If you READ the report and understand it, low speed tests are supposed to be conducted at a window between FL100 and FL140 and in NORMAL LAW.
The test was conducted at 3000 feet in DIRECT LAW by disconecting or failure of two FACs(15:37:08). The instant the A/C degraded to ALT LAW, the low speed test must be stopped. The purpose of this check is for LOW SPEED PROTECTIONS which are NOT avilable in DIRECT LAW.
There is no mention of a Flight Test Engineer on any part of the report, I wonder who was handling the readding or the parameters on the AIDS.
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Last edited by guiones; 25th Feb 2009 at 00:23.