HS 220-18 Aircraft Hot Rolled Normalized and Tempered Alloy

HS 220-18 is a low carbon, high silicon, chromium nickel molybdenum alloy steel. It was one of the first grades developed in the high strength class, combining strength with toughness and ductility. It has relatively high impact resistance because of its low notch sensitivity at the high hardness at which this alloy is commonly used. It is available as a basic electric furnace air melt and vacuum degassed product to meet the high aircraft quality standards of AMS 2301. In addition, this alloy is produced as Special Aircraft Quality to insure transverse ductility and toughness.

MIL-S-7108 - AMS 6418 - AMS 2301 - DMS 1841

Color Marking: Ends painted Purple with Pink Stripe

Physical Conditions E
Surface Condition 1

Stock Lengths 20' Approx.

Size	Estimated Weight per Foot	Estimated Weight 20-Ft. Bar
1/2	N/A .6682 lb	N/A 13.36 lb
3/4	N/A 1.504 lb	N/A 30.07 lb
1	N/A 2.673 lb	N/A 53.46 lb
1 1/4	N/A 4.176 lb	N/A 83.53 lb
1 1/2	N/A 6.014 lb	N/A 120.3 lb
1 5/8	N/A 7.058 lb	N/A 141.2 lb
1 3/4	N/A 8.186 lb	N/A 163.7 lb
1 7/8	N/A 9.397 lb	N/A 187.9 lb
2	N/A 10.69 lb	N/A 213.8 lb
2 1/4	N/A 13.53 lb	N/A 207.6 lb
2 1/2	N/A 16.71 lb	N/A 334.1 lb
2 3/4	N/A 20.21 lb	N/A 404.3 lb
3	N/A 24.06 lb	N/A 481.1 lb
3 1/2	N/A 32.74 lb	N/A 654.8 lb
3 3/4	N/A 37.59 lb	N/A 751.7 lb
4	N/A 42.77 lb	N/A 855.3 lb

1/2

N/A .6682 lb

N/A 13.36 lb

3/4

N/A 1.504 lb

N/A 30.07 lb

N/A 2.673 lb

N/A 53.46 lb

1 1/4

N/A 4.176 lb

N/A 83.53 lb

1 1/2

N/A 6.014 lb

N/A 120.3 lb

1 5/8

N/A 7.058 lb

N/A 141.2 lb

1 3/4

N/A 8.186 lb

N/A 163.7 lb

1 7/8

N/A 9.397 lb

N/A 187.9 lb

N/A 10.69 lb

N/A 213.8 lb

2 1/4

N/A 13.53 lb

N/A 207.6 lb

2 1/2

N/A 16.71 lb

N/A 334.1 lb

2 3/4

N/A 20.21 lb

N/A 404.3 lb

N/A 24.06 lb

N/A 481.1 lb

3 1/2

N/A 32.74 lb

N/A 654.8 lb

3 3/4

N/A 37.59 lb

N/A 751.7 lb

N/A 42.77 lb

N/A 855.3 lb

Size

Estimated Weight per Foot

Estimated Weight 20-Ft. Bar