Curtiss SOC Seagull

Airplanes

Length

9.4488 m

Flat Wing Span

10.9728 m

Height

4.2672 m

Flat Wing Area

31.7728 m²

Cruise Speed

214.0428 km/h

Max Speed

265.5418 km/h

Max Ceiling

4541.52 m

Number of Engines

First Flight

1934-04-01

Entry Into service

1935-11-12

Number Built

322

Maximum Range

1086.307 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Range (km)
Curtiss SOC Seagull	1086.307

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Avro Antelope		9.4488	10.9728	Compare
Aichi F1A	Nakajima Hikari	9.3	11	Compare
Arado Ar 197		9.2	11	Compare
Avro 500		9.144	10.9728	Compare
Avro 627 Mailplane		9.144	10.9728	Compare
Canadair CT-114 Tutor	General Electric J85	9.7536	10.9728	Compare

All data (25 fields)

Name: Curtiss SOC Seagull
Manufacturer: Military designations USN
Description: The Curtiss SOC Seagull was an American single-engined scout observation seaplane, designed by Alexander Solla of the Curtiss-Wright Corporation for the United States Navy.
First Flight: 1934-04-01
Entry Into service: 1935-11-12
Production End: 1940-01-01
Service End: 1949-01-01
Designer: Alexander Solla
Type: Scout
Length (m): 9.4488
Height (m): 4.2672
Max Speed (km/h): 265.5418
Cruise Speed (km/h): 214.0428
Min Speed (km/h): 89.9623
Max Ceiling (m): 4541.52
Rate of Climb (m/s): 4.6482
Armament: 1× fixed, forward firing 0.30 in (7.62 mm) Browning AN/M2 and 1× flexible mounted rear-firing 0.30 in (7.62 mm) Browning AN/M2 machine gun; 2× 100 lb (45 kg) bombs or 325 lb (147 kg) depth charges underwing
National Origin: United States of America
Number Built: 322
Powerplant Description: 1 × Pratt & Whitney R-1340-18 single-row, nine-cylinder, air-cooled radial engine, 447 kW (600 hp) each
Primary Users: United States Navy, United States Coast Guard, United States Marine Corps
Wikipedia Article (URL): en.wikipedia.org/wiki/Curtiss_SOC_Seagull
Flat Wing Span (m): 10.9728
Flat Wing Area (m²): 31.7728
Number of Engines: 1