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. |
|
|
Thread Tools | Display Modes |
#41
|
|||
|
|||
Jay Honeck wrote:
: Hope that helps describe why they went to it. : Thanks, Cory! : Do you know if there's a legal way to put LEDs in my plane? : -- : Jay Honeck : Iowa City, IA : Pathfinder N56993 : www.AlexisParkInn.com : "Your Aviation Destination" I believe there's a company that make little plastic ring doodads to go around the instruments. Not cheap, though. The trouble with LED's is that they don't work the same as light bulbs. They're a current-controlled device, and a bulb is roughly a voltage^2-controlled device. If you have some of each, it'd be tough to get them to dim at the same "rate." As far as getting stuff approved, depends on your friendly neighborhood FSDO, I guess. You just fixed yours... leave well-enough alone! Wait a minute... didn't you taunt the airplane gods a week or two ago about how *everything* on your plane worked? :P~~ -Cory -- ************************************************** *********************** * The prime directive of Linux: * * - learn what you don't know, * * - teach what you do. * * (Just my 20 USm$) * ************************************************** *********************** |
#42
|
|||
|
|||
Wait a minute... didn't you taunt the airplane gods a week or two
ago about how *everything* on your plane worked? :P~~ Yep. This repair was part of the procedure that got everything to work -- I only just received the bill for it, now. At the moment, everything STILL works! :-) (Of course, it's too damned windy around here to fly -- again. Windiest March I've ever seen...) -- Jay Honeck Iowa City, IA Pathfinder N56993 www.AlexisParkInn.com "Your Aviation Destination" |
#43
|
|||
|
|||
OK, I did what you said. I read your App. Note 1. Also googled around for
other things you have written. I guess I still don't "get it." Your App. Note 1 references an AC that was superseded back in 1996, AC 20-62C, which is now AC 20-62D. The current version says in the definition of "Acceptable Parts": "(2) Parts produced by an owner or operator for maintaining or altering their own product and which are shown to conform to FAA-approved data." So how can an owner's home-made dimmer circuit can be installed without any approved data? You have cited the "Chief Counsel" on several occasions. Do you mean, by any chance, the "Assistant Chief Counsel for Regulation letter dated Aug. 5, 1993 " referred to in http://www.awp.faa.gov/new/fsdo/ans_jan2_98.htm? I would like to see that letter, if you know anywhere that it is published. Unless it is publicly available, it would be hard for someone to cite it as an authority. "Jim Weir" wrote in message ... I've been answering this same exact question for thirty-three years exactly the same way, and I'm not going to go into the song and dance here again. You can google the answer if you like, or you can download Applications Note 1 (the one I wrote back in 1972 as amended through last year) from www.rstengineering.com if you want the long answer. Or, I can reproduce it here if you all would like some flame bait. Jim "Dan Thompson" shared these priceless pearls of wisdom: -Wouldn't replacing an approved dimmer assembly with a home-made one be a -"major alteration" that would require a Form 337, and field approval of the -data, for return to service? Jim Weir (A&P/IA, CFI, & other good alphabet soup) VP Eng RST Pres. Cyberchapter EAA Tech. Counselor http://www.rst-engr.com |
#44
|
|||
|
|||
Jay Honeck wrote:
Ray has explained to you, twice in this thread, why transistors are used. If you can't understand the technology, stop commenting on it. Wow, we normally can't find anyone here to defend the high-tech 1974 Chevy Nova technology found in my Piper -- thanks! Using that logic, we'd might as well disconnect our yokes, and roll a brand new plane underneath them. It's not practical to redesign everything on our planes, just because you don't like the way they did it in 1974 (or '64 or '54). Your view is, um, refreshing, somehow. Kinda like the Amish, I suppose, but I guess I could get used to it. My engineering degree trumps your silly little english degree when it comes to commenting on technology. Actually, flying a 30 year old airplane, I have little choice. :-( Exactly, now your gettting it. -- __!__ Jay and Teresa Masino ___(_)___ http://www2.ari.net/jmasino ! ! ! http://www.oceancityairport.com http://www.oc-adolfos.com |
#45
|
|||
|
|||
My engineering degree trumps your silly little english degree when it
comes to commenting on technology. My Dad -- a high school grad -- used to have a word for all the engineers in his department. He called them "employees." ;-) -- Jay Honeck Iowa City, IA Pathfinder N56993 www.AlexisParkInn.com "Your Aviation Destination" |
#46
|
|||
|
|||
"Gene Kearns" wrote in
: broke within 1 hour because the mechanic (1) couldn't solder and (2) had no notion of how to properly suppport soldered wires against vibration. Not to mention prohibition against soldering (unless absolutely unavoidable) that most A&Ps have been taught. Unfortunately, you are right. Lots of A&P's (and IA's) work more off of old wives tales like this than facts. Studies have found that *correctly* formed connections, both crimp and soldered, have virtually identical (and low) failure rates in aviation use. Only the mode changes - crimps fail from corrosion or pull, *sometimes* from breakage at the connector. Soldered connections, improperly done, fail from breakage at the connector and from cold solder joints. The only real advantage to crimp connectors is that it is a little easier to *automate* the job, and hence they may be better in the hands of someone without training. Otherwise, both have their proper place. ----------------------------------------------- James M. Knox TriSoft ph 512-385-0316 1109-A Shady Lane fax 512-366-4331 Austin, Tx 78721 ----------------------------------------------- |
#47
|
|||
|
|||
"James M. Knox" wrote: Unfortunately, you are right. Lots of A&P's (and IA's) work more off of old wives tales like this than facts. No, A&Ps work with the methods and procedures defined in AC.43. The "bible" says no soldering unless absolutely necessary. George Patterson Battle, n; A method of untying with the teeth a political knot that would not yield to the tongue. |
#48
|
|||
|
|||
Ya know, this has all been great fun, but a huge time sink. I'll take the
thread up again next weekend, but I won't waste valuable engineering time with folks who have an honest difference of opinion. Opinion, mine as well as yours, are like assholes...everybody has one and most of them stink. See ya after hours... Jim Jim Weir (A&P/IA, CFI, & other good alphabet soup) VP Eng RST Pres. Cyberchapter EAA Tech. Counselor http://www.rst-engr.com |
#49
|
|||
|
|||
G.R. Patterson III wrote:
: No, A&Ps work with the methods and procedures defined in AC.43. The "bible" says : no soldering unless absolutely necessary. While this is not an unreasonable limitation, it is not possible to attatch wires to a potentiometer without soldering (the initial problem that the A&P mechanic was to fix), so I had (erroneously) assumed that this mechanic was knowledgeable about the proper practices of soldering and wire support in high-vibration environments. Sadly I was mistaken, but the ruins of the installation were recoverable with proper soldering technique and wire dressing. Perhaps we are (I am) expecting too much of one man. This particular mechanic is extremely knowledgeable about structures and most powerplane issues. He's less knowledgeable about electrical problems, and not at all comfortable with electronic items - I helped him diagnose some bad engine monitor probes (not in my plane). If he had told me "I do not think that I can perform this repair" I would have been perfectly happy, and would have gone elsewhere. -- Aaron Coolidge (N9376J) |
#50
|
|||
|
|||
Not to mention prohibition against soldering (unless absolutely
unavoidable) that most A&Ps have been taught. I was never prohibited from soldering and spent hours doing it. Granted this was 20 years ago. One thing about these aircraft dimmer switches is that there is typically very little service loop in the wire bundle so very often you have to lie on your back and solder upside down. I have also seen installations where it could take nearly an hour just to expose the switch for soldering and more to put it back together correctly. It always amazes me how often things were designed without any thought to future maintenance requirements. John Dupre' |
Thread Tools | |
Display Modes | |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Remote Switch for Pointer ELT --- Why Does It Need Voltage? | jls | Home Built | 1 | November 22nd 04 09:13 PM |
Jim Weir - PTT switch article? | Corrie | Home Built | 2 | October 4th 04 04:46 PM |
Panel Lights Dimmer | MII Driver | Home Built | 3 | April 3rd 04 01:56 AM |
74 Archer Nav light switch | Mike Noel | Owning | 8 | January 14th 04 03:56 AM |
Kit Plane Instrument light dimmer | Mickey | Home Built | 1 | December 3rd 03 05:46 PM |