A.Jackson Avro Aircraft since 1908 (Putnam)
Avro 531 Spider
First flown at Hamble in April 1918, the Spider was an unsponsored private venture single seat fighter in which many Avro 504K components were used for speed of manufacture. To this end a shortened rear fuselage of conventional construction with spruce longerons was married to a standard Avro 504K front fuselage and the engine was a' borrowed' 110 h.p. Le Rhone. There seems little doubt that the Avro company hoped that the Spider would replace the single seat Avro 504K night fighter in the Home Defence Squadrons. To simplify rigging (a time consuming operation not acceptable to squadrons in the field) all flying and landing wires were replaced by very rigid welded steel Warren girder interplane bracing. This comprised six faired steel tubes arranged in three inverted triangles on each side, anchored to the main spars of the upper mainplane and to the front spar of the lower. Ailerons were fitted only to the upper wing, the lower being shorter and with a chord of only 2 ft. 6 in.
The simple steel Vee strut undercarriage was reminiscent of the Avro 530 in modified form and the attempt made in the earlier design to improve substantially the pilot's field of vision was carried a stage further in the Spider by siting the cockpit under a circular aperture in the centre section. This was mounted close to the fuselage so that the pilot's head protruded above it. Armament consisted of a single synchronised Vickers gun on top of the fuselage and slightly to starboard of centre.
The little fighter was a delight to handle, with powerful and well harmonized controls which made it extremely manoeuvrable, and more than a match for many of its contemporaries. Performance was further enhanced by fitting a 130 h.p. Clerget and drawings were made for the installation of a 150 h.p. Bentley B.R.I rotary or a 170 h.p. A.B.C. Wasp I radial. Well-known pilots were invited to fly it in off duty hours and to give their opinions, for which purpose it was at the School of Special Flying, Gosport, from April 27 to May 18, 1918 and again on July 13. In this way the Spider became such a topic of conversation that the Air Ministry could not fail to take note of it. Nevertheless it was not ordered into production because the Sopwith Snipe had already been standardised as the R.A.F.'s next single seat fighter. The Spider was therefore used for experimental work which included benzole fuel tests at Alexandra Park in August 1919.
A considerably modified version of the Spider was allotted type number Avro 531 A. This had conventional two-bay, wire braced mainplanes rigged with a considerable stagger and using 504K-type interplane struts. With the 130 h.p. Clerget rotary the Avro 531A had a performance similar to that of the Spider. Serial allocation suggests that construction of only one Avro 531 and one Avro 531A was undertaken. There is no means of proving that the latter ever existed as such and it is probable that that machine donated its fuselage, undercarriage and tail unit to the civil Avro 538, and first flew in this form.
The Avro 538 emerged from the flight shed at Alexandra Park, Manchester, in May 1919 registered K-132, a temporary civil marking later changed to G-EACR. As far as is known these symbols were never carried and the machine's main adornment was the word AVRO in the usual enormous black letters. Although powered by a 150 h.p. Bentley B.R.I and intended as a racer, a main spar defect limited the machine's activities to straight and level flight, and a notice to this effect was displayed in the cockpit. Bearing fleet number 7, the Avro 538 was used solely by the Avro Transport Company's chief engineer J. C. C. Taylor, who flew it around the joyriding sites in order to sign out the Avro 504Ks.
SPECIFICATION AND DATA
Manufacturers: A. V. Roe and Co. Ltd., Clifton Street, Miles Platting, Manchester; and Hamble Aerodrome, near Southampton, Hants.
One 110 h.p. Le Rhone
One 130 h.p. Clerget
(Avro 531 A) One 130 h.p. Clerget
(Avro 538) One 150 h.p. Bentley B.R.I
Dimensions, Weights and Performances:
Avro 531 Spider Avro 531A Avro 538
Clerget *Bentley Clerget Bentley
Span (upper) 28 ft. 6 in. 28 ft. 6 in. 28 ft. 0 in. 28 ft. 0 in.
Span (lower) 21 ft. 6 in. 21 ft. 6 in. 27 ft. 0 in. 28 ft. 0 in.
Length 20 ft. 6 in. 20 ft. 6 in. 20 ft. 6 in. 20 ft. 6 in.
Height 7 ft. 10 in. 7 ft. 10 in. 8 ft. 6 in. 8 ft. 6 in.
Wing area 189 sq. ft. 189 sq. ft. - 210 sq. ft.
Tare weight 963 lb. 1,148 lb. 960 lb. 975 lb.
All-up weight 1,517 lb. 1,734 1b. 1,514 1b. 1,400 1b.
Maximum speed 120 m.p.h. 124 m.p.h. 120 m.p.h. 125 m.p.h.**
to 3,500 ft. - 2 min. 12 sec. - -
to 5,000 ft. 4 min. 0 sec. - 4 min. 0 sec. 4 min. 0 sec.
to 10,000 ft. - - - 10 min. 0 sec.
Ceiling 19,000 ft. - 19,000 ft. -
Endurance/Range - 2 1/2 hours 3 hours 320 miles
*Estimated figures. **Cruising speed 108 m.p.h.
(Avro 531 and 531 A) Serial allocation B3952 and B3953;
(Avro 538) One aircraft only, K-132/G-EACR, c/n 538/1, registered to A. V. Roc and Co. Ltd. 25.5.19, s.o.r.* 9.20
*Abbreviation used throughout to indicate 'struck off register'.
P.Lewis The British Fighter since 1912 (Putnam)
A. V. Roe followed up their 530 two-seat fighter with another fighter design - the single-seat 531 Spider. The new prototype was completed by April, 1918, and turned out to be a 110 h.p. le Rhone-engined biplane of striking appearance. In the interest of quick production particular attention was paid to using readily-available 504K parts in the airframe but, despite this admirable object, the Spider was a distinctive machine. The main feature which caught the eye immediately was the system of three pairs of V struts on each side which braced the unequal-span wings without the assistance of bracing wires, the upper wings being set close to the top of the fuselage so that the pilot’s head projected through the open centre-section. A peculiar point about the Spider’s armament was the fitting of only one Vickers gun at a time when two machine-guns had become more or less standard. Tests proved the machine to be excellent for its purpose with admirable manoeuvrability, its top speed at ground level with the 130 h.p. Clerget fitted being 120 m.p.h.
Another version of the Spider was planned as the 531A, based on the 130 h.p. Clerget with different biplane wing cellules and orthodox struts and wire bracing.
H.King Armament of British Aircraft (Putnam)
Spider. Although a contemporary drawing shows two Vickers guns on this 1918 'wireless scout' (the 'wireless' signifying rigid wing bracing) only one gun was actually fitted, though this had more than the normal amount of ammunition. The gun was mounted slightly to starboard of the centre line and was largely internal. One contemporary specification listed these items: 'gun, 70 lb; mounting and ammunition box, 20 lb; belt and 800 rounds, 60 lb; Very pistol with cartridges, 8 lb.# Like the later single-gun Hawker Hornbill, the Spider carried more than the usual quantity of ammunition for a Vickers gun.
Jane's All The World Aircraft 1919
An unsponsored private-venture single-seat fighter designed by Roy Chadwick and flown for the first time in April 1918, the Spider made use of a number of Avro 504 components and had a fabric-covered wooden structure with a system of Warren-girder steel-tube interplane struts. The upper wing was mounted close to the fuselage and directly above the cockpit. In its original form, the Spider was powered by a 110 hp Le Rhone 9J nine-cylinder rotary engine, and proved to possess exceptional manoeuvrability, but overall performance was not sufficiently in advance of the contemporary Sopwith Camel to warrant quantity production. Armament comprised one fixed synchronised 0-303-in (7,7-mm) Vickers machine gun, and a 130 hp Clerget 9B rotary was later fitted, and the following details relate to the Spider fitted with this power plant.
Max speed 120 mph (193 km/h) at sea level
110 mph (177 km/h) at 10,000 ft (3 048 m).
to 10,000 ft (3 048 m) 9.5 min.
Empty weight 963 lb (473 kg).
Loaded weight 1,517 lb (688 kg).
Span 28 ft 6 in (8,68 m).
Length 20 ft 6 in (6,25 m).
Height 7 ft 10 in (2,38 m).
Wing area 189 sq ft (17,55 m2).
W.Green, G.Swanborough The Complete Book of Fighters
AVRO 531 SPIDER UK
An unsponsored private-venture single-seat fighter designed by Roy Chadwick and flown for the first time in April 1918, the Spider made use of a number of Avro 504 components and had a fabric-covered wooden structure with a system of Warren-girder steel-tube interplane struts. The upper wing was mounted close to the fuselage and directly above the cockpit. In its original form, the Spider was powered by a 110 hp Le Rhone 9J nine-cylinder rotary engine, and proved to possess exceptional manoeuvrability, but overall performance was not sufficiently in advance of the contemporary Sopwith Camel to warrant quantity production. Armament comprised one fixed synchronised 0.303-in (7,7- mm) Vickers machine gun, and a 130 hp Clerget 9B rotary was later fitted, the following details relating to the Spider fitted with this power plant.
Max speed, 120 mph (193 km/h) at sea level, 110 mph (177 km/h) at 10,0 ft (3 050 m).
Time to 10,000 ft (3 050 m), 9.5 min.
Empty weight, 963 lb (437 kg).
Loaded weight, 1,517 lb (688 kg).
Span, 28 ft 6 in (8,68m).
Length, 20 ft 6 in (6,25 m).
Height, 7 ft 10 in (2,38 m).
Wing area, 189 sqft (17,55 m2).
Flight, March 20, 1919.
The Avro Machines
The Avro "Spider," Type 531. April, 1918.
The following spring saw an entirely different type of machine issue from the Avro works. This was a single-seater "Scout," in which the wing bracing was along quite unusual lines. From the illustrations it will be seen that, instead of the ordinary wing bracing wires or cables, the "Spider," as this machine was called, had Vee struts arranged in the form of a Warren truss. It may be remembered that in 1917 we published in FLIGHT a series of articles by "Marco Polo," entitled "Wing Bracing and Head Resistance," in which this particular form of wing bracing was dealt with. In this article the author expressed the opinion that although the combination of Nieuport Vee struts and Warren truss did not appear to give the absolute minimum of resistance, it did have a low resistance, while at the same time having the structural advantage that the distance between supports was reduced, thus resulting in a lighter structure, and that therefore the arrangement might be found to be worth trying.
This appears to be what the Avro designer has done, and we may therefore be pardoned a certain special interest in this particular machine. We understand that the "Spider" was extremely manreuvrable and light on the controls, and the accompanying table of performance indicates that the machine had quite a good turn of speed - 120 m.p.h. at ground level with a 130-h.p. Clerget engine is not bad - while the climb was also satisfactory. The pilot was so placed that his eyes were on a level with the top plane, in which a circular opening was cut out. This gave a good view both upwards and horizontally in all directions, while the small chord of the bottom plane gave a minimum of obstruction to downward visibility. The "Spider" might conceivably make a good sporting model, especially if fitted with a somewhat smaller engine, since the petrol bill for a motor of 130 h.p. would probably be more than the majority of owners would care to spend. However, as the machine is light there does not appear to be any reason why, in a slightly modified form, it should not be fitted with, say, an engine of 80 h.p. or thereabouts.
The Fighting Scout, type 531 A.
This machine is of the ultra-modern scout type, with two pairs of inter-plane struts on each side, and with the centre section struts slightly raked outwards. The centre section in the top plane has been left open, in the manner of the Sopwith Dolphin, and the pilot is so placed that his head is in the rear portion of, and slightly below, this opening, so that his view is interrupted to a small extent only. Generally speaking, the machine follows usual Avro practice, in the shape of its body and other main components, such as the semicircular balanced rudder etc. The figures relating to its performance are estimated, and are practically identical with those relating to the "Spider," which has, it will be remembered, the same engine power - a 130 h.p. Clerget. As the total wing area is practically the same in both these machines - differing only in the disposition of the area of top and bottom planes respectively - this affords an interesting comparison between the standard type of machine with two pairs of struts on each side and the Warren-cum-Nieuport type of bracing, accompanied, of course, by a large area top plane and a small area bottom plane. According to the figures given there is little to choose between the two forms, but the "Spider" type may be thought to give the better visibility of the two.
It may be pointed out that the figures of performance given in the table are estimated, the machine not having been flown at the time of writing this article. It is, however due to be tested almost any day now, and we hope shortly to be able to publish a photograph of it.