ATPL Performance - Class 6: Climbing.
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- Опубліковано 4 лют 2025
- ATPL Performance - Class 6: Climbing.
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Welcome to the 6th class in the Performance series.
After we take off we need to climb up to our cruising altitude. Depending on the environmental factors and aeroplane itself this climb will change. In this class we will look at how the climb angle and rate are altered.
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Aiming to assist with ATPL theory exams and the ground school aspect of ATPL training. Including helpful tips for studying and to use in the exam.
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Bro.....this is saving stuff......I'm on my way to the exam for my Flight Dispatcher Licence and this is helping me like A LOOOOOTTTTTT
You deserve a Gold Medal for this
This guy has the best atpl videos and the explanation is simple and easy to understand.
The train analogy is perfect 👍
I believe there to be a slight inaccuracy at 12:57 . It is mentioned that Vy is to be found between Vmp and Vmd, but Vy is always greater (or equal) to Vmd. At least this is what it makes us understand it as. Btw, thank you so much for the videos, not only on this subject but also the others, very good job :D
You’re so great man thank you 🙏
I don’t understand what you do with the fingers for Mach IAS and TAS. Could you please explain ?
Hi are these videos going over the topic or just a summary of the topic
Hey Grant, is this the last video of Performance or will you upload more?
Thank you for all your content
There will be some more for sure, probably about 10 or so more, just taking it easy over the Christmas period.
@@atplclassdamn man I’m actually doing performance I wish you will upload them soon much love
Can I please thank you for doing this. Your style of delivery makes thing really much easier to understand. Massively appreciate this.
@@atplclass sure thing. I just wanted to be sure before starting to study this subject. I hope you enjoyed Christmas and thank you so much for this content!
To be sure that i understood the analogy for the climb angle: flight path angle is the angle of the vertical trajectory of the plane over time whatever its attitude, and climb angle is the angle of the plane ?
Flight path angle: Where the plane is, compared to where it started on the ground draw a line and find the angle.
Pitch: aircraft nose compared to horizon.
Climb angle: vertical and horizontal comparison through the pocket of air it is currently flying.
In no wind conditions climb angle and FPA will be the same. But when we add in wind the pocket of air we are climbing through moves making the FPA lower (tailwind) or higher (headwind).
brand I can't get the train example right, may a graphic on that would help ! thanks !
unfortunately that it the best and simplest explanation i have
What's the name of song which goes in background at the beginning when you start to talk?
Mendex - Timeless (royalty free one hahah)
hello, whats the difference between excess power and excess thrust?
power is thrust over a period of time
thanks but when you write words, we cant read the letters because after the first alphabet the remaining alphabets are so small
That is just my handwriting mate
So am I right to call the climb angle angle of attack???
No. Angle of attack is between relative airflow and the chord of the wing. Whereas climb angle is based on the distance travelled through the air horizontally and vertically. Not to be confused with pitch angle which is just the angle between the main longitudinal axis of the plane and the horizon.
@@atplclass Thank you for the feedback
ROC=((T·TAS)-(D·TAS))/W, not ROC=((T-TAS)-(D·TAS))/W (the "·" instead of the "-" on the (T·TAS))