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Hi Scet;
I just noticed this post in passing. I'm sure Walt will comment from a first hand point of view, and the zip was one I missed in my "garage" of fighters I've flown. I'll take a shot at what you want and see how close it gets to being right anyway! :-) If I remember right, the BLC on the zip was actuated by a valve directly linked to the flap extension system. The EGT should be a function of the power percentage and nozzle position. I believe the EGT should be somewhere below 560 degrees on final with the BLC operative with flaps over 15 degrees. I don't remember what the visual indication was if any for the zipper to confirm BLC operation, but if memory serves, 82 to 85% rings a bell as a minimum on final to avoid uncommanded roll and sink. Keep in mind; I didn't fly this bird and am going on recall from hashing with some friends who did. Walt will have better answers for you I'm sure. Hope this helps a bit anyway. Dudley Henriques International Fighter Pilots Fellowship Commercial Pilot/ CFI Retired For personal email, please replace the at with what goes there and take out the Z's please! dhenriquesZatZearthZlinkZdotZnet "Scet" wrote in message ... When flaps are in the land position and boundary layer control is active, is there an increase in EGT that is sufficient to register on the cockpit gauge? If so, does the pilot look for the EGT rise to ensure the system is working? If not, is there an indication that the system is inoperative, is the aircrafts handling characteristics on approach indicative of system failure, or is it fail safe? Scet |
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