For the CAA i believe that NGV in a Reaction turbine are at constant pressure. I also found this one wrong: 210757. Its the same kind of question. Regards.
Can you confirm that CAA marks as valid that the pressure drops in the NGV in reaction turbine?
Another one i found which is contradicting other answers in BGS is this one: 210590
"The specific fuel consumption is inversely proportional to pressure altitude, at constant TAS." When the correct answer in most questions is that SFC increases/decreases SLIGHTLY with PA decreasing/increasing, so not inversely proportional and not directly proportional.
Last edited by flyfly4; 18th July 2016 at 15:04.