SURFACE DEICE SYSTEM and TRANSPONDER
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Hi all, when I execute the BEFORE TAKEOFF CHECKLIST of the Baron 58P I noticed that SURFACE DEICE SYSTEM test has something different from POH. Here there is this note: "When surface deice system is not in operation, Deice Pressure Gage should read approximately 4.5 to 5.5 psi". In the modeled aircraft the deice pressure gage, when surface deice system is not in operation, is always at zero.
About the transponder, I noticed that when I activate the avionic switch the Garmin GTX 327 transponder operetional status is ALT mode and the transponder of TDS GTNXi 750 is in STBY mode.