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typhoonpilot said:Good memory. More exactly, they reduce the fuselage vortex that can occur at high AOA. That vortex would impinge on one side of the vertical stabilizer and rudder thus decreasing directional control.
They were first introduced with the stretched DC-9-50 and appear on the MD-80 and MD-90 as well. They do not appear on the DC-9-30, B717, or other shorter versions as the fuselage vortex is not an issue.
TP