Originally Posted by
TheMadBrewer
Which says to me some staffer saw the .85 Mach number and didn't know/care about differences in temp/pressure and calculated ".85 * 765 = 651"
Given the transposition possibility, they may have just read
the Airbus spec sheet wrong, or typed it in wrong on the DL page. (In which case they also didn't cross-check the km/h.)
"Cruising speed:
902 km/h (560.48 mph)"
Though I don't know what altitude that assumes. Service ceiling is darn near 43,000ft!