VansAirForceForums  
Home > VansAirForceForums

- POSTING RULES
- Donate yearly (please).
- Advertise in here!

- Today's Posts | Insert Pics


Go Back   VAF Forums > Avionics / Interiors / Fiberglass > Electrical Systems
Register FAQ Members List Calendar Today's Posts

Reply
 
Thread Tools Search this Thread Display Modes
  #11  
Old 08-23-2006, 09:07 PM
cenutting cenutting is offline
 
Join Date: Jul 2006
Location: Fraser, CO
Posts: 7
Default Crimpers for different terminals

You can find the good PIDG insulated terminal crimper that Van suggests at Klein Tools. A website that sells this is "www.rimindustries.com". The crimper for the Molex/ D-subminiature pins can be bought at B & C,
www.bandc.biz/parts.html. Do not use the "oval" shaped cheap crimpers for anything except as a paper weight.
__________________
Craig Nutting
Kitfox S-6 N57CN - flying as of Oct 2005
RV-8 N58CN reserved
empennage finished, closed up the wings in Sep. 2006
A & P,CFI, ATP MD-80/ F-100/ B-757/ B-767/ B-777/ MD-11
Fraser, CO
Reply With Quote
  #12  
Old 08-30-2006, 09:27 PM
rlo1 rlo1 is offline
 
Join Date: Oct 2005
Posts: 115
Default

Steinair has a nice selection of reasonably priced tools. Fast service.
__________________
Ron Olmstead
Reply With Quote
  #13  
Old 08-31-2006, 09:00 AM
JonathanCook's Avatar
JonathanCook JonathanCook is offline
 
Join Date: Jun 2006
Location: Celebration, FL
Posts: 131
Default AeroElectric articles on the web

In addition to Bob Nuckolls' book he also has many reference articles on his web site. I found myself reading almost all his web articles one night. (How the time passes when you are having fun.) The articles are at http://www.aeroelectric.com/ARTICLES.HTML . A few articles relating to crimping and fast on connections are

http://www.aeroelectric.com/articles...rimptools.html

"FastOn vs. Ring Terminals . . . What's the Difference?"

Here is a critical review on methods of wiring including crimping vs. sodering and faston vs. threaded terminals and what Bob Nuckrolls' recommends.

http://www.aeroelectric.com/articles/rules/review.html

Good reading.

Jonathan
__________________
Jonathan

Celebration, FL 34747 (just SW of Orlando)
RV7
Working on Fuselage
dues paid for 2012
Reply With Quote
  #14  
Old 08-31-2006, 10:56 AM
Davepar's Avatar
Davepar Davepar is offline
 
Join Date: Jan 2005
Location: Seattle, WA
Posts: 1,166
Default

Quote:
Originally Posted by rlo1
Steinair has a nice selection of reasonably priced tools. Fast service.
It took 4 business days to ship my order placed last week. Not fast.
__________________
Dave Parsons, Seattle, WA, RV-7A, sold
www.dualrudder.com/rv7 - building blog
RunwayFinder.com - airport info, online charts, live METARs, TFRs, etc.
Reply With Quote
  #15  
Old 09-08-2006, 02:34 AM
Sprig Sprig is offline
 
Join Date: Sep 2006
Posts: 15
Default Fast On

I suspect, that just as the name sugests,,,, that Fast-ON = FASTER-OFF in flight conditions.

I'd NEVER use one. PERIOD.

Quote:
Originally Posted by uk_figs
I have been reading the Aeroelectornics book in preparation for starting some wiring and notice it refers to "fast-on" crimped connectors which look a lot like the automotive spade connectors, is this what most people use for connection to power busses etc? Are these different than the automotive parts for the higher vibration environment of an aircraft?
Of course, I might be wrong. Thankfully it won't be MY plane that has a failuremode experienced above.

Sprig
Reply With Quote
  #16  
Old 09-08-2006, 05:00 AM
William Slaughter's Avatar
William Slaughter William Slaughter is offline
 
Join Date: Jan 2005
Location: Houston, Texas
Posts: 469
Default

As Steve posted above, high quality versions of these connectors are not going to come loose accidentally. They are tight, tight, tight. I buy only the Tyco/AMP brand connectors (both FastOn and ring terminals), which are available from SteinAir, Digikey and other sources. I started with an AMP Pro Crimper II crimper and terminal kit from Digikey, and bought additional terminals from SteinAir. This combination is just a joy to use. Regardless of which type of terminal you choose, ring or FastOn, be sure and do a pull test for each terminal size/wire size combination.
__________________
William Slaughter
Houston, TX
RV-8QB
Reply With Quote
  #17  
Old 09-08-2006, 05:15 AM
Jamie's Avatar
Jamie Jamie is offline
 
Join Date: Jan 2005
Location: Atlanta, GA
Posts: 2,295
Default

Quote:
Originally Posted by Sprig
I suspect, that just as the name sugests,,,, that Fast-ON = FASTER-OFF in flight conditions.

I'd NEVER use one. PERIOD.

Of course, I might be wrong. Thankfully it won't be MY plane that has a failuremode experienced above.

Sprig
Quite the opposite, actually. You're in a very, very, VERY small minority, as the overwhelming number of finished RVs (and probably many other homebuilts) are using fast-ons with no problem.

I believe when the above poster was talking about the cheapo terminals loosening up he was referring to the CRIMP loosening, not the spade connecting mechanism. In fact, he could have been talking about ring terminals loosening up.

Take a fish scale and see how much you will need to pull a fast-on to separate a connection. Better to use logic and known, testable facts than anecdotal evidence. And by the way, there are several certified aircraft out there now using AMP PIDGs, not including many of the new LSAs our there using them.

Ok, having said (typed) all of that, you must build your airplane in whatever way makes you sleep better at night.

Also, I would recommend you complete a signature, as it would provide some insight/weight to your posts on the forum.

Best,
__________________
"What kind of man would live where there is no daring? I don't believe in taking foolish chances but nothing can be accomplished without taking any chance at all." - Charles A. Lindbergh
Jamie | RV-7A First Flight: 7/27/2007 (Sold)

Last edited by Jamie : 09-08-2006 at 10:00 AM.
Reply With Quote
  #18  
Old 09-08-2006, 09:51 AM
Davepar's Avatar
Davepar Davepar is offline
 
Join Date: Jan 2005
Location: Seattle, WA
Posts: 1,166
Default

I noticed a cool thing about the Fast-on connectors as I was using them yesterday. The spades have a hole in the middle of them and if you look really close at the terminals, they have a little catch that pops into that hole when properly installed. Belt and suspenders. No way it's coming loose in flight.
__________________
Dave Parsons, Seattle, WA, RV-7A, sold
www.dualrudder.com/rv7 - building blog
RunwayFinder.com - airport info, online charts, live METARs, TFRs, etc.
Reply With Quote
  #19  
Old 09-08-2006, 10:13 AM
jcoloccia jcoloccia is offline
 
Join Date: Sep 2005
Posts: 1,110
Default

Triple ditto....they aren't coming off and they grip tight enough to make a superb electrical connection. The ONLY thing I don't like about using them is if you're not careful in laying out your wiring on the terminal block, it can be easy to short things out by accident when working on them. I personally like to lay them out so the positive terminals are not too close to the grounds.

Then again I've worked on plenty where everything is right next to each other and never had a problem. I guess that's why I always disconnect the battery first
__________________
John Coloccia
www.ballofshame.com
Former builder, but still lurking 'cause you're a pretty cool bunch...
Reply With Quote
  #20  
Old 09-08-2006, 11:01 AM
Guy Prevost's Avatar
Guy Prevost Guy Prevost is offline
 
Join Date: Jan 2005
Location: albuquerque, nm
Posts: 1,167
Default

Let's do a quick analysis.

1. Let's assume that it takes 15 lbs force to remove a fast-on connector (it takes almost twice that). 15 lbf = 66.7N

2. Let's assume that the connector and the bit of unsupported wire after it have a mass of 100g. (Again very conservative--here on this planet that's almost .25 lbs of unsupported wire and terminal!)

3. Assuming we're not approaching the speed of light, F=m*a. Solving for acceleration (a), we have an acceleration required for removal of the Fast-On connector of 66.7N / 0.1kg=667 m/s^2, or 68.1 g's! Another thing to consider is that the acceleration would have to be in the same direction as the axis of the tab in order to cause a spontaneous disconnection. If the acceleration happens at 45 degrees to the tab axis, it'll take 96 g's to disconnect. ((68g)/sin(45deg)).

We're all free not to use FastOn connectors, but I don't think our planes or bodies will survive a large enough acceleration to cause one to depart its tab.

G
__________________
Guy Prevost
Albuquerque, NM
RV-8a Built, Enjoyed, Sold
Two Kids: Built, Enjoying
RV-10, Bought, Rebuilt, Enjoying
Build / First Flight Video: http://www.youtube.com/watch?v=8f9HXzZT1dE
Build Log: http://websites.expercraft.com/geprevo/

Arguing on the internet is like having a competition to see who can hit a brick wall the hardest. You may win, but you're still an idiot.

Last edited by Guy Prevost : 09-08-2006 at 11:02 AM. Reason: units!
Reply With Quote
Reply



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


All times are GMT -6. The time now is 07:02 PM.


The VAFForums come to you courtesy Delta Romeo, LLC. By viewing and participating in them you agree to build your plane using standardized methods and practices and to fly it safely and in accordance with the laws governing the country you are located in.