Performance - Landing (Class A)
Hi all,
just came across this (apparently) weird question, can someone explain how to figure out the correct answer or am I missing something?
At maximum landing mass, the structure of the aircraft is designed for a rate of descent:
- 250 fpm
- 600 fpm
- 200 fpm (this would be the correct answer, but how is this figured out, is there a formula or something )
- 220 fpm
Thanks in advance!
And I need a brake now!