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Manoeuver Load Diagram | Your ATPL guide to the V-N diagram.

  Рет қаралды 28,199

flight-club

flight-club

Күн бұрын

A simple explanation of a chart that shows the LOAD FACTOR LIMITS at certain airspeeds of a typical aeroplane.
0:00 Start
0:21 EAS axis
0:55 Load Factor axis
1:40 Positive Manoeuvre Boundary
1:53 Negative Manoeuvre Boundary
2:15 Stall Speed Vs
2:27 Positive Load Factor Limit Va
3:56 Maximum Positive and Negative Load Factor Limits
4:14 Design Cruise Speed Vc
4:50 Design Diving Speed Vd
Learn more about this topic in these videos:
• What is the Load Factor?
• All the V SPEEDS you n...
• What is COFFIN CORNER?
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Thanks for watching!

Пікірлер: 17
@Echo_Lima
@Echo_Lima Жыл бұрын
You helped me pass Pof , thank you very much for your videos .
@NicoQtn
@NicoQtn 2 жыл бұрын
Very useful :) Those animations are always spot on ! Thanks a lot
@flightclubonline
@flightclubonline 2 жыл бұрын
Glad you think so!
@ralfsingmann6580
@ralfsingmann6580 2 жыл бұрын
Simply perfect and I always recommend your channel to student pilots
@flightclubonline
@flightclubonline 2 жыл бұрын
Much appreciated!
@raccoonair
@raccoonair 2 жыл бұрын
Absolute perfect! Thank you...
@flightclubonline
@flightclubonline 2 жыл бұрын
Glad you like it!
@farayidarlingtonchaparadza20
@farayidarlingtonchaparadza20 Жыл бұрын
Clear and concise. Thank you
@ki6893
@ki6893 9 ай бұрын
Good lecture!From japan
@MyEmpire91
@MyEmpire91 2 жыл бұрын
This is incredible good. thank you!
@flightclubonline
@flightclubonline 2 жыл бұрын
You're very welcome!
@drseven1275
@drseven1275 2 жыл бұрын
Fantastic !! 🙏🙏🙏👍👍👍
@flightclubonline
@flightclubonline 2 жыл бұрын
Many thanks
@Echo_Lima
@Echo_Lima Жыл бұрын
can you make one video also for the gust diagram ? thank you very much !
@noshinmridula8399
@noshinmridula8399 2 жыл бұрын
Please make a video on screen height
@sabellex5609
@sabellex5609 Жыл бұрын
Va is not directly at 2,5 LF ; its sligthly behind
@dylanpachuca1844
@dylanpachuca1844 2 ай бұрын
Every airplane is different load factor limit for positive on archer is 4.4 G at utility category. And va in our archer is found by doing a formula is “Va @ max (113) * √(current airplane weight/max weight)= Va. also the Va is always changing as fuel is being consumed
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