Model Kartonowy - Marek Pacynski(Model Cardboard) 011 - Curtiss So3C 'seamew'(1-33).pdf

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Seamew.cdr

Printed in Poland at publishing house patternel:

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The Curtiss SO3C-1 Seamew was a two-seat

reconnaissance aircraft developed by the US Navy and

were sold to Great Britain under Lend-Lease. It was

originally called the Seagull in the States but following the

naming of the "Seamew" by the FAA it was later also

adopted by the USN. The original SO3C-2 Lend-Lease

version delivered to the FAA had additional bomb rack

under fuselage and arrester gear as well as other

refinements over USN versions. The next version was the

Seamew 1, the FAA equivalent of SO3-2C. 250 lend-lease

aircraft were ordered for the FAA. While the Seamew was

intended for catapult launch on the Royal Navy's ships, it

never saw operational service. Many of the first aircraft

were initially transferred from Roosevelt Field in March

1943 to TOC 1 NAGS Yarmouth and on to the RN January

1944 for shipping amongst others to Worthy Down. Since

the type was not a great success it was declared obsolete

and scrapped from September 1944 onwards. The aircraft

was relegated to second line squadron usage and the

majority of the aircraft were used to train TAG's in Canada.

The last aircraft in the RN served until 1945. In addition to

the Curtiss SO3C-1 Seamew there was the Queen Seamew,

which was the FAA equivalent of SO3-1K; 30 were

ordered under lend-lease. Ordered under Requisition No.

BAC/N-1-857. Cancelled. Intended delivery of 30 target

drone conversions never materialised.Remaining at

Roosevelt Field, before converstion to RN Queen

Seamews

Manufacturer:.........................Curtiss

Designation System: ..............U.S. Navy / Marines

Designation Period:................1934-1946

Basic role: ..............................Scout Observation

Crew: ......................................Pilot & Observer

Specifications

Length: .........................35' 8" (10.8 m)

Height: .........................14' 2"(4.3 m)

Wingspan: ....................38' (11.5 m)

Wingarea:.....................293.0 sq ft(27.2 sq m)

Empty Weight:.............4,800 lb (2,176 kg)

Gross Weight: ..............7,000 lb (3,174 kg)

Propulsion

No. of Engines:......................1

Powerplant: ...........................Ranger V-770-8

Horsepower (each): ...............600

Performance

Range: ...................................1,150 miles (1,851 km)

Cruise Speed: ........................125 mph (201 km/h)

Max Speed:............................172 mph (276 km/h)

Climb:....................................720 ft/min (219 m/min)

Ceiling: ..................................15,800 ft (4,815 m)

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part number 3

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