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Thread: MAX’s Return Delayed by FAA Reevaluation of 737 Safety Procedures
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Old 15th Jun 2019, 09:34
  #425 (permalink)  
Peter H
 
Join Date: Jun 2008
Location: Cambridge UK
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Originally Posted by DaveReidUK
I'd be very surprised if there is/was much scope for redesigning the stab pivot and/or the jackscrew geometry in a way that would significantly reduce the aerodynamic loads on the jackscrew (and therefore on the trim wheel).
Discussed to some extent over in Tech Log at THS hinge point
Last edited by Peter H; 16th Jun 2019 at 11:34. Reason: Previous link not working.
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