Net t/o flight path - 2nd seg ?

[tathepilot]

sorry I don't have a whiz wheel anymore... It's all good, doing an ATP type... the performance class that my company gave was half-azz so it was hard for me to understand the finer points...

that is not an excuse, i know that im not perfect, my oral was rescheduled a week earlier so i needed the help and i got it so thanks...!!!!

 

[MauleSkinner]

As far as I know, there are three of us in the entire world that still carry one...just didn't know you weren't one of us.

Fly safe!

David

 

[tathepilot]

It's the second-easiest way to answer your question...the easiest would be to look under 100 knots in the rate of climb table and read 592, move the decimal point two places to the left, and get 5.92% climb gradient required.

Fly safe!

David

wow, extremely accurate.. thx.

 

[FastJP4]

Rise over run = percentage

360 divided by 6076 = .0059249 X 100 yields 5.92%


Percentage X run divided by 100 = rise

5.92 X 6076 = 35969.92 divided by 100 = 359.6992 or 360

Substitute your 3.5%

3.5 X 6076 = 21266 divided by 100 = 212.66

Two important equations you should store in your brains hard drive.

 

[tathepilot]

Rise over run = percentage

360 divided by 6076 = .0059249 X 100 yields 5.92%


Percentage X run divided by 100 = rise

5.92 X 6076 = 35969.92 divided by 100 = 359.6992 or 360

Substitute your 3.5%

3.5 X 6076 = 21266 divided by 100 = 212.66

Two important equations you should store in your brains hard drive.

Thanks!!