It strikes me that testing the Engine Cut Off sensors would entail putting them in liquid hydrogen at the same pressure as they experience in the External Tank, which uses tanks that are at least 30 feet high. Then, cycling the tank a few times, with a long period of no hydrogen followed by a period of high pressure liquid hydgrogen. There seems to be a regieme which can lead to failure that we haven't detected yet.<br /><br />The ECO sensors are in place to prevent the Space Shuttle Main Engines from trying to run without fuel, which could lead to an explosion. They are part of the original design, a safety feature in case of a failure of the ET which would allow the fuel to leak, or in case the engines consume more fuel than predicted. Years of experience with this vehicle have led to knowing how it behaves quite well, as long as certain things are avoided, like launching in really cold weather, or letting large chunks of foam from the ET strke the orbiter. So, when it is decided that the failure pattern on the ECO sensors is within a regieme with little risk, that is not a blind decision, but a rational assesment of risk. <br /><br />I am a bit more surprised at the decision regarding the Auxillary Power Unit, but this mission is considered essential to the International Space Station program, and a great deal of money has been on hold while waiting for construction to continue. With the daylight constraints, and weather factors in launches later in the year, making this window is apparently critical. <div class="Discussion_UserSignature"> The secret to peace of mind is a short attention span. </div>