1931
Location

Race Details
1931 Schneider Cup Course
The 1931 contest was scheduled for 12 September over a triangular circuit above the Solent and Spithead, off the Isle of Wight. Heavy rain and poor visibility postponed the flight for a day; Flight Lieutenant John N. Boothman completed it on 13 September. Contemporary reporting describes a 50-kilometre circuit flown seven times anticlockwise: 350 kilometres in all, usually rendered as 217.48 statute miles (about 217.5 miles). The map is a modern approximate reconstruction on a satellite-style background, not a survey of the 1931 pylon positions. Nature’s 19 September 1931 report confirms the triangle, Solent/Spithead location and total distance; a contemporary announcement reproduced in the North Otago Times specifies the 50 km circuit and seven anticlockwise laps.
Route and landmarks. The course lay across the eastern Solent between Hampshire and the Isle of Wight. The start/finish was off Ryde. Contemporary eyewitness coverage describes Boothman rounding St Helen’s Point, then West Wittering, before turning again at Browndown Anchorage and returning across the Solent. Those place names support the broad triangular reconstruction shown on the map; the exact historic positions of the start line and turning pylons are not established by the sources consulted. Treat the illustrated points and straight connecting legs as approximate. The October 1931 account in The Motor Sport gives the landmarks and describes the flying turns.
Start and course procedure. The 1931 course was not the quadrilateral flown in 1929: the Royal Aero Club announced a triangular route. Before the timed course, the aircraft had to demonstrate seaworthiness by taking off, climbing, landing, and taxiing on the water; Boothman completed that trial before crossing the start line. The timed flight was then seven circuits. The 1931 report does not provide a surveyed list of pylon coordinates or reliable leg-by-leg distances, so none are asserted here. The contemporary race report describes Boothman’s seaworthiness trial and the route landmarks.
Distance and uncertainty. Seven 50 km laps equal 350 km; period and later references round the statute-mile equivalent to 217.5 miles, while 217.48 miles is the more precise conversion. A few sources call the 50 km figure “just over 31 miles” or round the lap to 32 miles; those are approximate descriptions, not evidence of a different official distance. The U.S. Air Service’s historical account gives seven 50 km laps and 217.48 land miles. A 1931 Nature article calls this the “eleventh contest,” but that ordinal conflicts with the accepted sequence of twelve contests from 1913 through 1931; its course and race facts remain useful, while the ordinal appears erroneous.

The course length and map’s red line is a visual reconstruction, not a claim to the exact historical buoy layout.
The Winner
(2,350 hp)
340.08 mph

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The Supermarine S.6B is a British racing seaplane developed by R.J. Mitchell for the Supermarine company to take part in the Schneider Trophy competition of 1931. The S.6B marked the culmination of Mitchell's quest to "perfect the design of the racing seaplane" and represented the cutting edge of aerodynamic technology for the era.
The S.6B was last in a line of racing seaplanes to be developed by Supermarine, following the S.4, S.5 and the S.6.[1] Despite these predecessors having previously won the Schneider Trophy competition twice, the development of the S.6B was hampered by wavering government support, which was first promised then withdrawn, and then given once more after a high-profile public campaign encouraged by Lord Rothermere and backed by a substantial donation by Lady Houston. Once government backing had been secured, there were only nine months before the race, so Mitchell's only realistic option was to refine the existing S.6, rather than attempting a new design.
Race setting and competitors
The twelfth Schneider Trophy contest was held over the Solent on 13 September 1931. Scheduled for the previous day, it was postponed because of poor weather. France and Italy withdrew, leaving Great Britain without an international challenger. The British team needed to complete the course to claim its third consecutive victory and keep the Trophy permanently.
The British entry included two new Supermarine S.6B racers and a Supermarine S.6. Flight Lieutenant John Boothman flew S.6B S1595, powered by a Rolls-Royce R engine rated at about 2,350 hp. The S.6B developed the S.6 with a more powerful engine and refinements for the 1931 contest.
Race events and results
Boothman completed seven laps of the 50 km course in 38 minutes 22.2 seconds, averaging 340.08 mph (547.3 km/h). His flight qualified as the race victory and secured the Trophy for Britain. During the course, he also set a 100 km record at about 342.9 mph.
The other British aircraft were prepared as part of the team, but there was no international race between competing nations. After Boothman’s victory, Flight Lieutenant George Stainforth flew an S.6B in a separate speed record attempt, averaging 379.05 mph over the measured course.
Recorded results:
| Result | Pilot | Aircraft | Time / average speed |
|---|---|---|---|
| Winner | John N. Boothman (Great Britain) | Supermarine S.6B S1595 | 38:22.2; 340.08 mph |
| Team aircraft | F. W. Long (Great Britain) | Supermarine S.6B S1596 | Prepared; no recorded Trophy race result |
| Team aircraft | L. S. Snaith (Great Britain) | Supermarine S.6 N248 | Prepared; no recorded Trophy race result |
Winner and significance
Boothman’s victory gave Britain its third consecutive Schneider Trophy win, following the victories of 1927 and 1929. Under the rules, Britain took permanent possession of the Trophy, bringing the contest to an end.
The result capped years of development by Supermarine and Rolls-Royce. The S.6B’s streamlined design and powerful R engine demonstrated the speed achieved through collaboration between aircraft designers, engine makers, pilots and support teams. The technology and experience gained through the Schneider programme contributed to later British aircraft development.
Sources: Nature, “The Schneider Trophy Contest” (1931); Schneider Trophy 1931 race history; This Day in Aviation, 1931 race account.




























































