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Avro 529

Avro 529
Avro 529.png
Role Long-range bomber
National origin United Kingdom
Manufacturer A.V. Roe & Co.
First flight April 1917
Number built 2
Developed from Avro Pike

The Avro 529 was a twin-engined biplane long-range bomber of the First World War. Two prototypes were built but no production ensued.

The Avro 529 was Avro's second twin-engined aircraft and their second attempt at a heavy bomber. Their first in both categories was the Pike, developed in early 1916 to Royal Flying Corps (RFC) guidelines for a short-range bomber. The Pike arrived too late to secure orders from the RFC who would order the Handley-Page O/100 and for the Royal Naval Air Service (RNAS) who had ordered the Short Bomber. Nonetheless, after trials of the Pike, the Admiralty ordered two prototypes of an enlarged Pike for a long-range bomber role. This was the Type 529.

Like the Pike, it was a large twin-engined biplane of the then-standard wood and canvas construction. It had three-bay wings without sweepback, dihedral or stagger, partly to facilitate wing folding. The vertical tail was different from that of the Pike: it had a small, roughly triangular fin and a rudder with a round balance surface above the fin, a reminder of Avro's "comma" rudder form.

The fuselage was rectangular in cross-section and seated three in separate cockpits. The pilot sat just forward of the wing leading edge, there was a gunner's position (with emergency dual control) midway between the trailing edge and the tail and the front gunner/bomb-aimer's position was in the nose. Both gunners' positions were provided with a .303 in (7.7 mm) Lewis Gun mounted on a Scarff ring. The landing gear used two main wheels on split axles, plus a tail-skid.

The two prototypes differed from each other chiefly in their powerplants. The first, just known as the Avro 529 had a pair of uncowled Rolls-Royce Falcon water-cooled in-line engines mounted midway between the wings. Each produced 190 hp (140 kW) and drove four-bladed, opposite-handed wooden airscrews. It carried 140 gal (636 L) of fuel in a tank in the centre fuselage.


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