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Saro Cutty Sark



 
 
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Old December 7th 17, 03:17 PM posted to alt.binaries.pictures.aviation
Miloch
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Default Saro Cutty Sark

https://en.wikipedia.org/wiki/Saro_Cutty_Sark

The Saro A17 Cutty Sark was a British amphibious aircraft from the period
between World War I and World War II, built by the British firm Saunders-Roe
(also known as SARO). The aircraft was named after the ship Cutty Sark, rather
than the garment.

In 1928, Sir Alliot Verdon Roe sold Avro. He bought an interest in S. E.
Saunders, flying boat manufacturers based at Cowes, Isle of Wight, southern
England; the company was renamed Saunders-Roe. The A17 Cutty Sark was the new
company's first design. It was a shoulder-winged twin-engined four-seat
amphibian monoplane with an all-metal hull and plywood covered wings. The
above-wing pylon-mounted engines could easily be changed, and a variety of
different engines were used to power Cutty Sarks, including 104 hp Cirrus Hermes
Mk 1s and 120 hp de Havilland Gipsy IIs. The Saro A19 Cloud was developed from
this design.

Only 12 Cutty Sarks were built, and none lasted long in service, but the type
nevertheless saw service with many users in the United Kingdom, Australia,
Canada, New Zealand, China, Japan and the Dominican Republic.


Role
Amphibian

Manufacturer
Saunders-Roe

First flight
4 July 1929

Introduction
1930

Number built
12

Production aircraft

A17/1 : The prototype G-AAIP was first flown 4 July 1929. Bought by Captain
Campbell Shaw and Flight Lieutenant Tommy Rose for Isle of Man Air Services.
Returned to Cowes in 1933 after being damaged by floating timber.

A17/2 : VH-UNV was exported to Australia by Matthews Aviation flying the Bass
Strait between Melbourne and Tasmania from May 1930. On 8 November 1931 the
aircraft was driven by wind into a pier at St. Kilda, and Mr E. Lloyd, a
passenger who attempted to assist, was killed by a propeller. In 1935 it was
sold to Pioneer Air Services. In 1937 it was sold to Keith Caldwell, a young
barnstorming pilot from Lindfield NSW (not to be confused with the NZ WWII
fighter ace of the same name); on 15 October 1937, at the same time as he joined
Qantas as a pilot, Caldwell sold VH-UNV for £700 to the airline as a trainer. It
was written off after landing on water with the undercarriage extended on 5
April 1938.

A17/3 : a.k.a. "L3". Sold to the RNZAF. It was first flown on 3 March 1930, then
shipped to New Zealand aboard the SS Mataroa (fr) where it was reassembled by 28
May 1930. It operated from Hobsonville, Auckland for the next six years. After
221 hours and 5 minutes flying time it was judged worn out beyond economic
repair. L3 made its last flight on 23 November 1936, after which it served as an
instructional airframe. It was scrapped in 1939.

A17/4 : G-AAVX before being sold to Canada as VR-SAA in 1930.

A17/5 : G-ABBC named "Progress I" operated out of Blackpool to the Isle of Man
by British Amphibious Airlines. Attempts to replace it with an A.19 Cloud after
1933 were blocked due to SARO's decision to operate an airline from the Isle of
Man.

A17/6 : Acquired by the Royal Air Force as S1575.

A17/7 : Sold to Canada as VR-HAY

A17/8 : Served in the Kwangsi Air Force in China, but was returned to Britain as
G-AETI.

A17/9 : Initially registered G-ABVF then exported to Japan.

A17/10 : Registered G-ACDP to Air Service Training Ltd., used by No 3 E & RFTS
until 1942.

A17/11 : Registered G-ACDR to Air Service Training Ltd., used by No 3 E & RFTS
until 1942.

A17/12 : Registered G-ADAF. This may be the machine exported to the Dominican
Republic in 1935, and written off in 1942.

Specifications (Genet Major engine)

General characteristics
Crew: two pilots
Capacity: 2 passengers
Length: 34 ft 4 in (10.46 m)
Wingspan: 45 ft 0 in (13.72 m)
Height: 11 ft 2 in (3.40 m)
Wing area: 320 ft² (29.7 m²)
Empty weight: 2,725 lb (1,239 kg)
Loaded weight: 3,900 lb (1,770 kg)
Powerplant: 2 × Armstrong-Siddeley Genet Major, 140 hp (104 kW) each

Performance
Maximum speed: 107 mph (93 knots, 172 km/h)
Cruise speed: 90 mph (78 knots, 145 km/h)
Range: 315 miles (274 nmi, 507 km)
Service ceiling: 9,000 ft (2,740 m)
Rate of climb: 500 ft/min (2.5 m/s)




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