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GRUMMAN F4F WILDCAT
Specifications

Type: Naval Fighter
Origin: Grumman
Crew: 1
Models: G-36, Martlet, F4F-1 to -4 &
   Eastern Motors FM-1 and FM-2
First Flight:
   XF4F-2: September 2, 1937
   XF4F-3: February 12, 1939
Service Delivery:
   G-36 and F4F-3: March 1943
   FM-2: February 1940
Final Delivery: August 1945
Production: N/A

Powerplant:
XF4F-2:
   Model: Pratt & Whitney R-1830-66 Twin Wasp
   Type: 14-cylinder two-row radial engine
   Number: One       Horsepower: 1,050 hp

G-36 & Martlet I (Wildcat I):
   Model: Pratt & Whitney R-1820-G205A Cyclone
   Type: 9-cylinder radial engine
   Number: One       Horsepower: 1,200 hp

F4F-3:
   Model: Pratt & Whitney R-1830-76
   Type: N/A
   Number: One       Horsepower: 1,200 hp

F4F-4 & FM-1 (Wildcat V):
   Model: Pratt & Whitney R-1830-86
   Type: N/A
   Number: One       Horsepower: N/A

FM-2 (Wildcat VI):
   Model: Pratt & Whitney R-1820-56
   Type: 14-cylinder twin-row radial engine
   Number: One       Horsepower: 1,350 hp

Dimensions:
Wing Span: 11.6m (38 ft.)
Length: 28 ft. 9 in. to 28 ft. 11 in.
Length (FM-2): 8.5m (28 ft. 10 in.)
Height: 3.6m (11 ft. 11 in.)
Wing Area: N/A

Weights:
Empty (F4F-3): 4,425 lb.
Empty (F4F-4): 4,649 lb.
Empty (FM-2): 4,900 lb. (2226 kg.)
Loaded (F4F-3): 5,876 lb.
Loaded (FM-2): 7,412 lb.


Performance:
Max. Speed (F4F-3): 523 km/h (325 mph)
Max. Speed (F4F-4, FM-1): 509 km/h (318 mph)
Max. Speed (FM-2): 534 km/h (332 mph)
Initial Climb (Typical): 2,000 ft/min (610 m/min)
Initial Climb (Early Versions): 3,300 ft/min
Initial Climb (Main Production): 1,920 ft/min
Initial Climb (FM-2): over 2,000 ft/min
Service Ceiling (Typical): 10,670m (35,000 ft.)
Max. Range (Typical): 1448 km (900 miles)

Armament:
XF4F-2:
Two .50 Colt-Brownings in fuselage

F4F-3:
Four .50 Colt-Brownings in outer wings

F4F-4 & Subsequent variants:
Six .50 Colt-Brownings in outer wings

Bomb Load: F4F-4, FM-1 & FM-2
Underwing racks for two 250 lb. (133 kg) bombs.

Avionics:
N/A


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