Yak-List Digest Archive

Thu 10/11/12


Total Messages Posted: 4



Today's Message Index:
----------------------
 
     1. 06:00 PM - AD notes for Yaks & CJs (cjpilot710@aol.com)
     2. 08:49 PM - Re: AD notes for Yaks & CJs (Walter Lannon)
     3. 08:51 PM - Re: AD notes for Yaks & CJs (Dale)
     4. 09:55 PM - Re: CJ-6 Engine trouble (jetjockey)
 
 
 


Message 1


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    Time: 06:00:32 PM PST US
    From: cjpilot710@aol.com
    Subject: AD notes for Yaks & CJs
    I know a goodly number of those on the Yak-list are not RPA members, and thus most likely didn't get the email alert about two incidences involving a Yak and a CJ. I've copied the text only. I think its a good idea to share this info right away. Recently, an Australian Yak-52TW was in a descent at 240 MPH. The aircraft had a sudden onset of an audible drone rapidly followed by a loud bang. The aircraft then vibrated violently. The trim tab broke into 4 parts. Only one of the parts remained on the elevator. The trim tab push rod also broke at the attachment point. Notice the cracked elevator skin above the torque tube. In addition to the trim tab and left elevator, the engine rubber mounts were also broken. A complete analysis of this incident is still pending. However, the RPA is asking all TW owners specifically and all 52 owners in general to routinely preflight all trim system components for wear and excessive play. The elapsed time between the onset of the drone noise and the vibration was 1-2 seconds. The pilot was able to slow the aircraft down and land without incident. The aircraft was new in 2004 and only has 245 hours total time. the aircraft is used for aerobatics less than 5% of the time and has been well maintained. The trim tab broke into 4 parts. Only one of the parts remained on the elevator. The trim tab push rod also broke at the attachment point. Notice the cracked elevator skin above the torque tube. In addition to the trim tab and left elevator, the engine rubber mounts were also broken. A complete analysis of this incident is still pending. However, the RPA is asking all TW owners specifically and all 52 owners in general to routinely preflight all trim system components for wear and excessive play. ____________________________________________________________________________ ____ Bill Blackwell notified Scott Andrews today of a cracked rudder counterbalance weight tube he found while performing a conditional inspection. Scott informed as many of the Phoenix area CJ owners as he could to inspect their aircraft. They found one aircraft with a welded patch on the counterbalance arm that was probably done in China. This picture shows the location of the crack. It is below the rudder bell crank and just above the 90 degree support bracket. This picture shows the repair Bill made to the tube. It does not show the crack he found.


    Message 2


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    Time: 08:49:27 PM PST US
    From: "Walter Lannon" <wlannon@shaw.ca>
    Subject: Re: AD notes for Yaks & CJs
    Pappy; Could you post the photos? Very interested in the CJ balance arm crack. Many thanks; Walt From: cjpilot710@aol.com Sent: Thursday, October 11, 2012 5:57 PM Subject: Yak-List: AD notes for Yaks & CJs I know a goodly number of those on the Yak-list are not RPA members, and thus most likely didn't get the email alert about two incidences involving a Yak and a CJ. I've copied the text only. I think its a good idea to share this info right away. Recently, an Australian Yak-52TW was in a descent at 240 MPH. The aircraft had a sudden onset of an audible drone rapidly followed by a loud bang. The aircraft then vibrated violently. The trim tab broke into 4 parts. Only one of the parts remained on the elevator. The trim tab push rod also broke at the attachment point. Notice the cracked elevator skin above the torque tube. In addition to the trim tab and left elevator, the engine rubber mounts were also broken. A complete analysis of this incident is still pending. However, the RPA is asking all TW owners specifically and all 52 owners in general to routinely preflight all trim system components for wear and excessive play. The elapsed time between the onset of the drone noise and the vibration was 1-2 seconds. The pilot was able to slow the aircraft down and land without incident. The aircraft was new in 2004 and only has 245 hours total time. the aircraft is used for aerobatics less than 5% of the time and has been well maintained. The trim tab broke into 4 parts. Only one of the parts remained on the elevator. The trim tab push rod also broke at the attachment point. Notice the cracked elevator skin above the torque tube. In addition to the trim tab and left elevator, the engine rubber mounts were also broken. A complete analysis of this incident is still pending. However, the RPA is asking all TW owners specifically and all 52 owners in general to routinely preflight all trim system components for wear and excessive play. _________________________________________________________________________ _______ Bill Blackwell notified Scott Andrews today of a cracked rudder counterbalance weight tube he found while performing a conditional inspection. Scott informed as many of the Phoenix area CJ owners as he could to inspect their aircraft. They found one aircraft with a welded patch on the counterbalance arm that was probably done in China. This picture shows the location of the crack. It is below the rudder bell crank and just above the 90 degree support bracket. This picture shows the repair Bill made to the tube. It does not show the crack he found.


    Message 3


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    Time: 08:51:24 PM PST US
    Subject: Re: AD notes for Yaks & CJs
    From: "Dale" <dale@frii.com>
    Only 240 mph? Why the slow down. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=385159#385159


    Message 4


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    Time: 09:55:29 PM PST US
    Subject: Re: CJ-6 Engine trouble
    From: "jetjockey" <jetjockey@alumni.utexas.net>
    Some years back my aircraft was mistakenly fueled with auto fuel containing ethanol. The tainted fuel absolutely destroyed the carburetor diaphragm. The symptoms you describe are exactly what I experienced. If you find a source for replacement diaphragms, please post this information to the list as I cannot find a source for them any longer. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=385165#385165




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