Short Scylla

The Short L.17 Scylla was a British 4-engined 39-seat biplane luxury airliner designed and built by Short Brothers at the request of Imperial Airways and used by them for scheduled flights between London and European cities e.g. Paris. Two aircraft were built, the Scylla (G-ACJJ) and the Syrinx (G-ACJK). Both served with the airline until its merger into BOAC in 1939, and both were finally taken out of service the following year.

Design and development

The Scylla was a land-based development of the Short Kent (S.17) flying boat, essentially using the Kent's aerostructure above a redesigned fuselage. It was a large, all-metal biplane (wingspan of 113 ft, 34,44 m) powered originally by four Bristol Jupiter XFBM radial engines mounted on vertical struts between the upper and lower planes. The square-section braced-framed fuselage was mounted below the lower wing. The tail unit comprised a single vertical fin and a horizontal tailplane mounted on the fin at approximately one quarter height. The Scylla was originally fitted with a Flettner trimming aerofoil to ease the forces on the rudder controls; an experimental servo tab on the rudder was tested on G-ACJJ Scylla for a time. Experience gained with the latter possibly contributed to a later patent application submitted jointly by Shorts and Dudley Lloyd Parkes on 7 August 1936.

The forward undercarriage comprised one fixed wheel on each side, mounted on 3 diagonally braced struts, one to the upper and two to the lower edge of the fuselage; there was a single tailwheel. Ailerons were fitted to both upper and lower wings.

The engine nacelles were designed to receive Bristol Jupiter, Pegasus or Perseus engines without modification, a far-sighted and sensible provision, which later enabled e.g. the two inboard Jupiters of G-ACJK Syrinx readily to be replaced with Perseus IIL sleeve valve engines, to test their performance in airline conditions. When Syrinx was re-built (after it had been severely damaged when blown over by sidewinds while taxiing at Brussels airport), it was fitted with four Pegasus XC engines.

Operators

Template:Country data United Kingdom

• Imperial Airways

Specifications

Data from Barnes and James, p.278

General characteristics

• Crew: 4
• Capacity: 39
• Length: 83 ft 10 in ft (25.5 m)
• Wingspan: 113 ft (34.44 m)
• Height: 31 ft 7 in (9.6 m)
• Wing area: 2,615 ft² (243 sq.m)
• Empty weight: 22,650 lb (10,290 kg)
• Loaded weight: 33,500 lb (15,200 kg)
• Powerplant: 4× Bristol Jupiter XFBM air-cooled radial, 555 hp (414 kW) each

Performance

• Maximum speed: 137 mph (220 km/h)

The two L.17 aircraft, G-ACJJ Scylla and G-ACJK Syrinx, had at different times three different engine configurations between them:

1. Four Bristol Jupiter XFBM one-row radial poppet valve piston engines of 595 hp (444 kW) each
2. Two Bristol Jupiter XFBM radial poppet valve radial piston engines of 595 hp (444 kW) (outer pair) and two Bristol Perseus IIL sleeve valve radial piston engines of 540 hp (400 kW) each (inner pair)
3. Four Bristol Pegasus XC radial poppet valve piston engines of 660 hp (492 kW) each

See also

Related development

• Short Kent

References

• Barnes C.H. & James D.N (1989). Shorts Aircraft since 1900. London: Putnam. ISBN 0-85177-819-4. 
• Cassidy, Brian (2004). Flying Empires: Short ‘C’ class Empire flying boats (PDF). Queens Parade Press. Retrieved on 2007-01-15.
• Gunston, Bill (editor) (1980). The Illustrated Encyclopedia of Propeller Airliners. London: Phoebus. ISBN 0 7112 0062 9. 
• Century-of-Flight.net: Short Scylla. Retrieved on 2007-01-18.
• Short L17 Scylla. Imperial Airways project. Retrieved on 2007-01-24.

This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Short Scylla".