LED Strobe lights for experimentals

AlphaPilotFlyer

Line Up and Wait
Joined
Dec 15, 2020
Messages
509
Display Name
AlphaPilotFlyer
Anyone with experience LED strobes for experimentals? Currently have stock Whelen on a c172 that continues to bleed through radios and can’t seem to get it any better…so going LED. TSO/certified stuff too expensive and it’s in experimental category so looking at non-cert options for right wing (have ADBS combo on left) and for tail. Also thinking about building my own as components cheap and the flash chip and programming doable.
 
I have AeroLED combo nav lights and strobes on my RV. I originally had some radio noise, on some freqs, but not all. Using shielded wire and running the grounds back to my main ground (forrest of tabs on the firewall) solved the problem.
 
we put FlyLED on my RV8 and are very happy with them. Don’t notice any interference with coms, and they sure are bright
 
We've got NavStrobe lighting (TSO'd, too!) on our 182. I'm pretty happy with them, especially for the price. One of our whalen strobes went out, and it was a ton cheaper to go this route than to even mess with the whalen. I haven't found a downside to them, yet.

 
I know a couple guys that have used these in their experimentals. And one that has them in a certified aircraft. All have been very happy with birghtness, longevity, color and of course price.

 
I had this issue forever with ANY led landing light. Then I got this thing and it made it 99% better. I would highly recommend.

 
I have an old TKM radio that checks out fine but seems to pick up noise from everything, while intercom and other radio are fine. Trying out one of these Eliminator filters on it soon and will report back.
 
Sorry for the delay! Happy to report back that the Lonestar Eliminator filter removed all the noise from my old MX11 radio. Very happy with the results. Though I should preface this with the fact that I did isolate the radio down to the only device picking up the noise.
 
Why not go with a matching pair?

 
cost was issue, but I would still need the original strobe box for tail strobe and it would likely still have the interference
 
Anyone with experience LED strobes for experimentals? Currently have stock Whelen on a c172 that continues to bleed through radios and can’t seem to get it any better…so going LED. TSO/certified stuff too expensive and it’s in experimental category so looking at non-cert options for right wing (have ADBS combo on left) and for tail. Also thinking about building my own as components cheap and the flash chip and programming doable.
Your bleed through is the coax. Switch to RG400.
 
Your bleed through is the coax. Switch to RG400.
FYI: RG-400 is overkill on small aircraft unless required by a specific installation requirement. RG-58 is more than enough provided it is in a serviceable condition. And if the RF noise was coming from the coax then it usually means the shielding has lost its ground somewhere. Hardly a reason to replace it vs to fix the ground problem.
 
RG-58 is more than enough provided it is in a serviceable condition.
Sure, if you expect to change it every 10-15 years. Take a look at the life expectancy. And this is why you start to get such crappy radio transmissions and receptions well before the radios need to be changed.

RG-400 is military grade and has a minimum of 20 years, but usually will go longer.
 
Sure, if you expect to change it every 10-15 years. Take a look at the life expectancy.
Not my experience. If its installed and maintained properly have seen it last and perform well past 30 years. I would never change out RG-58 just to change it out. As to the radio performance issues, I've found its more a lack of preventive mx or inspection than part failure with same issue on the entire electrical system. Nothing on an aircraft is a "set it and forget it" item.
 
Anyone with experience LED strobes for experimentals? Currently have stock Whelen on a c172 that continues to bleed through radios and can’t seem to get it any better…so going LED. TSO/certified stuff too expensive and it’s in experimental category so looking at non-cert options for right wing (have ADBS combo on left) and for tail. Also thinking about building my own as components cheap and the flash chip and programming doable.
I’ve seen a few experimental LED setups, and I’d definitely focus on proper EMI filtering and grounding before building one from scratch. If the Whelen is bleeding into the radios, the LED driver and wiring layout will matter just as much as the light itself. A non-certified unit may be fine for an experimental, but I’d still test it thoroughly for radio interference before committing to it.
 
for sure..... bleed thru is often a cumulative issue on old planes with everything grounded to air frame and old radios. I don't fly it much at night so usually just shut it off on frequencies effected so not much motivation to continue digging too deep. added a common avionics ground terminal that connects to battery strap which helped. .. these old strobe energy pulses pack a punch and find ways to get to common ground with so much chassis grounds.
 
Quick story. A local mechanic had his certs suspended when a customer airplane was ramped and non approved LEDs were discovered. The owner installed them but the IA had done an annual and didn’t catch it. 6 months of no revenue for a one man shop.

Think about your IA before you install illegal parts.
 
My c172 is experimental so no worry there….but wondering, what did FAA use as a violation basis? Does part 43 d have a reference to inspecting for non conforming equipment? I get if the installation job stands out or non secure in some way, or the equipment is blatantly obviously non conforming. But if such equipment is installed with normal methods and appears as any other led set, what responsibility does IA have to check log books for anything not factory, or look for markings such as PMA, TSO, etc? .. If so, that’s a lot of responsibility and work to inspect for any different than original items then the log book entry or markings. Seems the owner or operator that installed it would be on the hook as they are ultimately responsible for airworthiness….IA if they were deemed negligent in not realizing it.

Do you know if FAA did anything with owner?

I come across several AnPs that don’t work on anyone else’s plane even though they are constantly asked and offered more than fair money , citing responsibility concerns. Reasons as this further prove their point. Thanks for chiming in..food for thought.
 
what responsibility does IA have to check log books for anything not factory, or look for markings such as PMA, TSO, etc? ..
When an IA signs an annual inspection, he accepts responsibility the aircraft conforms to its type design back to the date of its original AWC, which is the main point of the annual. Technically, they revalidate the AWC per ICAO requirements, which is why until the mid-1950s only the CAA performed annuals and actually issued a new AWC every year. The EASA still does follow that path for most aircraft. And unless the owner, or whoever made the illegal installation, made a log entry or personally confesses to that install, there is no regulatory path to violate that person. So it falls to the last person who signed the book who is held responsible. As I've stated in the past, aviation works on a closed system principal where everyone is required to follow all the rules and, in these cases, follow Block 6 of the aircraft AWC. So, in my book, the only proper punishment for these type people, or hangar fairies in general, is a public hanging.
 
Last edited:
Hmmm…public hanging for installing a non cert led kit? Seems bit harsh for a recreational SE piston. The kit obviously worked and likely powered by same circuit breaker as old unit which would likely been rated more for the wiring on a LED counterpart which may be issue. What if someone installed the non-certified version of say a Garmin G5 artificial horizon because its half the cost and what they could afford…. What draconian punishment would be worthy of such a dastardly act? Same unit, same manufacturing process and components, just a different PN and price tag. Maybe if there was a method to legally install either at local AnP level, little things like swapping the circuit breaker or fuse and other basics would be addressed.

Studies prove bigger artificial horizon screens significantly reduce disorientation, especially compared to legacy 3 inch Gyros, and remain the primary factor on a Titanic amount of fatal crashes. Would replacing the stock 3” gyro with an affordable bigger but non cert unit be likewise worthy of public capital punishment?

I am not advocating for a free for all in installing non conforming components, but, such pistons are operated as personal aircraft or in training missions and vast vast majority in day VMC. , not carrying cargo or passengers over the Atlantic at night. The average age of legacy pistons are now 50+ years old and cost to keep them with modern and safer equipment is cost prohibitive.

If an owner wants to install a led kit from the experimental market, FAA should have a process within the field approval mechanisms that requires a minimum basis for equipment approval with local AnP and maybe FSDO based on thinks like reliable exp service history for such non critical components, and installation using certified standards … if the LEDs fail at night, unlikely even for a cheap kit to happen at rare night flight , big deal, there’s a beacon…fix it. No One is flying into ORD at night in their sparrow hawk or tiger.

Same for a exp EFIS….how many spatial orientation crashes may have not happened and lives saved if pilot had a 10” artificial horizon screen to reference, maybe with terrain depicted to reduce CFIT as a free bonus. This is not the 1940s when now draconian cert regulations were written and equipment and tech was new and unreliable. How many times has your smart phone failed in normal conditions with all the use and daily vibrations and charging cycles and occasional drops? Are you telling me the 1950 manufactured vac pump and mechanical gyro is more reliable than a modern smart phone or tablet? If so, may want to upgrade from the Nokia to something in the last couple of decades.

FAA own study said a basic auto pilot would significantly reduce number of fatal crashes, identified that their own cert process was cost prohibited and primary reason why such devices don’t exist, and did nothing to change it, knowing more fatalities will continue that could have been prevented. There are several proven systems from the exp world that could easily and safely be installed on old cert birds , but short of a full expensive STC it won’t happen simply because others that share your view that modifying anything on a 50 year old antique w/o following the 70 year old FAA testament , regardless of its non critical function and fail safe design or aircraft mission. is this really worthy a sentence of death. If so, I’d argue it’s worth the risk installing it considering the known downside stats.

As an AI you should see the obstacles regulations present to upgrading old aircraft, especially in terms of safety or reliability, and , asymmetric cost for benefits, and advocate for practical regulations that allow such….. are you running for FAA fan club president?

curious, what would your recommended sentence be for someone installing a standard Stewart Warner fuel level sensor purchased online for $35 instead of the same SW unit from Cessna with the inked PMA# for over $300, and works great & last long time (same SW # on Cessna part and been around in tractors and cars since 1940s)… asking for a friend.
 
Hmmm…public hanging for installing a non cert led kit? Seems bit harsh for a recreational SE piston.
Not at all. I think the next time you sit across from an FAA ASI who is trying to determine whether to suspend or revoke your certificate and livelihood because someone else decided to skip the rules and not document their work, you'll feel the same way. Thankfully in my experiences these owners weren’t smart enough to cover all their tracks and instead received their own violation. Unfortunately, not all mechanics are as lucky as me. Bottomline, if you don’t like the rules fly amateur-built or ultralight. Simple.

Maybe if there was a method to legally install either at local AnP level, little things like swapping the circuit breaker or fuse and other basics would be addressed.
Except there has been an existing legal method for that exact requirement for decades. Its called a Part 43 alteration which any mechanic can perform. And its the same method I've used to install quite a few un-approved parts on TC'd aircraft to include un-approved LEDs, un-approved avionics, and many other types of parts. This is basic MX 101 level stuff.

Same with your G5 install comment. If you actually knew and understood the regulations and available guidance, you would know that the FAA already addressed this issue 10+ years ago under their Safe Skies program guidance that allowed the installation of a certified G5 or similar electric primary indicator as a minor alteration in certain TC’d aircraft. However, that guidance was driven by the real issue of vacuum system failure rates instead of screen sizes.

Regardless, I think it's obvious your on-going lack of basic regulatory knowledge is behind the failure of your V8 project more than anything else, especially when others have succeeded with similar alterations. No FAA fan club membership required.
 
Not at all. I think the next time you sit across from an FAA ASI who is trying to determine whether to suspend or revoke your certificate and livelihood because someone else decided to skip the rules and not document their work, you'll feel the same way. Thankfully in my experiences these owners weren’t smart enough to cover all their tracks and instead received their own violation. Unfortunately, not all mechanics are as lucky as me. Bottomline, if you don’t like the rules fly amateur-built or ultralight. Simple.


Except there has been an existing legal method for that exact requirement for decades. Its called a Part 43 alteration which any mechanic can perform. And its the same method I've used to install quite a few un-approved parts on TC'd aircraft to include un-approved LEDs, un-approved avionics, and many other types of parts. This is basic MX 101 level stuff.

Same with your G5 install comment. If you actually knew and understood the regulations and available guidance, you would know that the FAA already addressed this issue 10+ years ago under their Safe Skies program guidance that allowed the installation of a certified G5 or similar electric primary indicator as a minor alteration in certain TC’d aircraft. However, that guidance was driven by the real issue of vacuum system failure rates instead of screen sizes.

Regardless, I think it's obvious your on-going lack of basic regulatory knowledge is behind the failure of your V8 project more than anything else, especially when others have succeeded with similar alterations. No FAA fan club membership required.
a lot to unpack, but got 20-30 minutes waiting for a ride, so here goes.....

First, RE V8 project failure. In the commercial sense, you are right, it was a failure, but not for the reasons you state. As noted in our early post during development, our mission was not commercial at all; it was first a challenging cool project we thought, and then to prove a solution to what ills GA could be a practical and cheaper solution than others trying and often failing. We determined the engine was the problem child and such a solution needed to use mostly mass produce components modified as needed to meet same basis as original engine and airframe after alterations. It wasn't until after flying the 2nd test aircraft around that we were literally over run with inquires and owners wanting to convert as well as dealer inquires worldwide that we began designing a plug and play FWF kit. The failure here wasn't understanding FAA regs or the topics you mention as we had the experience and skill set, but not understanding the FAA lack of "interest" in keeping old planes flying regardless if quieter, cleaner, lead free, or 60% cheaper. We had little to no hurdles from FAA ACO, MIDO or local FSDO other than usual dot the i and cross the T early on, in fact most were encouraging. It was later FAA Washington and executive policy level, mostly lawyers, whom had far greater resources than us to fight any battle. Most of which you can read about on www.corsairV8.com if you are home trying to fall asleep.

I'm not going to further bore anyone already bored enough to read another post answering about the C172-V8 FAA issues and answering your prior inquires as already asked and answered to even my dismay, but I say again this: For the project to get an STC, or even exp assured that there would be no issues selling an exp kit (again G1 was already issued and doable other than a DO178 cert level), we would need to engage in civil lawsuits and/or hire active DERs to support a case that wasn't a contention of technical nature, but of policy). We needed to understand that FAA would at least return calls or not take years to respond to required correspondences before proceeding. GA is littered with customer deposits on stuff than never gets thru certification or takes longer and over budgets eventually leaving buyers broke and an airplane unusable....taking deposits to fund a potentially legal battle(s) was in no ones interest. again, the commercial aspect wasn't our fundamental goal so there was little interest in pursuing what would likely be a long expensive battle against a systemic opposistion.

Again, you are correct in stating the thing was a failure, but only in commercial terms. Our stated mission was to prove practical solutions based on GA dwindling size and demographics and cost factors basis for success was possible and proved hypothesis (also a cool project for us). We took a beat up C172 destined for salvage (due to condition and engine being 400 hours over TBO with 2 weak cylinders and making metal), installed a modified modern mass produced FADEC software controlled engine solution, that cost less than half to fly and takes different types of fuel, out performs any other C172 ever built, and cost about same as rebuilding original engine with new rings, pistons, and lots of labor. It was used to train several pilots receiving private, CFI and commercial licenses in it including FAA check rides (of which all examiners liked flying it). It's actually pretty cool. We flew it over the Rockies today sightseeing at 12-13K ft occasionally dropping down for closer looks (hot day about 16-17k density altitude) with no issues AND burning car gas that cost me $3.86/gal.... all while costing less than $28/hr to fly! Try that on a new stock C172.

Its actually quite a feat considering the many that never got as far as us even with massive funding comparingly.

You ask why other engine succeeded where we failed, such a Delta Hawk. Its an apples to orange comparison considering DH has been at it sine mid 1990's I think, i believe shut down at least once, and later raised significant capital.... they still have not got the C172 STC as of yet that I know of (could be wrong as I don't follow industry much now) and talking with its reps at last years OSH the target cost was over $100k, similar to Continental's diesel C172 kit....I wish them the best as anything new to GA is needed. But from a business perspective, the same perspective we had when considering selling our V8 kit, what solution does a diesel engine costing more than most of the existing C172's total value have beside eliminating AVGAS? there is not much of an operating cost savings compared to OE O360 as well; a big ask unless operating where AVGAS isn't practical. AS the AVGAS replacement STCs expand and covers all versions of c172 and similar aircraft that DH will likely target , the value proposition significantly decreases and potential buyers will likely calculate how many engine overhauls of original O360 engine could they get for initial acquisition costs and op cost delta. EPS diesel engines, another long term developer of clean sheet design, wenk BK after close to $60m spent.

Our goal was a solution that cost about same as rebuilding 0360 when it reached TBO, and a significant cost savings in fuel and support that made flying affordable and cleaner and reignite GA. If we had the financial resources to push through, we would have likely also went BK or have a similar product price point that defeated the mission .... As I said, it cost me less than $30/hr to fly today and have a projected TBO of over 4k hours (based on real data, not random... remember its a 500 HP engine flat rated to 220HP or less if selected in software) using synthetic oil, but the op cost i cite above are based on 3K hrs TBO. If we tried to make a clean sheet design, it has proven to be impossible, let alone at these target price points. Not a fair comparison.

So, the C172-V8 project was a huge success from our initial goal , not so much as a commercial one. But we got a cool plane out if it.


You suggest I don't have a firm grasp on field alterations. My point of your contention is AnPs have a certain freedom in installing non-approved articles without a formal outside approval as a 337 or ACO interaction. The example which sparked this was installation of a non approved (whether it a TSO, STC, FA or other) LED strobe system. You stated that you have the ability to deem it a minor repair and install it with just a MLB entry, which I believe as well. I supposed your contention was due to owner not disclosing to IA, but considering fact that you would/could likely just of inspected the install and make it legal with a MLB entry, indicating such an alteration posed little safety hazard and doesn't seem to be a safety factor,,,say as opposed to installing some prop found at a yard sale on a part 135 turbo prop with PAXs.... the public hanging seemed a bit much.
 
continued...
My point was if FAA allowed such non-conforming parts to more easily be accepted if already documented as installed on like TC and manufacturer supplies instructions that normally found by installer AnP on certified docs, there would be less resistance from AnP to install and cost & benefits to owner. In these modern times, not everything needs to go through a FAA process and be certified. Case in point is FAA used to allow prior approved field approvals for solely approving like new alterations..... i think this stopped early 2020s, but it took a lot of uncertainty, time and often cost out of the process. The trick was finding the prior approval without N#. I believe this improved the overall safety.

current prior approved alterations need additional supporting data even though that same FSDO approved others for same.... what's the point? These approvals can take months, be happily approved by one FSDO depending on who you get, or denied by another, and/or referred to ACO which will take even longer and likely be referred to an expensive DER, maybe more than one! The FAA has this prior approved type of data and should make it available and easily searchable (if not already) to AnPs and manufacturers of equipment to include in packaging to speed up process and reduce cost.

I'm not sure I agree with your standing on being able to install many non cert stuff such as avionics via MLG minor entry.... say someone ask to install a non TSO nav/com in a c172. Since TC is IFR, a TSO would be required or some method of noting TC has some form of restriction... but not sure... this type of non cert in to cert aircraft topic comes up routinely in exp circles and gets complicated and likely up for interpretation at fsdo. I remember a AnP in the 80s installing car tape or CD players in planes as such a minor entry and later had issues with FSDO after an IA called them.... I think he was required to do a 337 and come up with some approved method of wiring it. Another guy wanted a battery charger connector installed in the baggage area and shop intended to use a connector from a salvaged other plane under impression it was certified (allbeit for other TC). They sent in a 337 and didnt wait for reply..... FSDO said hole may affect structure and electrical high amp wiring or something, referred it to ACO for engineering input, and told to get a structural DER to see if the hole in skin would not yield strength....the DER made a drawing and hand calculations demonstrating the steel mounting flange of the connector would be as strong or better to dissipate the load. Guy and shop said they will never assume things will be easily approved and regret it. Point is, there is a lot of subjectiveness to minor alterations and most AnPs I know are reluctant to take most on without some guidance, and it would be helpful to owners, as well as shops often that decline for reasons as technical (as lack lack of data/instructions) or later liability.

I am not familiar with the safe skies program you mention, but expect its something like the NORSEE program.....regardless, if the FAA allowed the G5 to be installed as primary instrument replacement without "certified" backup, I expect it was similar to older letter of authorization approvals, which are based on some historical data and include typical ICA and install data, much like a prior field approval for more complex articles. This program makes complete sense for reasons noted above, as opposed to installing a IPAD display bluetoothed to a EFIS box that displays same data.... my point remains, FAA allows the exp G5 because others have installed it under some guidance and data supports it can be installed with just the minor entry, as opposed to the IPAD EFIS which would be denied the minor entry, denied the 337 and certainly referred to ACO to be told you need to get an STC requiring electrical and software DERs. I'm just saying, expand this program to other products so there's no guessing and its installed properly.

I hope this clears up your misconceptions.
 
I hope this clears up your misconceptions.
It doesnt. But it does further support your lack of understanding on how the FAA system works and what it prioritizes especially with your trips to DC. And your attempt to blame the FAA as corrupt and out to destroy recreational GA to cover up that lack of understanding is disengenuous to say the least. Especially when that same "corrupt" FAA allows other rec GA projects to continue without issue and in some cases actually gives support to them.

You suggest I don't have a firm grasp on field alterations.
No I stated you didnt have a grasp on alterations. As shown in the example in Post 23, there are numbers of mechanics who have had certificate actions against them simply because an owner did not document their work or take responsibility for it when issue came to light. It goes well beyond whether the actual work is a safety concern or safety factor, or can be simply corrected by a logbook entry. Thats the point you dont understand.

As to the subjectiveness of the mx side, it will always be there given the definition of airworthy is both objective and subjective. But to blame the FAA for this when it falls to the individual mechanic who makes that subjective determination, once again shows your lack of understanding how the system works. And if you want examples, just read all the subjective pre-buy vs 1st annual stories on PoA.

And so on...
 
But to blame the FAA for this when it falls to the individual mechanic who makes that subjective determination, once again shows your lack of understanding how the system works.
No lack here, just misunderstanding on your part of what I stated, which was that AnPs are rightly reluctant to make the determination of minor alterations due to individual interpretations on the wide discretion they have. More specifically and to point, one AnP may refuse to make the alteration and other may not, or other may require a 337 …and others may call the FSDO for guidance or consult with other AnPs which I think we can agree just adds more randomness. To this point, I merely suggested FAA should maintain a searchable data base of approved 337s which would remove any doubt and fast track similar future FAs, and non cert parts manufacturers could include relative tech data for minor alterations , much like their certified counter parts, that could be used as sole supportive data in alteration being a minor one….. as is now, there may be dozens if not more of different FAs for the same exact alteration and many likely denied or referred to ACO simply due to different FSDO or individuals receiving it. What difference if prior approvals substantially make it legal, or starting from scratch each time…. Some may say it protects PMA or TSO owners from competition, or mucks up the regulations requiring mass produced stuff from needing TSO or other certifications. Either way, owners pay the price of such inefficiencies.

. likewise for same AnP considering if propose alteration meets the minor criteria confidently. When I worked as DER or development side, relevant data was everything in decision process and prior like approvals that service history later demonstrated the modifications/components/techniques/etc proved safe and reliable allowed validated data to use on other similar projects, which could significantly reduce cost and time…. The problem was finding such former projects as no direct data base existed so many efforts were repeated. I merely suggest that manufactured non cert stuff like led lights could have basic tech info in packaging to streamline the decision process and remove some of the randomness.

You seem to be of thought that AnPs should make each alteration decisions solely on their own based on their personal interpretations….. based on their sense of “subjective and objective “determination…. I would argue contrary to point of the controlled closed safety system you directly advocate is contradictive to this insomuch as the mission is to remove, if not eliminate, such subjectiveness and objective ness of individuals within your system This is the reason aviation, and all critical mission industries for that matter, have systems to strictly limit the “objectiveness “ you state should be the fundamental basis in this topic mater. This is the reasons there exist SOPs, detailed manuals for everything from designing, testing, certifying, maintaining, flying a plane… not to mention loads of other approved docs that simply try to give official interpretations of the same info of things like AC’s or white papers. When I approved manuals and guidance, my job was to remove as much possibility of the randomness you advocate as the fundamental basis. If your basis was the best time proven solution we would need little such guidance. Moreover, such an approach has proven dangerous due to its resultant Radom ness and converts the controlled system you claim paramount to one of open to interpretation and thus more uncontrolled.

I’m curious how you believe such personal interpretations you argue as fundamental basis conforms to your closed system effectiveness? Contrast with your adamant use of the same exact drive belt purchased anywhere other than from Cessna at amplified cost puts the entire system in peril? One would think having thousands of AMTs solely determining how to install and wire up a new device without normal guidance is less of safety issue… a Swiss air md11 that crashed into the ocean off Halifax due to a new entertainment system wire fire shows how dangerous simple mods can be, and this was a certified alteration. More over, why my mere suggestion of having access to relevant prior and relative data, which traditionally improves matters of interpretation and decision process consistency, is worthy of your criticism ? We all have different internal biases and backgrounds and levels of critical thought, making any decision different. Thus, the reason for the tools I mention above for guidance.

But it does further support your lack of understanding on how the FAA system works and what it prioritizes especially with your trips to DC
I do know how the FAA cert system works for the most part and as a former DER I actually represented the agency in engineering determinations of compliance of large aircraft part 25 jets. However, if your remark is that I don’t understand the how FAA works in the GA segment, I agree with you….. I thought it would be essentially the same with the bigger dollar and bigger companies I worked with in the jetliner world. There, things got done and calls returned, officials promptly responded and budget for delegations of connected DERs was the norm. Not so much in GA except seemingly for the well connected or well funded to afford their own private FAA reps on their own payroll. I should have realized this early on considering GA’s lack of evolution and few key players. …but again, it wasn’t on our radar initially as our v8 wasn’t going to be a commercial endeavor, and later I thought we solved the issues FAA had been advocating for, so figured we would have at least some support rather than the opposite.

Never traveled to DC, there was no point. I do not think you have a real understanding of the process and experience in trying to work with a public agency with a mission to advance aeronautics and have the very public servants you pay and who’s job it is to deal with you simply ignore you so you eventually give up (as many have, us included) or screw you over by taking years to respond to required paperwork. The FAA allows individuals to work with them directly on certifications rather than only delegation…. This is how the system is supposed to work.

After years of this from multiple levels and divisions and FAA leaders, there is no question it was systemic and intentional, and only could be resolved with us hiring insiders as “operational consultants” or hire attorneys to simply get these public servants to do their job that I pay them to do, and no FAA leader cared or saw concern…if not corruption, what would you call it? And find a new line in stating we don’t understand the process…. Even if we had no clue anyone should get a response. We are not the only ones with this experience and reason ga is stuck in the 50s and so expensive and why more and more new tech is coming from outside the US. So until you build something from chalkboard to flying prototype without huge amounts of funding, mission prove it , and breeze through the straight forward benevolent FAA cert process you claim exist, working with the motivated FAA directors eager to help find solutions they have proclaimed for decades, save your some how self enlightenments critiques until you do, and criticism to those that actually have.
 
I’m curious how you believe such personal interpretations you argue as fundamental basis conforms to your closed system effectiveness?
No idea where you came up with that definition of the “closed system” reference I’ve used, but it wasn’t me. The closed system I refer to is that every part that enters the system or every maintenance task performed in the system, there is someone who takes responsibility for that task or part.

As to eliminating any subjectiveness in maintenance you would need to start at the top and change the regulatory definition of airworthy for the simple fact the second half of that definition: in a condition for safe operation, is about as subjective as it gets.

Contrast with your adamant use of the same exact drive belt purchased anywhere other than from Cessna at amplified cost puts the entire system in peril?
Again, no. I believe I stated the reason behind Piper charging $300 for a Gates belt you can buy at NAPA for $15 was Piper’s Production Certificate requires them to check the belt conforms to the appropriate aircraft type design, ie., closed system. And that added cost is reflected in the Piper price. But if I were to buy that same belt at NAPA, I, as the installer, would conform the belt to the type design, ie., closed system, before I legally installed it on the aircraft as a minor alteration. And the reason for the alteration is it does not carry the Piper part number, ie., the type design. Got it now?

More specifically and to point, one AnP may refuse to make the alteration and other may not, or other may require a 337 …and others may call the FSDO for guidance or consult with other AnPs which I think we can agree just adds more randomness.
Not really. You’re missing the one key part: a mechanics personal limitation in accepting risk and liability. You can have all the databases you want of previous mx work, 337s, or whatever, but it still won’t change the fact that when a mechanic signs the book he owns that mx task forever. Which is similar to your declaration you would only market your V8 STC to foreign customers due to liability issues in the US. Some people simply accept risk better than others and that drives the “randomness” more than anything else which no database can prevent.

Same goes for vendors not including your suggested “relative technical data” for minor alterations. They don’t want the liability either, which the mechanic assumes at installation. Pasted below is the only regulatory guidance to a mechanic for any and all maintenance they will perform on an aircraft. Not very objective, is it? And then there are aircraft with no OEM maintenance manuals or ICAs as mentioned in (a) below. So your only option at that point is referencing something “acceptable to the Administrator” which is equally hyper-subjective but its regulatory.

So, in reality, you’ll find that subjectiveness is a wide-spread “feature” within aircraft maintenance. And the only way to curb all that subjectiveness would be to add 1000s of more rules to Part 43 to force all mechanics to perform mx in a specific objective manner. And you thought rec GA was bad now?

1787277782514.png

However, if your remark is that I don’t understand the how FAA works in the GA segment, I agree with you….. I thought it would be essentially the same with the bigger dollar and bigger companies I worked with in the jetliner world.
This has been my exact point. I never stated you didn’t have any experience, you just lacked understanding how things worked at that level. It’s the same reason I limit or decline any work at the Part 135 10 pax or 121 levels as it takes a different skill set and knowledge base to offer any effective advice or results.

After years of this from multiple levels and divisions and FAA leaders, there is no question it was systemic and intentional, and only could be resolved with us hiring insiders as “operational consultants” or hire attorneys to simply get these public servants to do their job that I pay them to do, and no FAA leader cared or saw concern…if not corruption, what would you call it?
I’d call it an Agency shift toward commercial operations oversight and the subsequent loss of funding to the private ops sector from that shift. Up until the mid-1980s the FAA had dozens of General Aviation District Offices to handle all requirements for GA aircraft from operational issues, to maintenance, to even certification requirements. For example, there were 5 GADOs in my state at that time, plus there were separate offices that handled air carrier requirements.

Then by 1990 or so all the GADOs were closed, along with the ACDOs (Air Carrier) and were replaced by a single FSDO, or multiple FSDOs depending on the state size. So in my state we went from 8 FAA district offices to a single FSDO to handle all FAA requirements. And that change had the biggest effect at the GA level and more importantly the private, recreational level.

Why? At the same mid-80s timeframe, the GA fleet imploded with Cessna stopping production, support shops closed by the dozens and so on. Plus at the same time the effects from Deregulation were starting to come into their own, and there were far more airline pax who beetched about their air service than Part 91 owners complained about their loss of a GADO. End result, congress prioritized funding the airline side and still does today. So end result on the Part 91 recreational side was you now had to perform all the certification/approval leg work yourself and hire DER/DARs for what the previous GADO could do all in-house for free. But again that wasn’t the FAAs call, that was strictly congress and where they sent the money.

And that is how the current STC process works. So either go with that benevolent flow or don’t. And with the ACOs now gone due to reorganization and funding changes, I’m sure that flow will change once again. Regardless, in the big picture, the FAA STC process is still the easiest and most flexible in the world, which even attracts dozens of applicants from overseas every year to get their STCs here. But, for the record, I have been there, got the T-shirt, made the movie, and the sequel. So, if you can’t handle the critiques and criticism, then simply don’t post. However, it still doesn’t change the fact people are navigating and completing that same STC process without issue on a regular basis.
 
Quick story. A local mechanic had his certs suspended when a customer airplane was ramped and non approved LEDs were discovered. The owner installed them but the IA had done an annual and didn’t catch it. 6 months of no revenue for a one man shop.

Think about your IA before you install illegal parts.
Is that non-PMA'd lights? Lights that needed an STC? Or even a field approval (when they used to do such things)?

Were they strobe or beacon lights? Position?

Curious, as LED/light replacement stories are always interesting and many times hilarious.
 
And your attempt to blame the FAA as corrupt and out to destroy recreational GA to cover up that lack of understanding is disengenuous to say the least.
The FAA is corrupt and is out to kill GA. Here's a small snippet of a very long list:
They insist on a drop in 100LL replacement vs allowing the 80%+ of planes that could use a replacement today. Several of the unleaded fuels are ready to go... but the FAA insists on wearing blinders.
The FAA computes AD costs on an $80 an hour shop rate.
The FAA computes 121 AD hourly rate at $60/hr
The FAA has mandated ADS-B and allows its use for taxes/fees.
AnPs cannot do an annual, but a rando jabrony can sign a condition inspection after a two week class.
The FAA has not increased DPE/DME numbers to account for growth.
The FAA has not regulated DPE fees or put regulatory pilots rights for DPE misbehavior.
The FAA prohibits moving certificated airframes into E/AB (like the 172-v8 you need an STC which they can simply run you out of money getting)
Registration fee is $5. That doesn't cover the cost of the process. They pretty much stopped issuing new registrations and just gave a blanket letter. (IMHO: raise the fee to $100 and use that cash to benefit GA) Aka poorly managing the process because the FAA doesn't care.



Not at all. I think the next time you sit across from an FAA ASI who is trying to determine whether to suspend or revoke your certificate and livelihood because someone else decided to skip the rules and not document their work, you'll feel the same way.

You have to have screwed up real good to be in this situation. I don't need the details, but some sort of context is needed... and the LED example posted was nowhere near a complete enough example. I do know of a few that have had suspensions (like 3) but they were honestly so far in the 'yeah, that's bad' (two had their pilots cert suspended for not reporting DUI and one MX refused a drug test) land that it was a surprise that it was only 90 days.

As for OP: you never stated what kind of light. Landing? Strobe? navigation? beacon?
 
The FAA is corrupt and is out to kill GA. Here's a small snippet of a very long list:
The only thing corrupt here is your continued attempt to come across as a knowledgeable “AnP” mechanic. If you actually had that knowledge, you would know where to find the reasons behind all those snippets on your list to include the AD labor rates.

You have to have screwed up real good to be in this situation.
In addition, if you had that knowledge, you would also know any violation, no matter how small, is governed by the guidance in CFR Part 13 and Order 2150.3 Compliance and Enforcement Program. And that 90% of FAA violations are dealt with at the compliance or administrative levels vs the enforcement level as no one wants an enforcement action against a certificate unless there was intent and a personal disregard of the regulations.

Maybe you should read up on this area as a number of your posts on your perception of maintenance may get you in front of an ASI sooner than later? ;)
 
I found creating a loop through a ferrite core greatly eliminates EMI. It fixed the static issue I had with my LED landing lights.
 
I tried ferrite but not a significant help with my old coms on orig strobe system....where did you place it?
As close to the light as I could get it. It didn’t work with a straight pass through. I had to loop it with the overlapping portion of the loop going through the core.
 
thanks....my problem child is the old Waylon pulse strobe lights. I'll try one of each light.
 
The only thing corrupt here is your continued attempt to come across as a knowledgeable “AnP” mechanic. If you actually had that knowledge, you would know where to find the reasons behind all those snippets on your list to include the AD labor rates.


In addition, if you had that knowledge, you would also know any violation, no matter how small, is governed by the guidance in CFR Part 13 and Order 2150.3 Compliance and Enforcement Program. And that 90% of FAA violations are dealt with at the compliance or administrative levels vs the enforcement level as no one wants an enforcement action against a certificate unless there was intent and a personal disregard of the regulations.

Maybe you should read up on this area as a number of your posts on your perception of maintenance may get you in front of an ASI sooner than later? ;)
Boo hoo you got proven wrong so you pull out the tired ol attack from (supposed) authority.

I'll notice that you don't have a single answer for my very short list of FAA blunders. And no, citing the regs isn't the answer, the regs are the problem. But you think you are to smart HAHAHAHAHAHAHAHAHAHAHAHAHHAAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHHAHAHAAHAHAHAHHAAHHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHA
HAHAHAHAHAHAHAHAHAHAHAHAHHAAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHHAHAHAAHAHAHAHHAAHHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHA
HAHAHAHAHAHAHAHAHAHAHAHAHHAAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHHAHAHAAHAHAHAHHAAHHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHA
HAHAHAHAHAHAHAHAHAHAHAHAHHAAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHHAHAHAAHAHAHAHHAAHHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHA
HAHAHAHAHAHAHAHAHAHAHAHAHHAAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHHAHAHAAHAHAHAHHAAHHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHA
HAHAHAHAHAHAHAHAHAHAHAHAHHAAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHHAHAHAAHAHAHAHHAAHHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHA
HAHAHAHAHAHAHAHAHAHAHAHAHHAAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHHAHAHAAHAHAHAHHAAHHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHA
HAHAHAHAHAHAHAHAHAHAHAHAHHAAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHHAHAHAAHAHAHAHHAAHHAHAHAHAHAHAHAHAHAHAHAHAHAHAHAHA that you (think you) have sort of retort or answer.

man just typing that makes we want to laugh so hard I have to tinkle. brb

Ok, potty break over.... where was I? Oh yeah, I'm waiting for your response and no, your self described 'in-tell-ect' ain't gonna cut it.

So lets see how you try and go off on a tangent and not address the very specific problems with the FAA I mentioned.

How well is the FAA managing the DPE/DME shortage?
How many decades has the FAA wasted and still not certified unleaded gas (yet MOGAS is fine) because they have the notion that a 100% drop in is required.
How do you handle DPEs/DME's that abuse applicants, charge the outrageous fees and leave the applicant at the mercy of an examiners whims?
And show me an owner that's gotten an AD letter and thinks the cost of compliance is correct. The shop that's charging $80 an hour is gonna get REAL popular REAL fast.

There's a few topics... go ahead and impress me with your in-tell-ect slugger. Heck just answering ONE might give you SOME sort of credibility.
 
Back
Top