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Old 27th Jul 2012, 15:24
  #118 (permalink)  
Join Date: Jan 2006
Location: Europe
Posts: 403
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!
Transsonic2000 is offline