the “B” exam.

The most famous motorized Gray Wolf was “Humpolec I” from 1937. An active MLL branch has been operating in the town of the same name since 1934. It was created spontaneously after Ludvík Elsnice’s lecture on sport flying and non-motorized in particular, which was organized for the public by the local Sokol Committee in the spring of 1934. Members of the local branch of the MLL with instructor Mr. Karel Doubek began flying the glider in 1934. Later, they acquired another glider Zlín V and school glider “Kamarád”. In October 1936, the construction of the Gray Wolf began in the workshops of MLL Humpolec. It was to be motorized from the beginning. The members of the local branch decided to address the issue of engine location somewhat differently than the original design had envisaged. They installed the engine on the bow, not on the ready handles on the wing canopy. The designer of this change was Jiří Smrčka. It involved necessary modifications to the basic design of the EL-2M. The external dimensions of the glider have been retained, but the longitudinal members have been strengthened, diagonals have been added to the fuselage, the wing has been moved partially forward and both seats to the rear to maintain the center of gravity. The Walter Atom was placed on a tubular bed above the front of the fuselage. According to some sources, the fuel tank was located in the bow, but the photos from the flight show the location in the center of gravity between the seats for the pilot and the passenger.

Virtually all members of the then (and members!) MLL gliding department in Humpolec took part in the construction, the witnesses highly praise Mr. Karel Dvořák – carpenter and Mr. Stanislav Prokop – mechanical locksmith. According to records from the time of construction of the glider, approximately 1,800 hours were worked on its production and the total construction cost was CZK 24,000. The costs were largely covered by a subsidy from the Ministry of Public Works, which is not so surprising in this case, considering that the chairman of the local Humpolec branch of MLL was the then district governor, Mr. Jaromír Němeček.

The flight was carried out on 11 April 1937 by Ludvík Elsnic himself, while a load in the form of a 50 kg sandbag was placed on the second seat. The first start using a rubber rope with an engine running at full throttle took place on a small hill behind Humpolec between the roads to Jiřice and Brunka. There are a number of photos. Ludvík Elsnic was allegedly very satisfied with both the flight characteristics and the workshop design, as well as with the solution of placing the auxiliary engine on the bow. Many others flew after him the same day. Then the glider received a new “coat” with a large inscription “HUMPOLEC” on the fuselage and was ceremoniously baptized on Sunday, May 17, 1937 in Humpolec, surrounded by, among other things, gliders Zlín IV and Z-V and glider “Kamarád”. The ceremony began at 10:00 in the morning on the Upper Square. The protector of the baptism was Division General Ing. Jaroslav Fajfr, other guests were the famous pilot Maj. Hess, the then mayor of Humpolec, Jan Šimek, etc. The district governor, Mr. Jaromír Němeček, was present at the baptism as the chairman of the local branch of MLL. The baptism itself was performed by Mrs. Růžena Motejlová by placing a bouquet of flowers on the cabin of the glider. The “Atom” engine was also started demonstratively. Sergeant Motyčka demonstrated over the square in an Avia 122. An abridged audio recording of the entire baptism was broadcast on national radio the same afternoon. In addition to photographs from the baptism, there is reportedly an amateur film.

In mid-June 1937, together with other aircraft “Humpolec” was exhibited at the National Air Show in Prague, where it flew “along its axis” with the pilot L. Elsnic. After the show, he flew from Kbel Airport. It was flown back to Humpolec by the then leader of the MLL promotional squadron, Capt. Uncle. “Humpolec” flew, piloted by Mr. Smrčka, Rudolf Steyskal and others, and became quite popular in the republic. Even well-known gliders from Prague, such as Stejskal, Vahala and others, even came to Humpolec to fly a glider. Among other things, the well-known acrobatic pilot Sergeant Motyčka, a member of the acrobatic group Cpt. Fr.Novák.

In 1937, the Gray Wolf flew for about 30 hours without any problems. Even in 1938, “HUMPOLEC I” served the Humpolec without any problems. On June 16, 1938, this EL-2M was demonstrated at Rané to President Beneš, who visited the airport. At that time, the glider was already equipped with a windshield and the propeller received a spinner. It was part of the last gliding races on Raná before the war.

The use of the Humpolec motorized Gray Wolf in Czech hands was not ended until the occupation by Germany in 1939. The last flight in Czech hands was completed by “HUMPOLEC I” on March 13, 1939. The Germans came to Humpolec on March 16. They took the glider to the airport in Německý Brod and allegedly flew there until it was destroyed.

The plywood cover on the back of the fuselage is relatively weak, which in some modes allegedly caused the “tail” to twist imperceptibly, but this is not at the expense of safety. The minimum landing speed is about 40 km / h. For motorized versions, the flight characteristics depended on the load (mostly single-pilot engine versions flew, only in Moravská Ostrava it was used more regularly as a two-seater), engine power, propeller type and efficiency and, last but not least, weather, especially air temperature. The motorized versions all started with a rubber rope or autostart, they were not able to do so on their own.

The Walter Atom engine from “HUMPOLCE I” was discovered in Waltrovka in 1945 and returned to the Humpolec gliders. It was built into the prototype “HUMPOLEC II”, which was Pitrman’s second-hull. Construction of a two-seater motor glider with a thrust engine in the fuselage nacelle. The new glider was never completed.

Another motorized version was a copy of the Gray Wolf from MLL Lysá nad Labem. In 1938 they used a two-stroke inverted two-cylinder Pejšek JPK-20 (established in 1937 at the company Josef Pejšek Kralupy nad Vltavou) with an output of 15 kW (20 hp) at 1700 rpm. Again, it was a classic installation above the wing canopy. The engine was arranged as a push, the engine bed was designed as an aerodynamic cover with an integrated gas tank. The motorcycle worked reliably, according to period information, the glider climbed very well with it. In July 1938, pilot Jindřich Hnilička reached an altitude of 2800 m. By the end of 1938, this Gray Wolf allegedly flew for 21 hours to the complete satisfaction of its owners. However, the occupation in March 1939 also marked the end of his career.

The staff of the Aviation Museum in Kbely had been trying to get this glider into the collections since the beginning of the museum’s existence. They once received word that there was an unfinished copy of the Gray Wolf in Humpolec in the 1950s. However, it turned out that nothing of it had survived in the early 1970s.

In the spring of 1972, the museum staff established contact with the creator of the EL-2M, Ludvík Elsnic. As a witness to the beginnings of our sailing, he handed over a number of rare photographs and other documents to the museum. Of course, there was also talk of the Gray Wolf. “Then I’ll come on Thursday and describe the negatives!” said goodbye once as he left the museum. And on Thursday, August 9, 1972, he came. He was carrying a package in his armpit. “My mistress has such a good memory! I mentioned the Gray Wolf at home, and she says: You, Ludvík, there are some drawings in the attic! And they were.”

Several months have passed. In mid-October 1972, two museum workers went to Slovakia to search for the Avia C-2 aircraft. Unsuccessfully. The road also took them to Trenčín. And when they were in Trenčín, they went to see “Uncle” Kralovič, a well-known Slovak aeroclub glider. Coincidentally, the existence of the Gray Wolf’s drawings was mentioned. “Send them to me, I’ll see what they think could be done. I promised you something to do in the museum anyway,” Anton Kralovič offered. And so at the end of October, the drawings of the Gray Wolf came to Trenčín. In November 1972, a rudder, wing ribs, fuselage bulkheads, etc. began to be built in the Kralovič apartment.

Gradually, word spread among the “air people” that a Gray Wolf was being built in Trenčín. Perhaps this also contributed to the phone ringing in the Kbel Museum in mid-January 1973. Called Pavel Vančura, then editor of the Aviation and Cosmonautics magazine.

“His colleague Luděk Štětka from the World of Engines editorial office, looking at photos of old gliders, including the Gray Wolf, said that his uncle had a similar plane at home in the attic.” The reaction of the museum staff was quite normal. In cooperation with the L + K editorial office, they set out to verify this track as soon as possible. On January 25, 1973, the search party headed to the address: Josef Duben, Lipí u Náchoda. But no one was home at the address given. Mr. Duben worked part-time on the ski lift. Fortunately, the searchers discovered his wife, and she willingly let the “guests” into the ground. “There really were wings of an old glider, but the fuselage was missing. To a timid question, whether somewhere by chance…. Mrs. Dubn replied, “Yes, there is something else in the shed, we wanted to burn it!”

To everyone’s delight, it was really the hull of the Gray Wolf! Nobody even expected such a successful completion of the search operation. Even Anton Kralovič did not want to trust the telegram to stop the construction of the replica that the original Gray Wolf had been found. Until he received an invitation to take over the “wolf” for repairs, he lived in fear that he had fallen victim to a bad joke.

And so, on February 9, 1973, L. Elsnic, Anton Kralovič, the editors of L + K and the staff of the Aviation Museum met in Lipí u Náchoda with Mr. Josef Dubn. Josef Duben donated the EL-2M glider. However, it was characteristic of Czech conditions that he had previously offered a glider to the then National Technical Museum, and that did not even answer him. Individual parts of the glider left their hiding places in the attic and shed in Lipí, moved to the back of a truck, and traveled to Trenčín at night. Another was already the work of a group of enthusiasts from the Trenčín Aeroclub led by Anton Kralovič. It was necessary to peel off all coatings, repair ribs and partitions, then coat everything again and finish the surface treatment. Some newly made parts according to drawings by Ludvík Elsnice were used, such as a rudder, but many parts were additional. However, no one was in a bad mood, the Gray Wolf was, and it was original! After six months of intensive work after working hours, on Saturdays and Sundays, the repair of Gray Wolf No. 5 was completed. Anton Kralovič never admitted it, but witnesses claim that he “jumped” into the air with the repaired Gray Wolf before his transfer to Prague. The glider was transported to Kbel on August 9, 1973. He spent nineteen days folded in an exhibition on the ground, then was definitively assembled and hung under the ceiling of the hall. It left this place only once, when moving to the newly opened hall – a hangar of the Wagner type, in which the museum exhibits aircraft focused on the period 1918 – 1938.

A search of the history of the preserved Gray Wolf specimen gradually revealed that this was indeed the fifth piece produced. It was completed at the beginning of 1935 (some sources speak only of 1936, but Mr. Duben insisted on 1935, which would correspond to the assigned serial number) from the funds of the local group MLL in Náchod. He was given the name “Dinka” (bears them on the bow) after the then necessary patron, who paid a quarter of all expenses. “Two young boys from Letov” came twice everywhere to supervise the construction. According to Josef Dubn, Mr. Bergman from Náchod also indirectly helped in the construction, giving the sailors free to eat at the time. Even the money saved in this way went to the construction of the glider.

It is not known today where the fifth Gray Wolf specimen flew. Among other things, it took off in Hradec Králové with the help of autostartes at the military training ground, Na Žďárkách, in the vicinity of Náchod and elsewhere. Surprisingly, it flew the most in the winter, as in the summer the local farmers levied charges for destroying the grass. “Šeďas” flew to the full satisfaction of the local MLL gliding unit until the war. With the arrival of the Nazis, it “disappeared” and spent the entire war in the double wall of Mr. Dubn’s barn. It flew again after the war, but only sporadically. Witnesses recalled that, probably due to the unretained coating of the upholstery canvas, its glide on the slope was significantly lower than that of the Grünau Baby flying at the same time. The last time it flew on May 1, 1949, it was actually black. It flew 10 minutes on the slope, and it was probably the last ten minutes in the history of this glider, if we disregard his unconfirmed jump after the repair in Trenčín in 1973.

In the summer of 2005 Ing. Ivo Pujman (from Beroun) looked into possibilities to finish a replica of this glider, which he and his friend Josef Dlouhy began building.

Span: 13.5 m
Length: 6.8 m
Wing chord: 1.36 m
Wing area: 18 sq.m
Elevator span: 3.5 m
Empty weight: 130 kg
Flight weight: 200 – 330 kg
Wing load: 11.1 – 18.33 kg / sq.m
Min. descent 1 person: 0.95 m / s
Min. descent 2 person: 1.3 m / s

EL-2M Humpolec
Empty weight with fuel: 200 kg
Take-off weight with fuel max: 340 kg
Climb: 1 – 2 m / s
Cruise speed: 100 km / h

EL-2M from MLL Lysá nad Labem
Ceiling: 2800 m
Consumption: 7 l / hour of flight

EoN Olympia 4 / Olympia 402 / Olympia 403 / Olympia 409 / Olympia 415 / Olympia 419

The first three marks of Olympia, which formed the bulk of the production of this type, differed little from the DPS Meise, but in the 1950s Elliotts began development of a new family of high performance Olympia variants
incorporating laminar flow wings, and leading to the Olympia 419, which was sufficiently different from the first three marks of this design as to be almost a new type.

First of these new variants was the Olympia 4, later known as the 401, first flying in 1954, which was a Mk 2, G-ALNF, fitted with a laminar flow wing of NACA 64-series section, identical in span (15m) and plan form to the previous wing. The 401 had a revised fuselage nose section, square-cut rudders and elevators. Frise ailerons were featured but these were found to have only marginal power at low speeds and, after the 401’s debut in the 1954 World Gliding Championships, these were enlarged and the wing itself modified. G-ALNF was then fitted with a 17m span wing of the same aerofoil sections at root and tip, thus becoming the Olympia 402; aileron chord and span were increased. It was flown by Bill Ivans of the USA into fifth place in the 1956 World Championships, but was lost in an accident on the last day of the competition.

For the 1956 World Championships the Olympia 4 prototype was converted to 17 m / 55 ft 3.5 in as the Olympia 402.

The Olympia 4 / 401 was succeeded by the Olympia 403 prototype, G-APEW, which retained the 17m span wing with a slightly thickened root but introduced some important design changes; this made its debut at the 1957 British national championships. The tail surfaces were entirely redesigned with increased area, the tailplane now being an all-moving surface which could be hinged upwards for transport. It had an anti-balance and trimming tab which at first covered the full span but was later reduced to half span. The fuselage was extended 10in forward by inserting an extra bay between the main bulkhead and the cockpit, and both the cockpit canopy and fuselage ‘neck’ were widened, that part of the fuselage under the wing being redesigned. The first flight of the 403 was in 1957.

The 403 was subsequently fitted with type 419 tailplane.

The next variant was the Olympia 419, which had the wing span increased to 18.9m (62ft), longer span Frise ailerons, a slightly longer nose than the 403 and greater rudder area, these changes giving better low speed performance and tailplane balance than the 403. The NACA 64-series laminar flow wing section was used. The 419 was constructed mainly of spruce, and all surfaces were covered by birch ply except for the rudder, tailplane and wings inboard of the ailerons. Balsa wood was used extensively as a filling for the wing ribs and as a non-structural material for wing tips and fairings.

The undercarriage consisted of a jettisonable twin wheel main unit and a tailskid, and the main landing skid under the forward fuselage was of stainless steel. Both the Olympia 419 prototype and the Olympia 415, which was a 15m span version of it, first flew in 1958; the latter did not go into production but the 419 was marketed at a price of £2,150 and in the end eight were built. These put up some good performances in both World and British National championships flown by such pilots as Nicholas Goodhart and Peter Scott.

On the 419X there was a main skid only, with droppable wheels.

The Olympia 415 was the Standard Class version of the 419, with reduced wing span. The first flight of the prototype was on 27 April 1958.

Variants:

EoN Type 5 Olympia 4
New wing section
Wingspan: 15.0 m / 49 ft 2 in
Length: 7.27 m / 23 ft 10 in
Wing area: 15.33 sq.m / 165 sq.ft
Aspect ratio: 15
Wing section: NACA 64,3 618 root / 64,4 421
Empty weight: 204.12 kg / 450 lb
AUW: 322.0 kg / 710 lb
Max L/D: 36

EoN Type 5 Olympia 401
Revised 4, with new nose and square-cut empennage. 180 mm (7 in) shorter.
Wingspan: 15.0 m / 49 ft 2 in
Length: 7.09 m / 23 ft 3 in
Wing area: 15.33 sq.m / 165 sq.ft
Aspect ratio: 15
Wing section: NACA 64,3 618 root / 64,4 421
Empty weight: 204.12 kg / 450 lb
AUW: 322.0 kg / 710 lb
Max L/D: 36

EoN Type 5 Olympia 402
As 4, modified for 1956 World Gliding Championships with 17.0 m (55 ft 3.5 in) span.
Wingspan: 17.0 m / 55 ft 3.5 in
Length: 7.27 m / 23 ft 10 in
Wing area: 15.33 sq.m / 165 sq.ft
Wing section: NACA 64,3 618 root / 64,4 421
Empty weight: 204.12 kg / 450 lb
AUW: 322.0 kg / 710 lb
Max L/D: 36

EoN Type 6 Olympia 403
1957 development of Olympia 402, with strengthened and shortened fuselage (7.47 m (24 ft 6 in). New fin and rudder, all moving tailplane.

Eon Type 6 Olympia 415
1958 Standard class (15.0 m (49 ft 3 in)) span version of 419.
Span: 49 ft 3 in / 15.0 m
Length: 24 ft 6 in / 7.47 m
Wing area: 161 sq.ft / 14.95 sq.m
Aspect ratio: 15
Empty weight: 550 lb / 250 kg
Max weight: 820 lb / 372 kg
Wing loading: 22.6 kg/sq.m / 4.3 lb/sq.ft
Min sinking speed: 1.84 ft/sec at 46 mph
Best glide ratio: 35:1 at 52 mph

Eon Type 6 Olympia 419 / 419X
Long span, long fuselage version of 403.
Span: 62 ft 0 in / 18.9 m
Length: 25 ft 6 in / 7.77 m
Wing area: 186 sq.ft / 17.28 sq.m
Aspect ratio: 19.9
Empty weight: 606 lb / 275 kg
Max weight: 900 lb / 408 kg
Wing loading: 21 kg/sq.m / 4.3 lb/sq.ft
Min sinking speed: 1.84 ft/sec at 46 mph
Best glide ratio: 38:1 at 52 mph

EoN 463
Span: 49 ft 2.5 in / 15.0 m
Length: 21 ft 0 in / 6.4 m
Height: 5ft 8 in
Wing area: 132 sqft / 12.26 sq.m
Aspect ratio: 18.0
Wing section: NACA 643618/421
Empty weight: 400 lb / 181 kg
Max weight: 630 lb / 286 kg
Water ballast: None
Max wing loading: 23.33 kg/sq.m / 4.78 lb/sq ft
Max speed: 136 mph / 117.5 kt / 218 km/h (in smooth air)
Max rough air speed: 74 kt / 137 km/h
Stalling speed: 30 kt / 56 km/h
Min sinking speed: 2.2 ft/sec / 0.67 m/sec at 42.5 mph / 37 kt / 69 km/h
Best glide ratio: 32:1 at 48 mph / 42 kt / 78 km/h

Olympia 4
Type 6 Olympia 403
Olympia 419
Olynpia 463

EoN 10 Olympia / Chilton Olympia

Chilton Olympia

Just after the war, when sporting gliding was getting started again, it was evident that there would be a need for new sailplanes to supplement the surviving prewar ones, and to fill the gap until such time as postwar designs could go into production it was a logical step to build some of the best German prewar designs, some captured examples of which had been brought to Britain, in British factories.

A combination of a desire to make use pre-war glider experience and refusal by the Board of Trade to allow Elliotts to return to its prewar furniture-making activities led to a decision to enter glider manufacturing, starting with the production of an improved version of the well known DPS Meise known as the Olympia. The Olympia’s heritage goes back to when Hans Jacob’s glider won the contest to design a standard glider for the 1940 Helsinki Olympic Games (hence the Olympia name). Elliotts of Newbury took up the production of an internally modified version of this glider after the war, with the first example flying in mid January 1947.

This was originally to have been built in Britain by Chilton Aircraft Co Ltd, makers of the prewar DW1 ultralight, but after building a prototype, first flying in January 1947, Chilton disposed of the manufacturing and sales rights and associated drawings to Elliotts in 1952.

An initial production batch of 100 was started; the type soon proved to be popular with private owners and clubs, also being exported to a number of countries.

A single-seat sailplane of conventional wooden construction, Elliots improved and developed version of the Chilton Olympia, The Olympie 1 had no flaps, but airbrakes were fitted. The undercarriage was the main skid, plus tail skid. The prototype had its first flight at White Waltham on 17 January 1947, and the price in 1947 was £495.

The Olympia was built in three versions differing only in the landing gear; the Mk 1 had a central steel-sheathed ash skid under the forward fuselage very similar to the Meise’s, while the Olympia 2 had a built-in fixed central monowheel and the Mk 3 had a jettisonable dolly wheel landing gear.

A one-piece quickly detachable bubble canopy for the pilot with a sliding ventilation and clear-vision panel on the port side replaced the Meise’s framed canopy, and there was an aerobatic harness and provision for a back-type parachute.

Otherwise the Olympia is very similar to the Meise; the high cantilever wings are of wooden construction with plywood and fabric covering, with D-spars in the leading edge and DPS air brakes, while the wooden ailerons are fabric-covered. The all-wooden monocoque fuselage has a luggage compartment under the wing root with an access door on the port side. The tail unit is of wooden construction with plywood and fabric covering, and there is a trim tab in the starboard elevator. Price of the Olympia 2 in 1960 was £850.

Six Olympia gliders were built by Fokker under licence.

Olympia 1
Wingspan: 15.0 m / 49 ft 2 in
Length: 7.27 m / 23 ft 10 in
Wing area: 15.33 sq.m / 165 sq.ft
Aspect ratio: 15
Wing section: Gottingen 549 root / 676 tip
Empty weight: 204.12 kg / 450 lb
AUW: 303.9 kg / 670 lb
Wing loading: 20 kg/sq.m / 4.09 lb/sq.ft
Max L/D: 25
Min sink: 0.67 m/sec at 63 kph / 2.2 ft/sec at 39 mph

Olympia Mk.II
Span: 49 ft 2.5 in
Length: 21 ft 5 in
Wing area: 161.5 sq.ft
Aspect ratio: 15.0
Empty weight: 430 lb
Max weight: 670 lb
Max speed: 129 mph
Min sinking speed: 2.2 ft/sec at 39 mph
Best glide ratio: 25:1 at 45 mph

Olympia 2B
Wing span: 15.0 m (49 ft 2.5 in)
Length: 6.61 m (21 ft 8 in)
Wing area: 15.0 sq.m (161.5 sq ft)
Wing section: Gottingen 549/676
Aspect ratio: 15.0
Empty weight: 195 kg (430 lb)
Max weight: 304 kg (670 lb)
Water ballast: None
Max wing loading: 20.27 kg/sq.m (4.15 lb/sq.ft)
Max speed: 112 kt (208 km/h)
Stalling speed: 27 kt (50 km/h)
Min sinking speed: 0.67 m (2.2 ft)/sec at 34 kt (63 km/h)
Max rough air speed: 69 kt (128 km/h)
Best glide ratio: 25 at 39 kt (72.5 km/h)

EoN 460 / EoN 463 / EoN 460/463 / Elliotts AP/10 / EoN 465

EoN 460

Intended as a Standard Class 15m span single-seater to replace the popular Olympia, the EoN 463, also known as the EoN 460/463, was the production version of the EoN 460 and incorporated the design experience and certain features of the laminar flow Olympia variants, especially the Olympia 403 and 419.

The EoN 460, or Elliotts AP/10 Type 460 as it was also known, first flew in prototype form on 26 April 1960 and only the five prototype 460s were built; the first had an aspect ratio of 20 and an all-up weight of 600 lb, the second and third had an aspect ratio of 18 and an all-up weight of 630 lb, the fourth was the same as the first but with a modified one-piece canopy and the fifth prototype was the same as the fourth but had modified outer wing sections. The tail unit was very similar to the Olympia 419’s and, as on the latter, the tailplane could be folded upwards for transport. The shoulder wings were set slightly lower than the Olympia’s and the centre and forward fuselage were similar to the Olympia 419’s, while the same NACA 64-series laminar flow wing section as on the 419 was used.

The Type 10 C EoN 460 was fitted with a modified cockpit canopy. The Type D was as the Type C but with modified sections to the outer wing. All types were fitted with folding tailplanes and the wings have Frise type ailerons.

The production versions of the EoN 460 were known as the EoN 460/463. They wee as the 460 Type D but with an aspect ratio of 18, and an AUW of 286 kg / 630 lb.

The production EoN 463 first flew in April 1963 and a total of 48 were built; this was practically the same as the fifth prototype 460, with an aspect ratio of 18 and an all-up weight of 630lb. The fabric and stringer top fuselage fairing of the 460 was now replaced by a glassfibre one on the 463, which also had a glassfibre instead of plywood nose section and a new cockpit canopy.

Both the 460 and 463 have wooden wings with light alloy spars, plywood-skinned and with overall fabric covering; the wings are similar to the Olympia 419’s except for the reduced span, the Frise ailerons being fabriccovered and the DFS-type air brakes of plywood. The fuselage, like the 460’s, is a wooden Warren girder type structure with plywood covering and a glassfibre rear fairing. The tail unit is a conventional fabric-covered wooden structure and the tailplane, unlike the all-moving surface of the Olympia 403 and 419, reverts to conventional elevators with a trim tab in the starboard one. There is a fixed unsprung mono-wheel with an internal expanding brake, and a tailwheel. The pilot’s canopy has direct vision panels and a demister, and oxygen and radio can be fitted if desired.

The 463 was followed by the EoN 465, developed for the 1965 World Championships, only two of these being built, the first one, the Series 1, making its maiden flight on 8 March 1965. The 465 had the fuselage height reduced and the pilot seated in a reclining position to reduce cross sectional area and hence drag; the main landing gear skid was deleted and the monowheel centre raised. An all-moving tailplane was reintroduced which did not fold up for storage. Pendulum sealed ailerons were fitted. The EoN 465 Series 1 had an all-up weight of 680lb and the second one, known as the Series 2, had a thinner wing section than the Series 1 and a strengthened main spar; its all-up weight was 700lb and wing area was increased to 140sq ft.

The 465 Srs.1 first flew in March 1965 and the Srs.2 in April 1965.

Following the death of Elliott’s managing director, Mr H. C. G. Buckingham, in the summer of 1965 the firm’s board of directors, after reviewing the situation, decided to end glider production due to its increasing unprofitability.

EoN 465

Type 10 EoN 460 Type A
Wingspan: 15.0 m / 49 ft 2 in
Length: 6.4 m / 21 ft 0 in
Wing area: 11.15 sq.m / 120 sq.ft
Aspect ratio: 20
Wing section: NACA 64,3,618 root / NACA 64,4,421 tip
Empty weight: 159.21 kg / 351 lb
AUW: 272 kg
Max speed: 215 kph / 134 mph
Aerotow speed: 152 kph / 95 mph

Type 10 EoN 460 Type B
Wingspan: 15.0 m / 49 ft 2 in
Length: 6.4 m / 21 ft 0 in
Wing area: 11.15 sq.m / 120 sq.ft
Aspect ratio: 18
Wing section: NACA 64,3,618 root / NACA 64,4,421 tip
Empty weight: 159.21 kg / 351 lb
AUW: 286 kg
Max speed: 215 kph / 134 mph
Aerotow speed: 152 kph / 95 mph

EoN 463
Span: 49 ft 2.5 in / 15.0 m
Length: 21 ft 0 in / 6.4 m
Height: 5ft 8 in
Wing area: 132 sqft / 12.26 sq.m
Aspect ratio: 18.0
Wing section: NACA 643618/421
Empty weight: 400 lb / 181 kg
Max weight: 630 lb / 286 kg
Water ballast: None
Max wing loading: 23.33 kg/sq.m / 4.78 lb/sq ft
Max speed: 136 mph / 117.5 kt / 218 km/h (in smooth air)
Max rough air speed: 74 kt / 137 km/h
Stalling speed: 30 kt / 56 km/h
Min sinking speed: 2.2 ft/sec / 0.67 m/sec at 42.5 mph / 37 kt / 69 km/h
Best glide ratio: 32:1 at 48 mph / 42 kt / 78 km/h

EoN 465 Srs.1
Span: 49 ft 2.5 in / 15.0 m
Length: 21 ft 2 in / 6.45 m
Height: 5ft 8 in
Wing area: 132 sqft / 12.26 sq.m
Aspect ratio: 18.0
Wing section: NACA 643618/421
Empty weight: 400 lb / 181 kg
Max weight: 680 lb / 308.44 kg
Water ballast: None
Max wing loading: 23.33 kg/sq.m / 4.78 lb/sq ft
Max speed: 136 mph / 117.5 kt / 218 km/h (in smooth air)
Max rough air speed: 74 kt / 137 km/h
Stalling speed: 30 kt / 56 km/h
Min sinking speed: 2.2 ft/sec / 0.67 m/sec at 42.5 mph / 37 kt / 69 km/h
Best glide ratio: 32:1 at 48 mph / 42 kt / 78 km/h

EoN 465 Srs.2
Span: 49 ft 2.5 in / 15.0 m
Length: 21 ft 2 in / 6.45 m
Height: 5ft 8 in
Wing area: 132 sqft / 12.26 sq.m
Aspect ratio: 18.0
Wing section: NACA 643618/421
Empty weight: 400 lb / 181 kg
Max weight: 700 lb / 317.52 kg
Water ballast: None
Max wing loading: 23.33 kg/sq.m / 4.78 lb/sq ft
Max speed: 136 mph / 117.5 kt / 218 km/h (in smooth air)
Max rough air speed: 74 kt / 137 km/h
Stalling speed: 30 kt / 56 km/h
Min sinking speed: 2.2 ft/sec / 0.67 m/sec at 42.5 mph / 37 kt / 69 km/h
Best glide ratio: 32:1 at 48 mph / 42 kt / 78 km/h

Type 10 EoN 460
EoN 460/465

Elliots of Newbury Eon Type 9 / Kendall Crabpot / Kendall K.1

The initial version, known as the Crabpot, was designed by H. Kendall for the 1947 B.G.A. Two-seat Sailplane Competition. Conventional wooden construction, apart from the wings which had several spanwise webs and few ribs. The webs were 15mm thick, and the ribs were spaced at from 900 to 1200 mm pitch.

A cantilever wing, no flaps but airbrakes were fitted. All moving tailplane.

A project only, it won the competition.

Having one the competition, the Crabpot was re-designed. The wing section was altered, a “V” tail introduced, and the fuselage shortened. The wing material was altered and it was decided to manufacture it using an asbestos reinforced low pressure thermos setting plastic structure, a method that involved the use of heated concrete moulds and tailored felts. The wing was manufactured by F.G. Miles Ltd at Redhill Aerodrome, under the designation Miles M.76, but when tested, it broke up at a fraction of the design load. The K.1, as the Crabpot was by then known, was later built, using the traditional wooden construction methods, by Elliots of Newbury, as the EoN Type 9.

Only one was built, the first flight being at Lasham in March 1954, with full span ailerons. No CofA was issued as the K.1 was abandoned due to unsatisfactory flying characteristics, particularly unsolvable spinning problems.

Kendall Crabpot / K.1
Wingspan: 18.3 m / 60 ft 0 in
Length: 8.24 m / 27 ft 0 in
Wing area: 18.58 sq.m / 200 sq.ft
Aspect ratio: 18
Wing section: NACA 43018 root, NACA 43012A tip
Empty weight: 232 kg / 516 lb
AUW: 414 kg / 911 lb
Wing loading: 21.0 kg/sq.m / 4.3 lb/sq.ft
Max L/D: 27 at 77 kph / 49 mph

EoN Type 9
Wingspan: 18.3 m / 60 ft 0 in
Length: 7.01 m / 23 ft 0 in
Wing area: 18.58 sq.m / 200 sq.ft
Aspect ratio: 18
Wing section: NACA 66,3,418, NACA 64,2,415 tip
Empty weight: 300 kg / 661.5 lb
AUW: 453.6 kg / 1000 lb
Max speed: 200 kph / 125 mph
Stall: 64 kph / 40 mph
Max L/D: 35

EoN AP.7 / EoN Primary / EoN Eton

Elliott AP.7 EoN Primary

The EoN Primary, or Elliotts AP/7 Primary EoN as it is known in full, is a more modern but essentially very similar version of the Dagling/SlingsbyT-3 Primary and SG 38 formula of the 1930s for a simple single-seater basic training glider.

The prototype made its first flight in February 1948, and the first production model flew in April that year; the type was used not only by clubs but by the Air Training Corps and Combined Cadet Force under the service name of Eton TX Mk 1 to replace the Daglings previously used for Cadet instruction. It could also be supplied with a static training stand which acted as a simple flight simulator in which the glider was balanced on a pivot and wind forces assisted the trainee pilot to get the feel of the controls.

The constant chord wooden wing is wire-braced and has a high lift section of 12% thickness/chord ratio; it has a plywood leading edge and fabric covering, with fabric-covered wooden ailerons. Plywood leading edge spoilers are featured for use during ground-slides only. The fuselage is a flat wooden open girder-type structure supported by a horizontal beam with the landing skid underneath, with sprung compression legs; the pilot has a single open seat with minimum controls. Unlike the Dagling and Slingsby Primary, the EoN design did not have the option of a nacelle to provide some protection for the pilot. The tail unit is of fabric covered wooden construction and strut and wire braced, effective fin area being provided by filling in part of the open rear fuselage in front of the rudder.

EoN Primary

Production of the EoN Primary ended in 1958 after 80 had been built, but a number of these were still at Elliotts’ works at Newbury ready for final assembly in the spring of 1965, not long before Elliotts ceased all glider production.

Span: 34 ft 0 in 10.36 m
Length: 20 ft 6 in / 6.25 m
Height: 8 ft 0 in
Wing area: 180 sqft / 16.72 sq.m
Aspect ratio: 6.0
Empty weight: 250 lb / 113 kg
Max weight: 490 lb / 222 kg
Wing loading: 2.8 lb/sq.ft / 13.7 kg/sq.m
Max speed: 73 mph / 117 kph
Max aero-tow speed: 54 mph / 87 kph
Stalling speed: 27 mph / 43.5 kph
Max L/D: 8

Elliots of Newbury (EoN)

Elliots of Newbury grew out of an old-established joinery works that had existed oa a part of the Albert Works, Newbury, Berkshire site since the mid-nineteenth century. After the 1914-18 wat a change to furniture manufacture was made. During the Second World War Elliots became involved with glider manufacture, one of a number of furniture manufacturers that co-operated in the building of the large transport gliders. Elliots built about one third of the total Horsa production including the development of the hinged nose for the Mark 2 version, and it was also responsible for powered version of the Hamilcar glider. However, Elliots prime interest was the making of furniture. At the end of the war, when the contracts for transport gliders were coming to an end, the firm was hoping to resume furniture manufacture but, for technical reasons, was not “designated” by the Board of Trade for the manufacture of “Utility” furniture.

Early in 1945 the company was approached by Chilton Aircraft Ltd to make one pair of wings for the Chilton Olympia. Elliots had, by then, already planned to manufacture the Newbury Eon four-seat light aircraft but they agreed to make one pair of wings only for the Chilton prototype. Elliots refused to sell Chilton’s the wing jigs and maintained legal rights and ownership of their own manufactured jigs. Chilton’s later gave up all aircraft work and an agreement was subsequently reached whereby Elliots purchased from Chilton the production rights, fuselage jigs, and work in hand on all Olympia sailplanes.

Quantity production of the Eon Olympia commenced in 1946, and was followed in 1948 by the production of two further ex-German designs, the Grunau Baby sailplane and the SG.38 primary glider. Elliots, and their design consultants Aviation & Engineering Products Ltd, introduced improvements in each of the designs before commencing production.

Meanwhile, the Newbury Eon aircraft had its first flight in August 1947, and, in conjunction with their consultants, they produced a Design Study and tendered to the Air Ministry specification T.16/48 for a two-seat training aircraft in competition with Percival, Handley Page, and Auster. No further aircraft were produced by Elliots but aircraft parts were made, under sub-contract.

In 1954 a new version of the Olympia was produced as the original design was nearly fifteen years old. The Olympia 4, later known as the 401, was the first in a series of gradual stages of improvement and led to the 402 in 1956, the 403 in 1957, and finally, in 1958, to the Open Class 419 with its companion the 415 for the fifteen-metre Standard Class. Limited production of these latter types was then initiated. A completely new Standard Class sailplane was introduced in 1961 known as the Type 460. This was put into production and became very popular in Britain, resulting in a special version, the Type 465, being developed for the 1965 World Championships.

In the summer of 1965 the Managing Director of Elliots, M H.C.G. Buckingham died. He had been a keen supporter of the gliding movement for many years. After his death Elliots carried out a review of the firm’s activities and decided that it was time to end glider production due to its increasing unprofitability. A joint advertisement in the April 1966 “Sailplane & Gliding” announced that Slingsby Sailplanes Ltd had taken over the production of Eon Sailplanes. However, no Elliots designed gliders were ever built at Kirkbymoorside although spares were supplied and repairs undertaken.