Template talk:Engine thrust to weight table
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The Thrust-to-weight ratios for the J58 and F119 are wrong according to the data.
J58: 34000/6001 = 5.7 and not 5.2 as stated.
F119: 20500/3900 = 5.3 and not 7.95 as stated.
It is easy to change the t/w value to be consistent, but since it could be any of the three values (thrust, weight or thrust/weight) that are wrong, it is unclear which correction to make. I have left it wrong to at least show that the source data is suspect.