comp 2010 master lobes
.370 * 1.7 = .6290
.372 * 1.7 = .6324
.374 * 1.7 = .6358
.376 * 1.7 = .6392
.378 * 1.7 = .6426
If you do the math, the lobe lift x the rocker ratio gives you the lift at the valve. The values I calculated above appear in the 1.6 column.
Its a mis-print.
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