cigogne
I love flying!
Hi,
I'm building a Gaz'Aile aircraft (gazaile261.free.fr/indexAE.html) and plan to installing a Dynon glass panel (SkyView, radio, AutoPilot, transponder, 2x10" displays....).
I read the manuals thoroughly (for documentation sake... and also to dream a bit to be honest!) and I'm not sure about the "with full power" AOA calibration process…. May be because of my English… :-[
Does this mean that we have dynamically stall (this would be unsafe for the structure especially with full flaps)? More likely are the "with full power" tests (no flaps/full flaps) used to setup the AOA for taking off and go-around conditions? In this instance the test would consist in slowing down very close to the stall (by jotting down the stall speed found with no power in the same configuration), hit “STALL” button, go to full power, and pull the nose up to enter the stall.
Am I guessing right?
Thanks and regards.
I'm building a Gaz'Aile aircraft (gazaile261.free.fr/indexAE.html) and plan to installing a Dynon glass panel (SkyView, radio, AutoPilot, transponder, 2x10" displays....).
I read the manuals thoroughly (for documentation sake... and also to dream a bit to be honest!) and I'm not sure about the "with full power" AOA calibration process…. May be because of my English… :-[
Does this mean that we have dynamically stall (this would be unsafe for the structure especially with full flaps)? More likely are the "with full power" tests (no flaps/full flaps) used to setup the AOA for taking off and go-around conditions? In this instance the test would consist in slowing down very close to the stall (by jotting down the stall speed found with no power in the same configuration), hit “STALL” button, go to full power, and pull the nose up to enter the stall.
Am I guessing right?
Thanks and regards.