Specifications (R-3350-C18-BA)

Nov 2nd, 2009
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General characteristics

* Type: Twin-row 18-cylinder radial engine
* Bore: 6.125 in (155.6 mm)
* Stroke: 6.312 in (160.2 mm)
* Displacement: 3,347 in3 (54.56 L)
* Length: 76.26 in (1,930 mm)
* Diameter: 55.78 in (1,420 mm)
* Dry weight: 2,670 lb (1,212 kg)

Components

* Valvetrain: Pushrod, two valves per cylinder
* Supercharger: Two-speed single-stage
* Fuel system: Chandler-Evans downdraft carburetor
* Fuel type: 100/130
* Oil system: Dry sump
* Cooling system: Air cooled

Performance

* Power output: 2,200 hp at 2,800 rpm (takeoff power)
* Specific power: 0.66 hp/in³
* Compression ratio: 6.85:1
* Power-to-weight ratio: 0.82 hp/lb

R-3350 Applications

Oct 19th, 2009
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* Beechcraft XA-38 Grizzly
* Boeing B-29 Superfortress
* Boeing C-97 Stratofreighter
* Boeing XPBB Sea Ranger
* Canadair CL-28 Argus
* Consolidated B-32 Dominator
* Curtiss XBTC-2
* Curtiss XF14C
* Curtiss XP-62
* Douglas A-1 Skyraider
* Douglas BTD Destroyer
* Douglas DC-7
* Douglas XB-31
* Fairchild C-119 Flying Boxcar
* Fairchild AC-119
* Lockheed Constellation
* Lockheed P-2 Neptune
* Lockheed XB-30
* Martin JRM Mars
* Martin XB-33 Super Marauder
* Martin P5M Marlin
* Stroukoff YC-134

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