Відео

great video.

Great video. Very informative and helpful!

Great Explanation! Could be renamed "Airspeed for Dummies"!

Man, your physical example with the ruler, string, and water bottle makes the abstract real. Great demo. I wish all aviation subjects were simple like that.

Can you please explain why VX increase with altitude and VY decrease with altitude?

Explanation seems contrary to auto engine with a vacuum gage. In that application, gage will show 0 inches of hg. when throttle is wide open, but about 20 inches at idle. Still confused here. Apparently your manifold pressure gage, calibrated in inches of mercury, operates differently than a common vacuum gage??? Seems like your gage would change its reading just due to changes of elevation above sea level.

Very clear. The illustrations were key. They really are a great supplement to your verbal explanation. Too many teachers try to complicate their subject probably to demonstrate their own intelligence----------not what a teacher is there to do!

Good shit

Thank for the post, I have a Stinson V-77 Reliant that has exact same pneumatic flaps system.

Wait, nonprecision and precision rnav have lnav minima?

Prob the best video out there on this topic I’ve seen

Cool illustrations

Thanks great video

Excellent explanation

IR exams in 6 days, this video saved my life

Your explanations and diagrams are excellent. Hope you can make more despite lower than deserved views

Great Video for Aviation High School

Great video.

Very good video! (as you say the POH is somewhat lacking in detail). While writing do you happen to know what is the reason you mentioned that in norm both pumps run together, but in high only one runs (and which of the two depends on the switch position), seems a bit counter intuitive - for example in norm they could alternate every 30 seconds ? Perhaps it is related to redundancy.

Best explanation for Vy and Vx!❤

Thank you you very helpful

Thank you for this! This is the best video I've seen thus far explaining the cg effects on an airplane.

wouldnt the IAS be the same because the static port is accounting for less air molecules at higher altitudes?

My instructor was saying something about usable, fuel, and non-usable fuel at takeoff. so if you had 50 gallons to calculate you calculate 48 instead usable fuel

Exactly what I was looking for. Easy to follow, each component was adequately explained but to the point, the data was laid out beautifully. This is professional teacher level. You rock man!

Wow thank you. I have my checkride tomorrow in a DA42. This was clutch

PLEASE SOMEONE HOW DO YOU FIND THE BASIC MOMENT OF A PLANE I’m going actually insane?!? I can’t find the arm of empty weight for a Cessna 150 1976’s Commuter II.

Been a quick minute since I've flown the twinstar and am revising it's systems for an upcoming interview. Like you I have always found the manual for this aircraft the be seriously lacking. Great job on the video, very well explained.

Great video 🙌🏽

Can we say that critical angle of attack is lower with forward cg because stall speed is higher? On the other hand cl max is higher because we need to produce more lift?

Yes! This is simple and clear. A lot of other videos talking about vortices causes induced drag and I think that argument is wrong. Induced drag is caused by angle of attack and vortices causes down wash airflow, which reduced the lift. In order to create the same amount of lift, angle of attack needs to be increased, which in turn creates more induced drag.

Thank you for the explanation!

This is the best video out there to explaining this! Simple yet effective. Thank you! I will use this w my students

maxcfi, thank you so much for this awesome, visual video my man! I'm writing curriculum for an aviation maintenance high school course, and this video was so clear and understandable! You rock dude!

You made this incredibly easy to understand

Brilliantly explained!

Thank you for this simple explanation. I wish all my lessons were taught with Pusheen xD

my brain liked the video but my neck did not lol

amazing video - you explained it well! thank you!!

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....

This video helped me a lot more than the rest! Should have more views. Thank you!

Liked this video so much I subscribed. Very informative and easy to follow.

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?

Love it, nice and simple. Lolol to the cats...like a CAT approach...clever

this helped me a ton in understanding. Thank you so much

Great explanation

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

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 !!!

FANTASTIC explanation!! Thank you so much for sharing!!

I really needed to watch this. Thank you