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     1. 05:10 PM - Re: RV9-List Digest: 5 Msgs - 03/18/05 (Leland)
 
 
 
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| Subject:  | Re: RV9-List Digest: 5 Msgs - 03/18/05 | 
      
      --> RV9-List message posted by: Leland <federigo@pacbell.net>
      
      I reported this problem to Scott at Van's a few weeks ago. Scott did not 
      feel that it was a problem since you don't normally operate an RV's 
      ailerons against the stops, except perhaps in aerobatics. To avoid 
      contact with the push rod, I had to file the bottom part of the hole 
      through the rear spar until it almost contacted the rivets holding the 
      aileron bracket on. Bryan Wood recently reported that his test pilot 
      found that he could completely lock the ailerons in the "full" position 
      when the pushrod caught in the spar. I believe this problem will 
      eventually kill somebody.
      
      Another safety problem I encountered was that the torque value on the 
      nuts holding the lead weights on the elevators had decreased in value 
      from 25 inch-pounds down to 5. Apparently the lead slowly creeps under 
      pressure over time. I finally attached the Nyloc nuts using permanent 
      thread lock and glued the lead weights, nuts and bolts on with ProSeal. 
      I also sanded down the thickness of two of the weights so that there was 
      more clearance between the horizontal stabilizer and the weights.
      Leland
      Getting close to done
      
      >Time: 08:31:05 AM PST US
      >Subject: RV9-List: Aileron pushrod clearance
      >From: Gerry Filby <gerf@gerf.com>
      >
      >--> RV9-List message posted by: Gerry Filby <gerf@gerf.com>
      >
      >
      >Wrapping up the last parts of the wings ... installed the 
      >aileron pushrods and bellcrank.  Disapointed to see that the 
      >steel pushrod fouls the edge of the openning in the rear spar 
      >at both limits of aileron movement.  The max deflection of the 
      >aileron is within the limits set in the construction manual 
      >(Section 15) but you can alread see that the powder coat on the 
      >pushrod is being marred.  Also, at max up deflection one of the 
      >rivet heads that secure the rod end "catches" on the edge of 
      >the opening - this worries me - I see potential for a jammed 
      >flight control.
      >
      >Its hard to see how this cannot have been a problem in every 
      >kit since there's not much latitude for positioning given that 
      >all the holes are prepunched.
      >
      >Anyone else have these issues ?
      >
      >g
      >  
      >
      
      
      
      
      
      
 
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