A aviation & planes forum. AviationBanter

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Soaring
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

Electrical continuity of control linkages and electrical instruments



 
 
Thread Tools Display Modes
  #1  
Old June 26th 15, 02:54 AM posted to rec.aviation.soaring
son_of_flubber
external usenet poster
 
Posts: 1,550
Default Electrical continuity of control linkages and electrical instruments

I had the seat pan out of my glider and I noticed that there are several braided wires connecting the metal stick to other metal parts and the (-) side of the power distribution block, battery, and (via power distribution wires) to the (-) of the electrical instruments (with small fuses on each instrument).

I understand that this has something to do with possible lightening strikes and also minimizing RF interference for radio, transponder etc..

Can someone provide a better explanation (or a link)?

If lightening hits a control rod, what happens to the pilot holding the hot stick?

  #2  
Old June 26th 15, 02:56 AM posted to rec.aviation.soaring
son_of_flubber
external usenet poster
 
Posts: 1,550
Default Electrical continuity of control linkages and electrical instruments

On Thursday, June 25, 2015 at 9:54:02 PM UTC-4, son_of_flubber wrote:
I had the seat pan out of my glider and I noticed that there are several braided wires connecting the metal stick to other metal parts and the (-) side of the power distribution block, battery, and (via power distribution wires) to the (-) of the electrical instruments (with small fuses on each instrument).

I understand that this has something to do with possible lightening strikes and also minimizing RF interference for radio, transponder etc..

Can someone provide a better explanation (or a link)?

If lightening hits a control rod, what happens to the pilot holding the hot stick?


I have a fiberglass glider with some steel structural members (no carbon fiber) ... if that matters.
  #3  
Old June 26th 15, 05:04 AM posted to rec.aviation.soaring
2G
external usenet poster
 
Posts: 1,439
Default Electrical continuity of control linkages and electrical instruments

On Thursday, June 25, 2015 at 7:54:02 PM UTC-6, son_of_flubber wrote:
I had the seat pan out of my glider and I noticed that there are several braided wires connecting the metal stick to other metal parts and the (-) side of the power distribution block, battery, and (via power distribution wires) to the (-) of the electrical instruments (with small fuses on each instrument).

I understand that this has something to do with possible lightening strikes and also minimizing RF interference for radio, transponder etc..

Can someone provide a better explanation (or a link)?

If lightening hits a control rod, what happens to the pilot holding the hot stick?


Electric current WILL find a current path thru the glider in the event of a lightning strike. YOU don't want to be a part of that current path. These braids ensure that the current will go thru the control rods, which are capable of carrying that current, and not thru the pilot's body, or other parts of the glider that might disintegrate.

Tom
  #4  
Old June 26th 15, 07:36 AM posted to rec.aviation.soaring
Cookie
external usenet poster
 
Posts: 152
Default Electrical continuity of control linkages and electrical instruments

On Thursday, June 25, 2015 at 9:54:02 PM UTC-4, son_of_flubber wrote:
I had the seat pan out of my glider and I noticed that there are several braided wires connecting the metal stick to other metal parts and the (-) side of the power distribution block, battery, and (via power distribution wires) to the (-) of the electrical instruments (with small fuses on each instrument).

I understand that this has something to do with possible lightening strikes and also minimizing RF interference for radio, transponder etc..

Can someone provide a better explanation (or a link)?

If lightening hits a control rod, what happens to the pilot holding the hot stick?


Corrosion control??? All dissimilar metals at same potential....


Cookie
  #5  
Old June 26th 15, 12:22 PM posted to rec.aviation.soaring
Cookie
external usenet poster
 
Posts: 152
Default Electrical continuity of control linkages and electrical instruments

On Friday, June 26, 2015 at 2:36:24 AM UTC-4, Cookie wrote:
On Thursday, June 25, 2015 at 9:54:02 PM UTC-4, son_of_flubber wrote:
I had the seat pan out of my glider and I noticed that there are several braided wires connecting the metal stick to other metal parts and the (-) side of the power distribution block, battery, and (via power distribution wires) to the (-) of the electrical instruments (with small fuses on each instrument).

I understand that this has something to do with possible lightening strikes and also minimizing RF interference for radio, transponder etc..

Can someone provide a better explanation (or a link)?

If lightening hits a control rod, what happens to the pilot holding the hot stick?


Corrosion control??? All dissimilar metals at same potential....


Cookie


Probably not so much for corrosion...but rather for static electric charge....all parts bonded to prevent sparks / arcs...to protect people and equipment.
  #6  
Old June 26th 15, 12:47 PM posted to rec.aviation.soaring
Pat
external usenet poster
 
Posts: 4
Default Electrical continuity of control linkages and electrical instruments

This may be the link you need:
http://tinyurl.com/p7af5ww (accident report, pdf)
  #7  
Old June 26th 15, 03:15 PM posted to rec.aviation.soaring
[email protected]
external usenet poster
 
Posts: 112
Default Electrical continuity of control linkages and electrical instruments


I understand that this has something to do with possible lightening strikes and also minimizing RF interference for radio, transponder etc..

Can someone provide a better explanation (or a link)?


There's an explanation he https://www.faa.gov/regulations_poli...rame_handbook/

Vol 2, Chapter 11
  #8  
Old June 26th 15, 04:09 PM posted to rec.aviation.soaring
Bob Kuykendall
external usenet poster
 
Posts: 1,345
Default Electrical continuity of control linkages and electrical instruments

On Thursday, June 25, 2015 at 6:54:02 PM UTC-7, son_of_flubber wrote:

...possible lightening strikes...


Nitpick:

* Lightning strikes with a flash of light

* Lightening strikes with a sawzall



Bob K.
 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump

Similar Threads
Thread Thread Starter Forum Replies Last Post
Electrical questions AK Soaring 3 February 27th 08 02:39 AM
Gap Tape? Electrical OK? ContestID67 Soaring 10 May 2nd 06 07:37 AM
Electrical issue Jimmy B. Owning 8 March 2nd 05 12:11 AM
Electrical rewire Sam Fly Restoration 0 April 1st 04 03:11 AM
B-36 electrical system Q. John Mackesy Military Aviation 2 July 18th 03 05:41 AM


All times are GMT +1. The time now is 08:49 AM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2024, Jelsoft Enterprises Ltd.
Copyright ©2004-2024 AviationBanter.
The comments are property of their posters.