✅ Mental Math For Pilots | Easy Math Hacks Every Pilot Must Know

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In this video I will share with you hacks and tricks for simple mental math we pilots use in flight.
Mathematics for pilots.
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How to calculate crosswind component mentally and easily
How to calculate top of descent mentally and easily
How to calculate rate of descent easily and quickly
in-flight math for pilots
DME Arc distance calculation mentally and easily
All math required by pilots
How much math do pilot use
Rule of thumbs for pilots and shortcuts most tricks and hacks

Опубликовано:

15 сен 2024

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Комментарии : 64

@toddcianciulli921 Год назад

The crosswind math is genius as is the crab angle. Thank you very much for that.

@ATPLStudent Год назад

You're welcome I am glad you've found it helpful

@FA18Training 6 дней назад

At time 4min55, for me, TOD = ((Current Altitude -Target Altitude)/100)/desired angle of descent = ((Current Altitude -Target Altitude)/100)/3. In example time 5m42, my calcul is: TOD= ((5500-1500)/100)/3 = (4000/100)/3 = 40/3 = 13Na If we choice an angle of descent 5° TOD= ((5500-1500)/100)/5 = (4000/100)/5 = 40/5 = 8Na

@danielndala4598 2 года назад

I'm new but already fall in love with my first video on channel really thank you💞💞

@ATPLStudent 2 года назад

You’re welcome 😊

@MashaoSidwell 9 дней назад

I learned so much

@jacmwo9865 6 месяцев назад

I come your channel and it's very educative and easy to understand as i will be joining PPL classes in 5 months time from now,i thumb you up mate👍🏼!.Great work.

@ATPLStudent 6 месяцев назад

Thanks and welcome

@Lecichipsinc Месяц назад

Do it

@alejordann2fly411 Год назад

Gran Tip de video , me ayudo bastante en ejercicios de GNAV

@nikolamalakov8721 6 месяцев назад

Captain I have a question regarding the XWC. What if I encounter the situation of a tail wind. And it is above 90 degrees diference. Example: HDG 290 Wind from 170/20 290-170= 120 degrees difference 180-120= 60 degrees With the graph you provided 60 deg is WIND -1 so: XWC = 20-1 = 19 WCA = 8 degrees to the left HDG CORRECTED 288 degrees Is this simplification correct?

@fitrafi7645 2 года назад

Please do a similar version of admission test for emirates cadeT pilot training. Syllabus to cover, what maths and physics topic should we practice, what type of physics and maths can we expect during the training etc.

@yuvrajsharma1149 Год назад

Hey , do u know what to prepare for emirates pilot cadet assessment, as I am abt to go for it , pls

@cherrysoulmate6690 Год назад

@@yuvrajsharma1149 have you taken the assessment yet?

@IzlaNiya_ 8 дней назад

@@yuvrajsharma1149did you join?

@jhonatan64184 Год назад

Excelente video!!!! Muchas gracias 🙏

@ATPLStudent Год назад

De nada amigo

@FitXhub Год назад

Can you do another video on mental math on Hold/fuel calculations ? As well as more examples from this video please

@ATPLStudent Год назад

Sounds like a good idea, thank you for your suggestion will consider it.

@FitXhub Год назад

@@ATPLStudent thank you. Please soon!!

@Cosme422 Год назад

My suggestion is to please use a microphone so that the audio can have good quality. It’s a lot of noise.

@ATPLStudent Год назад

Thank you for your suggestion

@dusitthehto1946 Год назад

This is helpful thanks!

@ATPLStudent Год назад

You're very welcome mate

@AaronWbirdman 4 месяца назад

Great!

@1Mr.Legend1 Год назад

3:50 290-220=70 70*15=1050 1050/tas(100)= 10.5 degrees to wind.

@vaishnavraj5205 2 года назад

superb sir thank you sir

@ATPLStudent 2 года назад

All the best

@mrsumeetsaxena Год назад

Good One !

@ATPLStudent Год назад

Thank you

@bruno84 11 месяцев назад

How can you assume the WCA is half of the crosswind component without taking into account your airspeed? Your example would only apply if your were flying at 120kts. Any other speed and you'd have to apply a different w.c.a..

@ATPLStudent 11 месяцев назад

You are right, that is why I mentioned that that method is applicable mostly for General Aviation and single engine low performance aircraft where the TAS is about 100 to 130 kts

@bruno84 11 месяцев назад

I didn't see you mentioning it. That's why I commented so that people wouldn't think it would be always half the crosswind coponent. Anyway one easy rule to calculate your w.c.a. with any aircraft and speed is to divide the crosswind component by your speed in Nautical Miles per Minute. E.g. 120kt = 2nm/min. Given a 20kt crosswind: 20/2 = 10 degree w.c.a. 300kt (5nm/min) 20/5 = 4 degree w.c.a. Easy to apply to any speed. Still, thanks for the video!

@ATPLStudent 11 месяцев назад

@@bruno84 Thank you for your comment as well as for the trick, I learned something today. Much appreciated

@Zfx13 9 месяцев назад

The DME ARC rule can be used for NBD arcs as well?

@ATPLStudent 9 месяцев назад

Of course it can, provided you know the radius of the arc (how far away the arc from the NDB) if it’s about 13/14/15/16 miles then you may use the rule of thumb as explained in the above video.

@koller8930 3 месяца назад

I can do fourier and laplace tranform with pen and paper But I can't do 84*24 in my head in under 30sec .... :/

@VinceCartierBeats Год назад

Why did you mulipl GS*5 for rate of descent. Just trying to get an understanding of where you got the 5 from and not any other number?

@ATPLStudent Год назад

It's a rule of thumbs for easy mental math. it comes from the glide path in percent 3 degree glide path = 5.2% so it is actually GS x 5.2 but we drop the 0.2. If you want to go deeper of where it comes, you will find out that it comes a result of basic trigonometry

@VinceCartierBeats Год назад

@@ATPLStudent thank you man!

@donolsen6141 2 года назад

Are calculators allowed when factors like sinus come in play? And are basic calculators there in the interviews, or is it purely mental! Thanks for the vid btw!

@ATPLStudent 2 года назад

You hardly ever get to use sin and cos in flight, there are many rules if thumb for most of the calculations needed in flight, so don’t worry about that. As for ground school especially in Gnav and Mass and balance you are allowed to use a calculator. In interviews they only expect you to know rules of thumb and 1 in 60 rule and other very basic mental calculations just like the ones demonstrated in the video above.

@donolsen6141 2 года назад

@@ATPLStudent Thank you very Much!

@louditalian1962 2 года назад

Once you get the hang of it is easy.

@isaiah732 11 месяцев назад

For real, once you write main takeaways, and breakdown the formulas(which he’s already done) it’s very easy

@dsd-downshiftdave8056 8 месяцев назад

Did I miss something how did you get FL260- FL110= 15000ft- isn't cruise altitude 5500 minus target altitude 1500 would be 4000 Which would make rate of decent 4000/10= 400

@ATPLStudent 8 месяцев назад

I think you are confusing two examples with each other. FL260 is 26000 and FL110 is 11000. So, 26000 - 11000 = 15000 Got it ?

@dsd-downshiftdave8056 8 месяцев назад

@@ATPLStudent I must have missed that somewhere- at what part of the video is that

@FitXhub Год назад

Why do you divide by 4 on the DME arc ?

@ATPLStudent Год назад

Because of the 1 in 60 rule. For a 60 NM DME Arc each degree is1 min 30 NM DME Arc each degree is 30 sec 15 NM DME Arc each degree is 15 sec and since this calculation is merely a rule of thumb we consider 12/13/14 all as 15NM DME Arc. because of 15 seconds is 1/4 of a minute we multiply by 1/4 or simply divide by 4 the difference in radials. Hope this has clarified your doubt

@ihorkohut7290 2 года назад

Cool tips, thanks!

@ATPLStudent 2 года назад

No problem!

@criminalsxxx4394 Год назад

How are you figuring this out in the air? You got a calculator ?

@ATPLStudent Год назад

You don't need a calculator, you will get used to it with practice

@1Mr.Legend1 Год назад

5:33 Your calculation does not match exactly. This is correct; 5500-1500=4000ft GS120KTS 120kts/60h=2nm path per munite 4000ft/600fpm=6,66 minute (descends in 6.66 minutes with 600fpm) 6,66*2= 13,32nm. (it make progress 13.32 nm in 6,66 minutes at 120 kts.)

@ATPLStudent Год назад

You are using two different methods at the same time. you wont get the correct answer that way. I see the point you're trying to make here but that method of your corresponds to high altitude/high performance aircraft where during the descent the GS changes. if you are looking for Propeller/Low Altitude operations stick to the method in the video it's pretty accurate to manage your VNAV profile/TOD. thanks for your comment

@1Mr.Legend1 Год назад

No, I just calculated it on 120 kts. The process changes if we take wind into calculate. You shared a method without taking the wind into calculate, but it was not exactly correct.@@ATPLStudent

@USA2041 10 месяцев назад

My dear are there another formula for arc distance anyway 🙋‍♂️🙏

@ATPLStudent 10 месяцев назад

Thanks for watching buddy, I'm afraid the 1 in 60 rule is the best Rule of Thumb to find ARC distances

@tsunghanlee9044 2 года назад

GIVEN: True course : 105 degree , True heading : 085 degree , True airspeed : 95 kts , Groundspeed : 87 kts. Determine the wind direction and speed. (A)020 degree and 32 knots. (B)030 degree and 38 knots. (C)200 degree and 32 knots. According to u video the answer should be (B) but the answer is A why?

@richievaldez3607 Год назад

105-085= 20 degrees 95-87= 8kts crosswind According to table, 20 degrees is closer to 15 degrees off track = 1/4 of wind speed so: 8x4= 32kts wind speed So answer (A) is correct.