The 1916 Potlatch Bug was a single place, open cockpit biplane, built as an exhibition plane for motion picture work. One example was built, powered by a 50hp Adams-Farwell rotary.

Designed by Roy Chadwick, the Avro 531 Spider was an unsponsored private-venture single-seat fighter. The Spider used a number of Avro 504 components and had a fabric-covered wooden structure with Warren-girder steel-tube interplane struts.

Originally the Spider was powered by a 110hp Le Rhone 9J nine-cylinder rotary engine and flown for the first time in April 1918. Overall performance was not sufficiently in advance of the Sopwith Camel to warrant quantity production. Armament was one fixed synchronised 7.7mm Vickers machine gun, and a 130hp Clerget 9B rotary was later fitted.

The Spider prototype ended its days in the experimental role.

Engine: 130hp Clerget 9B rotary
Wingspan: 8.68 m / 29 ft 6 in
Length: 6.25 m / 21 ft 6 in
Height: 2.38 m / 8 ft 10 in
Wing area: 17.55 sq.m / 188.91 sq ft
Take-off weight: 688 kg / 1517 lb
Empty weight: 437 kg / 963 lb
Max. speed: 193 km/h / 120 mph at SL
Climb to 5000 ft / 1525 m: 4 min
Service ceiling: 19,000 ft / 5970 m
Range: 250 mi
Armament: 1 x Vickers 0.303 in mg

The Avro 530 two-seat fighter was designed in 1916 to compete with the Bristol F.2A, and the first prototype was first flown in July 1917. Powered by a 200hp Hispano- Suiza 8Bd eight-cylinder water-cooled engine, the Avro 530 was of wooden construction with fabric skinning, and mounted an armament of a single fixed and synchronised 7.7mm Vickers gun, a 7.7mm Lewis gun was mounted on a Scarff ring in the rear cockpit.
Performance of the Avro 530 proved to be good, but not sufficiently on that of the Bristol F.2A to warrant production orders and priority in the supply of the Hispano- Suiza engine was being given to the S.E.5a. During 1918, one of the two Avro 530 prototypes was flown with a 200hp Sunbeam Arab engine, revised undercarriage, an extended tail fin and flapless wings of new section with long-span ailerons, but development was subsequently abandoned.

Engine: 200hp Hispano- Suiza 8Bd eight-cylinder water-cooled
Take-off weight: 1216 kg / 2681 lb
Empty weight: 769 kg / 1695 lb
Wingspan: 10.97 m / 36 ft 0 in
Length: 8.69 m / 29 ft 6 in
Height: 2.92 m / 10 ft 7 in
Wing area: 30.23 sq.m / 325.39 sq ft
Max. speed: 183 km/h / 114 mph
Time to 10,000 ft / 3050 m: 15 min
Service ceiling: 18,000 ft
Endurance: 4 hr
Armament: 1 x Vickers 0.303in / 7.7mm mg, 1 x Lewis 0.303in / 7.7mm mg

The Avro 528 was a two-seat single-engined biplane ordered by the Admiralty in 1915, and not even the task for which it was intended is recorded. It had some similarities with the Avro 519 (a single seater intended for the RFC) and the twin-seat 519A, built for the RNAS, though neither of these were armed and both had 150 hp Sunbeam Nubian engines rather than the 225 hp Sunbeam of the 528. Both the 519s and the 528 had some shared features with the Naval Avro 504.

It was a large three bay biplane with unswept, unstaggered and constant chord wings of unequal span, the lower plane having a span 10 feet 0 inches (3.05 m) less than the upper. Ailerons were carried on the upper wings; both wings folded for storage. The fuselage had similarities with the Naval 504s though the overall length of the 528 was greater by about 4 feet (1.2 m): both had a generous fixed fin in contrast to the all moving, comma shaped rudder of the RFC’s 504s. The vertical stabiliser was also close in size to that of the 504, but the rather rectangular horizontal tail was nearly 60% greater in span. Like the 519s, the top of the fuselage carried a raised decking that provided deeper cockpits for the pilot, placed under the trailing edge of the wing and the observer/gunner, in a separate cockpit close behind equipped with a ring mounted gun. The fixed single axle undercarriage had no central skid.

The Sunbeam engine drove a four-bladed propeller and had a single, central and near vertical exhaust pipe. There were two radiators, mounted edge on (longitudinally) between the wings, rather than the single but similarly mounted radiators of the Avro 519s and the Avro 527. Two tank-like features are shown in both image and diagram on the lower wings just inboard of the innermost interplane struts; they may be fuel tanks.

The first flight was on 19 December 1916 at Avro’s Hamble factory. The aircraft remained troublesome, with a variety of propellers being tried but the Admiralty lost interest and the 528 last flew in April 1917.

Engine: 1 × Sunbeam, 250 hp (187 kW)
Wingspan: 65 ft 0 in (19.82 m)
Length: 33 ft 8 in (10.26 m)
Gross weight: 5,509 lb (2,504 kg)
Crew: 2
Armament: 1× 0.303 in (7.7 mm) Lewis machine gun in rear cockpit provision for bombs in nacelles under lower wing

The two-seat Avro 527 fighter was built for the RFC and flown for the first time early in 1916 with a 150hp Sunbeam Nubian eight-cylinder water-cooled engine. The mainplanes, undercarriage and tail assembly, were basically similar to those of the Avro 504, but the fuselage differed. Proposed armament consisted of a single free-mounted 7.7mm Lewis gun in the rear cockpit. The Avro 527 displayed a poor climb rate and the pilot’s forward view was impaired by the twin exhaust stacks of the Nubian engine. Only one prototype was completed, and development was discontinued during the course of 1916, a version with a longer-span wing, the 527A, also discontinued at the same time.

Engine: 150hp Sunbeam Nubian eight-cylinder water-cooled
Wingspan: 10.97 m / 36 ft 0 in
Max. speed: 166 km/h / 103 mph