Thank you for this simple explanation. I wish all my lessons were taught with Pusheen xD
@user-wo4mr6he2e8 күн бұрын
my brain liked the video but my neck did not lol
@Matthew93169 күн бұрын
amazing video - you explained it well! thank you!!
@D1566818 күн бұрын
Hey man great explanation, I’m trying to incorporate this into my lesson plans but can’t find it anywhere in the afm or phak, did you reference any books or acs for this? If so lmk please just in case the Dpe asks lol. Thanks again
@flightdeckq400pilot422 күн бұрын
YOU'VE MADE EXCELLENT TUTORIALS.....I RECOMMEND THESE TO ALL AIRLINE PILOTS AS REFRESH EXERCISES BECAUSE WITH TIME MANY THINGS FADE FROM MEMORY...CONTINUE THIS AND IF POSSIBLE VIDEOS ON HUMAN FACTORS AND MET WOULD BE USEFUL....
@itsfrank541229 күн бұрын
This video helped me a lot more than the rest! Should have more views. Thank you!
@dancrosby6091Ай бұрын
Liked this video so much I subscribed. Very informative and easy to follow.
@konansarah5961Ай бұрын
Hi, sorry im not to familiar with the term cruising faster or slower what does that mean for the range and endurance of the plane?
@believeachieve2847Ай бұрын
Love it, nice and simple. Lolol to the cats...like a CAT approach...clever
@lilbard3100Ай бұрын
this helped me a ton in understanding. Thank you so much
@_yakashiiАй бұрын
Great explanation
@micstonemic696stoneАй бұрын
N1 is the gas pressure after the compressors when entering the burn chamber and often used when starting the engine Itt is not used with a fan type engine and egt normally is normally is engine exhaust temperature Back to the drawing board with your attempt at educating others Sorry fella but facts are facts
@PilotFlyingJay2 ай бұрын
Wow thank you so much !!!!! This was the best explanation I’ve found… so many videos that are 30-40 minutes that I don’t understand and this completely broke it down to simple English, thank you !!!
@Dana_Bellamy2 ай бұрын
FANTASTIC explanation!! Thank you so much for sharing!!
@_miguel_tenorio2 ай бұрын
I really needed to watch this. Thank you
@DJeb862 ай бұрын
Can we use the rudder to maintain altitude during a turn ? Is this what is referred ad coordinated flight ?
@nimbapilot69258 күн бұрын
This may be too late but the answers to your question is No. you cannot used to keep the aircraft coordinated. This will keep the aircraft from skipping and skidding; and potentially get yourself into stall spin situations depending on the maneuver you are doing. Rudder usage is very important during stall maneuvers.
@DJeb868 күн бұрын
@@nimbapilot6925 great thanks, so what does a coordinated turn mean ?
@francisalgoso42412 ай бұрын
Thank you very much for the video!!
@TheChauole2 ай бұрын
Amazing video, but may I ask why the fuck is there music in the background? Bad call
@theiaminu53753 ай бұрын
You have never seen an actual vacuum gauge attached to an engine have you ?,,,, the engine will have the highest vacuum at closed throttle and the lowest vacuum at wide open throttle ....What you are describing would only happen outside the throttle valve ...
@maxcfi77183 ай бұрын
this is not a vacuum gauge as i’ve explained before. it is a manifold pressure gauge.
@theiaminu53753 ай бұрын
@@maxcfi7718 The manifold pressure is a vacuum the entire time the engine is running unless you have a supercharger ...the "pressure gauge will have numbers on both sides of zero .... all pressures are relative to atmospheric pressure ,,,, we do not take them to space to calibrate them .....
@maxcfi77183 ай бұрын
@@theiaminu5375 yes, but this is measuring the actual pressure in the manifold. hence why it’s lower when the throttle is closed and equal to atmospheric pressure when throttle is wide open (for a naturally aspirated engine.) my understanding is a vacuum gauge would measure the difference between atmospheric pressure and the manifold pressure, so it reads higher with the throttle closed. we do not normally measure vacuum on the engine in aviation
@theiaminu53753 ай бұрын
@@maxcfi7718 It's backward from what you would encounter in the REAL world ... low is to the left (counterclockwise)and high is to the right (clockwise) in every gauge you will find ....Even on a mass spectrometer ...
@maxcfi77183 ай бұрын
@@theiaminu5375 yes? and it is also on the manifold pressure gauge. not understanding what you’re getting at 😂
@Flow-.-3 ай бұрын
Simple yet perfect. Thank you.
@flyingplumber35653 ай бұрын
I’ve never truly understood weight and balance until now . Thank you !! lol
@jacksonbryantfilms3 ай бұрын
Dawg I can’t hear a word you’re saying over the music
@thevinylreview3 ай бұрын
Great explanation thank you so much
@benjaminsandor63493 ай бұрын
Thanks! Helps a lot! Learning to be a ramp agent at the moment
@jazzmeet69233 ай бұрын
Best explanation buddy. Thanks alott
@CashMoney52803 ай бұрын
Great content! I appreciate the knowledge THANK YOU.
@nelsonmorales49124 ай бұрын
Sir , with all your Respect . Aviation is a very serious Matter. Meaning that an individual that is learning the trade Needs to concentrate in what he or she is Learning. As a Matter of advice , Eliminate the Dinner Music and get Down To business.
@justinsmall70904 ай бұрын
Thank you sir for this video!
@MrMisterUtube4 ай бұрын
If IAS is = Static + RAM pressure, why is wind not affecting the RAM pressure? Lets say a headwind, Isn't wind cramming air molecules into the pitot?
@JRC03043 ай бұрын
I think it’s because all the ground speed you lose with a headwind still appears on your asi. Like 120kt ias with a 30kt headwind your ground speed is 90 kts but the extra 30kt headwind is still giving you the 120kt reading on your asi. So the wind is constantly affecting the Ram pressure which is why we calculate groundspeed. Don’t trust me on that though I’m kind of dumb lol.
@klugaric4 ай бұрын
In the equation Weight x Arm = Moment, why did you divide both sides with weight because from mentioned equation Arm = Moment/Weight already? It is not needed to divide it with weight.
@maxcfi77184 ай бұрын
i was deriving the other version of the equation. to go from weight*arm=moment to arm=moment/weight you must divide both sides by weight
@klugaric4 ай бұрын
I still don't understand why. 😄 If 3x2=6, then 2=6/3 If weight x arm = moment, then arm = moment/weight. You get the same equation without dividing both sides with weight. So my question is why the one would do that? P.S. Thanks for the videos, they are very helpful for understanding my PPL literature.
@maxcfi77184 ай бұрын
@@klugaric when you divide by weight on both sides it is in the denominator on both sides. so you end up with (weight*arm)/weight on the left side of the equation. weight cancels and you’re left with just arm on the left side of the equation. on the right side, you get moment/weight and nothing cancels. so you end up arm = moment/weight. this is the process you’re doing when you go between those equations, whether you know it or not. you are smart enough to just see how the equation can be changed without actually writing out the algebra but that is what you’re doing implicitly when you change the equation in that way.
@timw66974 ай бұрын
Mind if I ask were you got that model? (Im looking for a few)
@maxcfi77184 ай бұрын
it was a plastic model i bought and built from a hobby shop! not sure the brand
@mikemorell10574 ай бұрын
Amazing video
@mojo76184 ай бұрын
“You fly the approach as it wasn’t there “
@thejourney4434 ай бұрын
helped me so much. thank you
@redbaron89895 ай бұрын
Excellent tutorial. Best I’ve seen. Love how you incorporate using the different charts after crunching the numbers.
@shrik12345675 ай бұрын
Hi , is N1 only called NG on turboprop engine .? because there is also NP indicator .
@hl68595 ай бұрын
Thank you.
@zaharbj85945 ай бұрын
Excellent video made, it is clearly obvious that you put efforts into creating such a content, I really enjoyed and found this helpful. This video is very step by step informative even though it doesnt contain any single word, nevertheless it makes that format even more self-explanatory. I would really appreciate similar videos from you of the same type and length on other A320 procedures!
@nimbapilot69255 ай бұрын
thanks for the video
@maxcfi77185 ай бұрын
you’re welcome! side note - I used to live in Liberia!
@nimbapilot69255 ай бұрын
@@maxcfi7718 Oh really? Nice! how do you like being a cfi? we should link up sometime!
@paidtourist65635 ай бұрын
Im still confused as to why indocated speed and true air speed are needed. Just doesn't make sense to me why anyone would need to know how fast the air molecules are moving as opposed to ground speed. To me ground speed is the only speed that is relevant. Thats the speed it takes to you arrive from point A to point B right?
@maxcfi77185 ай бұрын
you need your true airspeed to calculate your ground speed. true airspeed plus headwind/tailwind component will give your ground speed
@user-of2iz1ft5c3 ай бұрын
Think about it like this, you need to know rate and number of the air molecules passing over the wings, because the rate at which they’re passing impacts whether you’re about to stall and airflow is about to breakdown or whether it’s about to rip your wings off - IAS. You need to know the speed of the air molecules passing in general so that you know how fast the actual aircraft is moving through the air, regardless of the number of molecules, their temperature etc in order to work out how was you will arrive somewhere - TAS.
@johnyx.official5 ай бұрын
Believe it or not, but you just helped me, making my first landing in DCS World 😅
@subaruford33445 ай бұрын
Question, how would one correct the altimeter after it made an error due to strong vertical gusts?
@subaruford33445 ай бұрын
That clicked, thank you!
@timdiggens70255 ай бұрын
Super helpful to recap pre check ride
@Tyleraviator995 ай бұрын
hey, on a cessna 172 basic empty weight includes unusable fuel so for fuel you would only do 37 gallons (if you are on a separate model then disregard)
@maxcfi77185 ай бұрын
check the manual but i believe it’s 40 gallons usable, the unusable fuel is in addition to that
@Tyleraviator995 ай бұрын
@@maxcfi7718 oh ok. I thought in a previous video you said that 40 is total
@maxcfi77185 ай бұрын
@@Tyleraviator99 it is total usable. we don’t count unusable, it’s already in the basic weight
@Tyleraviator995 ай бұрын
@@maxcfi7718 ok. Thank you!
@sunandgratitude75365 ай бұрын
Thank you so much for this. I can't tell you how much the visual helps. I was struggling with this but you've made it crystal clear. Thank you!!
@alianacawley18975 ай бұрын
Best airspeed video ever!
@elainegmorrison5 ай бұрын
I was always thinking of TAS increasing, not KIAS decreasing. And TAS was this mythical number that increased as you experienced decreased performance. This makes more sense.
@jfvillafuerte5 ай бұрын
Thanks for the tutorial, this information is very helpful!
@bekomcar5546 ай бұрын
Can diesel engine MAP value with turbo charger during idle have the atmospheric pressure?