Fly Past

(Barry) #1

20 RAF CENTENARY CELEBRATION PATROLLERS AND AIRLIFTERS


Type: Five-crew general reconnaissance fl ying boat
First fl ight: July 8, 1932; entered service May 1935
Powerplant: Two 525hp (391kW) Rolls-Royce Kestrel piston engines
Dimensions: Span 75ft (22.90m), length 53ft (16.20m)
Weights: Empty 10,010lb (4,540kg), all-up 16,040lb (7,276kg)
Max speed: 142mph (229km/h) at 3,280ft (1,000m)
Range: 1,100 miles (1,770km)
Armament: Three Lewis guns in bows and amidships. Bomb load: 1,000lb
(454kg)
Replaced: Supermarine Southampton
Taken on charge: 14
Replaced by: Saro London

SUPERMARINE SCAPA


SUPERMARINE


SCAPA

1935 TO 1938


T


he Supermarine Scapa began
life as a completely upgraded
and modernised version of
the company’s Southampton flying
boat (see page 10). In fact, when
it first flew on July 8, 1932 it was
designated as the Southampton
Mk IV.
All the Scapa, as it was christened
in October 1933, shared with
the Southampton was its
general dimensions and a family
resemblance in tail design.
The triple fins of its predecessor
were replaced with twin tails and
rudders, while the two pilots sat
side-by-side in a fully enclosed
cockpit. The earlier machine’s
wooden wings were swapped for
metal units, giving the Scapa an
all-metal construction, and the hull
itself was changed slightly to ensure
greater internal space.

RE-ENGINED
The most important change came
with the powerplants and how they
were mounted to the airframe.

The Southampton’s Napier Lions
had been fitted between the wings,
where they and their complex
wire bracing created substantial
aerodynamic drag. In the case of the
Scapa the Rolls-Royce Kestrels were
neatly cowled and faired into the
upper wings.

The prototype Scapa (S1648)
was followed by 14 production
variants for the RAF, with deliveries
completed by July 1936.
First to receive the new type was
202 Squadron in Kalafrana, Malta,
in May 1937 and these were soon
followed by Alexandria, Egypt-based

1918 2018

Below
Compared to earlier
fl ying boat designs, the
Scapa benefi ted from
advanced aerodynamics
and streamlining.
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