-T / T / +T | Comment(s)

Monday, August 11, 2003

'A Single Fastener in a Critical Flight Control Link'

ALPA's discussion of DC-8 pitch control design issues: Split Controls Unlike newer transport aircraft, the left and right sides of the DC-8's pitch control system cannot be isolated from one another in the event of a jam or malfunction on one side. The DC-8 was certificated in 1959, while the FARs [Federal...

 
Having trouble logging in? Contact Client Services at (301) 354-2100 or clientservices@accessintel.com.

This story is only available to paid subscribers. Please login below with your username and password if you are a subscriber.

Username:
Password:
What is my password?
blog comments powered by Disqus