Today's Message Index:
----------------------
1. 05:35 AM - FW: Yak-52 elevator failure (pilko2)
2. 04:03 PM - Re: Yak-52 elevator failure (Walter Lannon)
3. 04:27 PM - Re: Yak-52 elevator failure (William Halverson)
4. 08:20 PM - Re: Yak-52 elevator failure (Walter Lannon)
5. 08:37 PM - CJ6 Shimmy damper problems (CJ6XXK)
Message 1
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Subject: | Yak-52 elevator failure |
Trawling the website of Yak UK reveals this to be a well known gotcha.
http://www.yakuk.com/2000-004.doc
MPD: 2000-004
Subject: Crack in elevator control system pulley.
Applicability: Yakovlev/ Aerostar or a SA Y B AK 52 aircraft.
Reason: A 19 mm crack has been discovered in the elevator actuation part
number 5251 or 00-80-3 (referred to as "lever" in the Romanian parts
catalogue). The failure of this component could result in loss of the
elevator control.
Compliance: Within 50 hours from the effective date of this MPD, inspect
elevator actuation pulley parts number 525100-80-34 cracking on its
periphery below the attachment for the balance weight bracket, at the point
where the section reduces from a 10 mm to 7 mm. Inspect using dye penetrant
techniques. if the component is cracked, replace it before Further Flight.
Repeat this inspection annually at renewal of the permit to fly.
Sector
Message 2
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Subject: | Re: Yak-52 elevator failure |
Interesting!
How much weight is attached to this part? And for what purpose?
Walt
----- Original Message -----
From: pilko2
To: yak-list@matronics.com
Sent: Saturday, March 26, 2011 5:25 AM
Subject: FW: Yak-List: Yak-52 elevator failure
Trawling the website of Yak UK reveals this to be a well known gotcha.
http://www.yakuk.com/2000-004.doc
MPD: 2000-004
Subject: Crack in elevator control system pulley.
Applicability: Yakovlev/ Aerostar or a SA Y B AK 52 aircraft.
Reason: A 19 mm crack has been discovered in the elevator actuation part number
5251 or 00-80-3 (referred to as "lever" in the Romanian parts catalogue). The
failure of this component could result in loss of the elevator control.
Compliance: Within 50 hours from the effective date of this MPD, inspect elevator
actuation pulley parts number 525100-80-34 cracking on its periphery below
the attachment for the balance weight bracket, at the point where the section
reduces from a 10 mm to 7 mm. Inspect using dye penetrant techniques. if the
component is cracked, replace it before Further Flight. Repeat this inspection
annually at renewal of the permit to fly.
http://www.matronics.com/Navigator?Yak-Listhttp://forums.matronics.comhttp://www.matronics.com/contribution
Message 3
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Subject: | Re: Yak-52 elevator failure |
Well, the part is cracking on the upper side ... would it be due to aggressive
pull back forces on the stick?
+-----Original Message-----
+From: Walter Lannon [mailto:wlannon@persona.ca]
+Sent: Saturday, March 26, 2011 04:00 PM
+To: yak-list@matronics.com
+Subject: Re: Yak-List: Yak-52 elevator failure
+
+Interesting!
+
+How much weight is attached to this part? And for what purpose?
+
+Walt
+ ----- Original Message -----
+ From: pilko2
+ To: yak-list@matronics.com
+ Sent: Saturday, March 26, 2011 5:25 AM
+ Subject: FW: Yak-List: Yak-52 elevator failure
+
+
+
+
+ Trawling the website of Yak UK reveals this to be a well known gotcha.
+
+
+
+ http://www.yakuk.com/2000-004.doc
+
+
+
+
+
+
+
+ MPD: 2000-004
+
+
+ Subject: Crack in elevator control system pulley.
+
+
+
+ Applicability: Yakovlev/ Aerostar or a SA Y B AK 52 aircraft.
+
+
+
+ Reason: A 19 mm crack has been discovered in the elevator actuation part number
5251 or 00-80-3 (referred to as "lever" in the Romanian parts catalogue).
The failure of this component could result in loss of the elevator control.
+
+
+
+ Compliance: Within 50 hours from the effective date of this MPD, inspect elevator
actuation pulley parts number 525100-80-34 cracking on its periphery below
the attachment for the balance weight bracket, at the point where the section
reduces from a 10 mm to 7 mm. Inspect using dye penetrant techniques. if the
component is cracked, replace it before Further Flight. Repeat this inspection
annually at renewal of the permit to fly.
+
+
+
+
+
+
+
+
+
+
+
+ http://www.matronics.com/Navigator?Yak-Listhttp://forums.matronics.comhttp://www.matronics.com/contribution
+
Message 4
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|
Subject: | Re: Yak-52 elevator failure |
Possibly. The crack is originating at the section change where loads would
tend to concentrate but it may also be subject to bending loads from the
balance weight attached to the upper, heavier, section.
Possibly rudder induced transverse loading?
I don't understand the use of a balance weight in this location.
Walt
----- Original Message -----
From: "William Halverson" <william@netpros.net>
Sent: Saturday, March 26, 2011 4:21 PM
Subject: Re: Yak-List: Yak-52 elevator failure
>
>
> Well, the part is cracking on the upper side ... would it be due to
> aggressive pull back forces on the stick?
>
>
> +-----Original Message-----
> +From: Walter Lannon [mailto:wlannon@persona.ca]
> +Sent: Saturday, March 26, 2011 04:00 PM
> +To: yak-list@matronics.com
> +Subject: Re: Yak-List: Yak-52 elevator failure
> +
> +Interesting!
> +
> +How much weight is attached to this part? And for what purpose?
> +
> +Walt
> + ----- Original Message -----
> + From: pilko2
> + To: yak-list@matronics.com
> + Sent: Saturday, March 26, 2011 5:25 AM
> + Subject: FW: Yak-List: Yak-52 elevator failure
> +
> +
> +
> +
> + Trawling the website of Yak UK reveals this to be a well known gotcha.
> +
> +
> +
> + http://www.yakuk.com/2000-004.doc
> +
> +
> +
> +
> +
> +
> +
> + MPD: 2000-004
> +
> +
> + Subject: Crack in elevator control system pulley.
> +
> +
> +
> + Applicability: Yakovlev/ Aerostar or a SA Y B AK 52 aircraft.
> +
> +
> +
> + Reason: A 19 mm crack has been discovered in the elevator actuation
> part number 5251 or 00-80-3 (referred to as "lever" in the Romanian parts
> catalogue). The failure of this component could result in loss of the
> elevator control.
> +
> +
> +
> + Compliance: Within 50 hours from the effective date of this MPD,
> inspect elevator actuation pulley parts number 525100-80-34 cracking on
> its periphery below the attachment for the balance weight bracket, at the
> point where the section reduces from a 10 mm to 7 mm. Inspect using dye
> penetrant techniques. if the component is cracked, replace it before
> Further Flight. Repeat this inspection annually at renewal of the permit
> to fly.
> +
> +
> +
> +
> +
> +
> +
> +
> +
> +
> +
> +
> http://www.matronics.com/Navigator?Yak-Listhttp://forums.matronics.comhttp://www.matronics.com/contribution
> +
>
>
>
Message 5
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Subject: | CJ6 Shimmy damper problems |
I just done some high speed taxi runs in my cj6 today and have a few problems.
First thing is that i raise the the nose of the plane then put it down again and
i have got massive amounts of shimmy.
This was a brand new shimmy damper i bought and fitted as well.
Is there a special way to set them up?
Thanks Daniel
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=335149#335149
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