General Aircraft Croydon

ST-18 Croydon
GAL Monospar ST-18 Croydon, 1936
Role	Cabin monoplane
Manufacturer	General Aircraft
First flight	1935
Introduction	1935
Retired	1936
Number built	1

The General Aircraft ST-18 Croydon was a 1930s British cabin monoplane built by General Aircraft Limited.

Development

Following the mixed success of the earlier Monospar family of aircraft, the company designed a ten-seat light transport, the ST-18 (later named Croydon). Due to the longer-span wing, it was not a cantilever monospar wing but had to be fitted with bracing struts. The ST-18 was a low-wing monoplane, with a conventional tail unit and tailwheel landing gear, and hydraulically retractable main gear. It was powered by two Pratt & Whitney Wasp Junior radial engines mounted on the wing leading edges. It had a crew of three, and a cabin for ten passengers, a toilet and baggage compartment.^[1]

Operational history

On 16 November 1935, the sole aircraft (T22, later G-AECB) first flew at Hanworth Aerodrome, piloted by Harry M. Schofield. It performed well, but did not attract any orders, so the aircraft was prepared to establish a record for an Australia to England flight. On 30 July 1936, Lord Sempill, Harold "Tim" Wood, and two other crew left Croydon Airport for Australia. On 7 October 1936, during the return flight from Darwin, navigation errors occurred during the flight over the Timor Sea, and the aircraft made a successful forced landing on a coral reef (Seringapatam Reef). The crew members were immediately transported off the reef by local fishermen, and the aircraft was abandoned.^[1][2]

Specifications

Data from The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1938

General characteristics

• Crew: 3 (pilot, co-pilot and wireless operator)
• Capacity: 10 passengers
• Length: 43 ft 3 in (13.18 m)
• Wingspan: 59 ft 6 in (18.14 m)
• Height: 13 ft 15 in (4.09 m)
• Wing area: 454 ft² (42.18 m²)
• Empty weight: 8000 lb (3639 kg)
• Gross weight: 11,350 lb (5148 kg)
• Powerplant: 2 × Pratt & Whitney R-985 Wasp Junior SB 9-cylinder radial piston engine, 450 hp (336 kW) each

Performance

• Maximum speed: 203 mph (327 km/h)
• Range: 900 miles (1448 km)
• Service ceiling: 19,500 ft (5945 m)

Notes

1. ^ ^{a b} Jackson (1974), p. 310
2. ^ Flight 10 December 1936

References

• The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1938
• A.J.Jackson, British Civil Aircraft since 1919 Volume 2, Putnam & Company, London, 1974, ISBN 370 10010 7, Page 310