Pretty solid explanation! A couple of things to note though: 1) Rudder Boost is not an autopilot function. It is a function of the bleed air system which senses an increased pressure differential between engines if one is running at a higher power setting than the other. The rudder will be deflected into the direction of the higher power engine (single engine failure) to help control yaw in that emergency situation. A psi diff (PSID) of 60 psi will trigger rudder boost. 2) Engine auto ignition is not required for engine start. When the engine start switches are selected to "Ignition and Engine Start" the ignitors will fire as a function of that switch position. Engine auto ignition is armed prior to departure and will turn the ignitors on during low power phases of flight (flight in turbulence or in the descent) which is where engine flame out is likely to occur if flight in cloud occurs. Engine auto ignition once armed is triggered by a reduced power setting and is sensed as a function of torque. 3) Once the gen is online and powering the system unless it has a fault which will display a caution and CAS/annunciator there is no need to reset the right hand gen after the second engine start. You do have very good knowledge of the aircraft though! Hope this helps.
Google translator. Your tutorials are extraordinary, for me not knowing English is a problem. Some have Spanish subtitles. Yes, you can upload them with automatic subtitles in Spanish.
@@supanova88 wish you and family always healthy and have a great day, Sir. Anyway, that King Air looks cool, does Airfoillabs made other series of King Air as well ?
Pretty solid explanation! A couple of things to note though:
1) Rudder Boost is not an autopilot function. It is a function of the bleed air system which senses an increased pressure differential between engines if one is running at a higher power setting than the other. The rudder will be deflected into the direction of the higher power engine (single engine failure) to help control yaw in that emergency situation. A psi diff (PSID) of 60 psi will trigger rudder boost.
2) Engine auto ignition is not required for engine start. When the engine start switches are selected to "Ignition and Engine Start" the ignitors will fire as a function of that switch position. Engine auto ignition is armed prior to departure and will turn the ignitors on during low power phases of flight (flight in turbulence or in the descent) which is where engine flame out is likely to occur if flight in cloud occurs. Engine auto ignition once armed is triggered by a reduced power setting and is sensed as a function of torque.
3) Once the gen is online and powering the system unless it has a fault which will display a caution and CAS/annunciator there is no need to reset the right hand gen after the second engine start.
You do have very good knowledge of the aircraft though! Hope this helps.
Thanks for your input. I really appreciate it. It's an interesting aircraft.
Great stuff! Always been a fan, your BMS videos did me a world of favours a few years ago!
Thanks for your kind words. I really appreciate it.
Thank you for a great video! Love the way youre flow in explaining the systems along the actual check list items! Really Great! :)
Thanks for your kind comment.
Google translator.
Your tutorials are extraordinary, for me not knowing English is a problem. Some have Spanish subtitles.
Yes, you can upload them with automatic subtitles in Spanish.
I'm glad you found them. If anyone wants to provide foreign language subtitles that are TH-cam ready I would be happy to include them.
Hello Supanova or Mr. Falcon 4 BMS 😊
And hello to you. ;)
@@supanova88 wish you and family always healthy and have a great day, Sir.
Anyway, that King Air looks cool, does Airfoillabs made other series of King Air as well ?
Thank you
You're welcome. :)
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