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Type: Carrier based dive bomber
Origin: Curtis
Crew: 2
Models: SB2C-1 to SB2C-5
First Flight: XSB2-C-1: December 18, 1940
Service Delivery: June 1942
Final Delivery: 1945
Production: 7,200+

Powerplant:
Model: Pratt & Whitney R-1820-40 (G-205A) Cyclone
Type: 9-cylinder radial engine
Number: One      Horsepower: 1,100 hp

Dimensions:
Wing Span: 15.2m (49 ft. 9 in.)
Length: 11.2m (36 ft. 8 in.)
Height: 5.1m (16 ft. 11 in.)
Wing Area: N/A

Weights:
Empty: 4990 kg (11,000 lb)
Maximum: 7550 kg (16,607 lb)


Performance:
Max. Speed: 452 km/h (281 mph)
Initial Climb: N/A
Service Ceiling: 7530m (24,700 ft.)
Max. Range: 1786 km (1,110 miles)
  Armament:
Two 20mm cannon in wings Or
Four .50 in. machine guns in wings
Two .30 in. or single .50 in. machine guns in rear cockpit

Bomb Load:
1,000 lb. (454 kg) of bombs internally
Later versions added wing racks


Comments:
One of the most successful dive-bombers used by the allies, the Helldiver's development started out rather slow. The US services asked for 880 changes after the design had been accepted for production and to further complicate things the prototype crashed. The changes were necessary to try and standardize the design for all three American services. The type was designated the A-25 Shrike for the Us Army and the Cleveland by the RAF, who used the type briefly. Production was carried out by Curtis, Fairchild (SBF) and the Canadian Car & Foundry (SBW). From 1943 on the Helldiver flew in nearly every major action in the Pacific war.

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