Hi,
Many thanks for all of your answers.
My initial question was about, how to have in mind an order of magnitude of the likely acceleration stop distance, a Boeing 777-300 would need at full load.
(345 T, Full thrust, 15°C, Seal level, wet runway)
I had in mind, that a B777-200ER at roughly 200 Tons, would need at the same conditions listed above, 1300 Meters (4200 ft), right ?
As you know, the Boeing Laptop Tool, doesn't give this kind of informations.
One more time, I wanted to know this information just about a good "Situational Awerness" as nice to know !...
Best,
Skylark
