GalaxyFlyer wrote:Compressor stalls during an engine run.
GF
Sounds probable to me.
Compressor stalls can occur during ground runs if the airplane inlet is not directly oriented into the prevailing wind. The off axis wind vector plus the engine induced "sucking" vector causes the flow to separate and the fan face pressure to drop. The loss of mass flow causes the fan/compressor flow to reverse and the engine surges.
This is less often a problem for a subsonic airplane like a jet transport because the inlet lip can be fat and is more forgiving of off centerline airflows.
On supersonic airplanes, like the F-16, the inlets need to be sharp, making them prone to separation for off centerline ground run airflows.