Fits:
1982-1986 Chevrolet Camaro 2.5L 2474CC 151Cu. In. l4
1990-1992 Chevrolet Camaro 3.1L 189Cu. In. V6
1982-1992 Chevrolet Camaro 5.0L 305Cu. In. V8
1987-1992 Chevrolet Camaro 5.7L 350Cu. In. V8
1989 Chevrolet P20 5.7L 350Cu. In. V8
1989-1990 Chevrolet P30/P60 5.7L 350Cu. In. V8
1982-1986 Pontiac Firebird 2.5L 2474CC 151Cu. In. l4
1990-1992 Pontiac Firebird 3.1L 189Cu. In. V6
1989 Pontiac Firebird 3.8L 3800CC 231Cu. In. V6
1982-1992 Pontiac Firebird 5.0L 305Cu. In. V8
1987-1992 Pontiac Firebird 5.7L 350Cu. In. V8
This Radiator Size:
High Performance Racing Spec.
4-Row of tubes Core Racing Design
Core Material: All Aluminum
Tank Material: AA5052 Aircraft Grade Aluminum
Surface Finish: Aircraft Grade Raw Aluminum
Includes CNC machined filler neck and cap
Radiator Flow: Cross Flow
Core Dimensions: 26.26"W x 16.5"H
Overall Dimensions: 31.5"W x 19.7"H
Inlet / Outlet Diameter: 1-3/8" / 1-5/8"
Upper / Lower Hose Fitting: Driver / Pass
Trans Cooler Details: ¢26×290×M12*1.25(Z)
Mounting Type: Saddle
Mounting Specs: Vert - 22 3/8 Horizontal - 17 1/2
OEM Style Brass Petcock Drain.
Please Check the Size Before You Buy!
Description:
The core of the radiator is welded in vacuum brazing furnace, no epoxy.The Radiator are 100% welded by TIG.Stronger & Higher Capacity for Coolant than OEM units,Made of High Quality AA5052 Aircraft Grade Aluminum Construction
Aircraft Grade Aluminum radiator is designed to provide maximum cooling efficiency to prevent premature engine failure. Its light-weight, and high-heat transferring Aircraft Grade Aluminum features a tube and fin design that, dramatically increases surface area that enables the heat to dissipate more efficiently. This High Quality Aircraft Grade Aluminum Radiator is at least 35% to 45% more efficient than stock ones. Most importantly, it has a much higher capacity for coolant than stock ones, which means that your cooling system will be more efficient and will be more resistant to temperature surges in racing applications.
Aluminum plate is pressed, high quality and durable.
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