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The article was written to address the producing of parts by owner and operators. The article is not intended to imply that maintenance technicians or repair stations may not be able to manufacture parts in the course of accomplishing repairs or alterations. That in itself is another topic for another day.
The sun was setting on another hot August afternoon when the South Carolina Flight Standards District Office received the call from a local airport manager notifying the office that a Piper Cherokee had suffered a nose gear collapse during taxi operations. It was reported that the Cherokee suffered minor damage; the damage included a prop strike and lower cowling abrasion.
Early the next morning, the inspector assigned to investigate the incident picked up the preliminary information with one hand and his first cup of coffee with the other. As the aroma and warm flavor of his coffee cleared the night’s cobwebs from his mind, he eyeballed the incident information. As he read, he thought: "Let’s see, Cherokee 140, taxi, nose gear collapse, prop, cowling, etc., etc.—wait a minute, Cherokee 140? How can a 140’s nose gear collapse during taxi operations and cause this kind of damage? An Arrow, maybe, but a 140?"
Years of experience told the inspector there was a lot more to this story than had been reported. So on that hot, humid, August morning, he headed for the airport. His investigation uncovered a classic case of an aircraft owner making parts and doing everything wrong. The issues surrounding manufacturing approved parts, who can produce these parts, what makes a part approved or unapproved, all came up in the investigation.
Time and again aircraft owners and maintenance technicians are pressured into making parts. Why do we do it? Why do we take on that liability? Let’s look at the facts.
The average general aviation, piston single-engine aircraft is more than 32 years old; the average piston twin is more than 27 years old; and the average turbo prop is 19 years old. The GA aircraft fleet was never designed to last this long, and, when it comes to getting replacement parts to maintain these aircraft, here are a few of the problems we all face.
The aircraft has been out of production for years.
The aircraft is an orphan. No one even knows who owns the Type Certificate.
There is no technical support. If you ask for technical assistance, you are often told that no one really knows much about the aircraft anymore. The people who were around when the aircraft was built are all retired or dead.
Economy of scale forces aircraft manufacturers to build parts in quantities that make economic sense for the manufacturer. What this means is that parts are available, in about six or eight months!
The price of parts is a subject that we aren’t even going to talk about. Sitting in the middle, between a tired broken airplane, its owner, and all these parts problems, is the maintenance technician. Technicians, by their nature, are "can do" people. They live by the motto the difficult we do immediately; the impossible just takes a bit longer. But when it comes to making parts, this "can do" philosophy can really get them in trouble.
Let’s examine the rules governing the general privileges and limitations of a maintenance technician (or certificated mechanic as stated in FAR §65.81), and the rule governing a repair station’s privileges of certificates (FAR §145.51). Under both rules a technician or repair station may perform maintenance, preventative maintenance, and alterations on an aircraft, or appliances for which he is rated. Nowhere in either rule does it say that the maintenance technician or repair station can produce new parts! However, the maintenance regulations allow the manufacture of parts for repair (see number 11 in next question.
A maintenance tech or repair station can make patch plates, reinforcement splices, and incorporate them into the repair of a part. But again, a, a maintenance technician cannot make a brand new part for sale.
Here are some answers to those earlier questions.
Question: who can make a brand new part?
Answer: FAA Advisory Circular 21-29, Detecting And Reporting Suspected Unapproved Parts, states that there are eleven ways that a new part can be made. They are:
1. Parts Manufacturer Approval (PMA)
2. Technical Standard Order (TSO)
3. Type Certificate (TC) or Supplemental Type Certificate (STC)
4. TC with an Approved Production Inspection System (APIS)
5. Production Certificate (PC)
6. Bilateral Agreement
7. Any method acceptable to the Administrator.
8. Standard Parts (nuts and bolts)
9. Owner Produced Parts
10. Parts produced per STC instructions as part of an STC modification.
11. Fabricated by a qualified person in the course of a repair for the purpose of returning a TC product to service (which is not for sale as a separate part) under part 43.
All this sounds like bureaucratic alphabet soup, but, of all the ways listed, "Owner Produced Parts" is the one most misunderstood. FAR §21.303(b)2 makes a provision for an aircraft owner or operator to produce parts for maintaining or altering his or her own product. Under this provision, the Owner Produced Part can only be installed in an aircraft owned or operated by that person and the Owner Produced Part cannot be produced for sale to others.
Question: How is it that an aircraft owner can produce a part, but a skilled maintenance technician can’t?
Answer: The responsibility follows the money. Most rules are written so the responsibility for an action is placed with the person who has the economic authority to make it happen. (The Golden Rule)
Question: How does this owner-produced rule work? Does the owner have to make the part himself?
Answer: The answers can be found in a FAA Memorandum dated August 5, 1993, in which the assistant Chief Counsel for Regulation makes the following interpretation:
A part does not have to be solely produced by the owner to be considered an Owner Produced Part.
The aircraft owner must participate in the manufacture of the part in at least one of five
ways for it to be considered an Owner Produced Part. 1. The owner provides the manufacturer of the part with the design or performance data.
2. The owner provides the manufacturer of the part with the materials.
3. The owner provides the manufacturer with fabrication processes or assembly methods.
4. The owner provides the manufacturer of the part with quality control procedures.
5. The owner personally supervises the manufacture of the new part.
As anyone can see, the discriminators for determining owner participation in a new part’s manufacture are very specific in the interpretation. Attachment (A) to the 1993 Memorandum clearly stipulates that the FAA would not construe the ordering of a part as participating in controlling the design, manufacture, or quality of a part. The key point is that the aircraft owner must participate in the part’s manufacture.
Question: If the part is owner produced, is it also a FAA approved part? Can I install it in the owner’s aircraft?
Answer: If the Owner Produced Part has all the characteristics of an approved part, is only installed on the owner’s aircraft, and is not for sale, it would be considered a FAA approved part.
There are eleven ways (as listed earlier) to produce an FAA approved part. It doesn’t matter if a part is produced under the authority of a PMA, TC, or owner produced, it must have all the characteristics of an approved part. The four characteristics of an approved part are:
1. The part must be properly designed. A properly designed part means that the part’s design is FAA approved. Depending on the complexity of the part, a FAA approved design will have the following elements:
Drawings, specifications to define the part’s configuration and design features.
Information on dimensions, materials, and processes necessary to define the structural strength of the product.
Airworthiness limitations and instructions for continued airworthiness.
Any other data necessary to allow by comparison, the determination of airworthiness of later products of the same type. 2. The part must be produced to conform to the design. A properly produced part means the part conforms to the FAA approved design. Usually a properly produced part will have the following characteristics:
The part complies with all applicable structural requirements of its design.
The materials and products conform to the specifications in the design.
The part conforms to the drawings in the design.
The manufacturing processes, construction, and assembly of the part conform to those specified in the design. 3. The part’s production should be properly documented. A properly documented part provides evidence that the part was produced under an FAA approval and memorializes the production of the part.
4. The part must be properly maintained. A properly maintained part means that the part is maintained in accordance with the rules prescribed under FAR Part 43.
It is relatively easy for a part to meet the requirements of the August 5, 1993, Memorandum and qualify as an Owner Produced Part. The four characteristics of an approved part are like the four legs of a table with all four legs "equally sharing" the burden of an approved part. If one leg is missing, the table will fall over. In the same way, if any of the four characteristics of an approved part is missing, then the part may not be FAA approved.
A good example is the case of the Cherokee 140 with the collapsed nose gear, mentioned and shown in the beginning of this article. The investigation determined the following:
The original factory nose strut lower tube was pitted.
The aircraft owner had a strut tube locally manufactured.
A technician who knew of the part’s origin installed the strut tube.
The strut tube failed during the first operation, resulting in $7,000+ in damages.
Question: Was the strut-tube an Owner Produced Part?
Answer: Yes, legally it was an Owner Produced Part. The aircraft owner did participate in the manufacture of the part. The owner supplied the manufacturer a design for the part. He did this by giving the manufacturer the old lower strut tube and told him to duplicate it. (Reverse engineer)
Question: Was this a FAA approved part?
Answer: No, the part was not approved because the owner did not provide the manufacturer with an approved design or its equivalent. The part was not approved because it did not conform to the material specifications prescribed in the approved design. The part failed during its first operation and didn’t last long enough for maintenance to be a factor.
Question: Did the part producer (aircraft owner) or the maintenance technician who installed the strut-tube violate the FAR? Who should be held accountable?
Answer: The answer is both! The maintenance technician violated the rule the moment that he signed the maintenance records and approved the aircraft to return to service with the knowledge the part he installed was unapproved, that is he apparently understood that the part was produced by the owner. The question he should have asked the owner was "how the part was produced so as to meet the performance rules of part 43.13 of the Federal Aviation Regulations." The aircraft owner violated the rule when he knowingly operated the aircraft with an unapproved and undocumented part installed.
Question: This incident with the Cherokee 140 was wasteful, tragic, and dangerous. If the aircraft owner wanted to make an Owner Produced Part, what should he have done?
Answer:
The owner should have used the original manufacture’s prints and specifications (FAA approved design). It would have saved him time, money, and maybe his life.
Reverse engineer to develop a design if you must, but do your research and submit the resulting design to the FAA for approval. Depending on the complexity of the part, reverse engineering may result in a new design. This design is the aircraft owner’s, not the original manufacturer’s, and is not automatically FAA approved. The finished part must still meet the requirements of the performance rules of section 43.13. Always contact your local FSDO for guidance.
Produce the new part to conform to the approved design. Nothing more, nothing less. Stronger is not always better.
The aircraft owner (part’s producer) or the technician who installs the part should document or memorialize the production of the part in the aircraft records. It would be wise if the installing technician requires the part producer (aircraft owner) to memorialize the parts production in the aircraft records with a statement worded in a similar form as the one below, on this page.
After the part producer memorializes its production. The installing technician must make a maintenance record entry indicating that he or she installed the part. After all, installing the Owner Produced Part is a maintenance function. Aircraft owners can perform preventative maintenance, but not maintenance.
Eliminating the Confusion
A maintenance technician can repair a part, but sometimes the distinction between repairing a part and producing a brand new part is hard to determine. The circumstances surrounding the repair, the part’s complexity, availability of manufacturer’s data, and industry practices all are determining factors. For a lack of a better term I call making this determination the "Test of Reasonableness."
Example Scenario: An aircraft wing is damaged. The damaged parts include a wing rib, a 24-inch stringer, and wing skin. The aircraft Structural Repair Manual provides material specifications for the skin and stringer. A new wing rib is purchased from the aircraft manufacturer and the technician fabricates a stringer and wing skin using the damaged parts as a template. The technician installs these parts and repairs the wing in accordance with the manufacturer’s instructions.
Is this a repair or did the technician produce a new part? The stringer and wing skin do have a part number in the parts catalog for that aircraft, so let’s consider the following facts:
The material specifications were published and readily available.
The parts were simple and the fabrication processes for the parts involved common tools, skills, and standard industry practices.
Templates for the reliable reproduction of the parts were available (Design).
The parts were incorporated into a repair in accordance with the manufacturer’s instructions.
In this case, the "Test of Reasonableness" would determine this to be considered a repair, even though the technician did fabricate a stringer and skin.
Reality Check
Maintenance technicians must face a cold hard fact. Aircraft owners can make parts, but they cannot install them. Installing Owner Produced Parts is a maintenance function and only technicians can do that. That makes technicians the "gatekeepers" for parts and guardians against the introduction of substandard and unapproved parts into the fleet. Under this rule the responsibility is the technician’s to determine airworthiness before returning the product to service. There is no one else to shift the burden of blame to. The technician’s name is on the blame line.
Owner Produced Parts can be summarized as follows:
Under the Federal aviation regulations, aircraft owners can produce a brand new part for their aircraft; technicians and repair stations can’t.
For a part to be considered "owner produced," the owner must have participated in its manufacture in at least one of the five ways prescribed in the 1993, Memorandum.
An Owner Produced Part must have all four characteristics of an approved part before it is considered a FAA approved part and eligible for installation.
Sometimes the distinction between producing a new part and making a repair is hard to determine. When in doubt call the local FSDO and ask for guidance.
Maintenance technicians are the gatekeepers for parts entering service in the fleet. Technicians bear the lion’s share of the responsibility. The technician’s name is on the blame line.
The availability of parts is a constant problem with our aging general aviation fleet. As time passes, Owner Produced Parts may be the only alternative available for maintaining some of it. With the passage of time, technicians are going to be increasingly forced to face the challenge of determining the airworthiness of Owner Produced Parts. There are five points summarized here. Remember the five and stay alive!
Don Dodge is the Airworthiness Safety Program Manager at the South Carolina FSDO.
Calling FSDO in the morning. If this works out I can do a CAD drawing of "a" strut to send in to the FSDO. If approved I will make it avaliable to the group so anyone that would like to make their own will be able to.
Say I have an aileron control rod with one end squashed. Now, in reality, I'm going to go get another used one, and that's my story and I'm sticking to it. With money, even.
But, I'm working with a airplane built before WWII, and I don't have a solid faith in being able to find used parts still good for everything for forever.
Given that I can't find a blueprint for the 15-rib wing BL12-65, how would I be legal to engineer the part, given that no drawings for it appear to exist, and the factory either doesn't actually exist and isn't interested in returning phone calls?
By the same token, if I made a drawing of it in autocad with all dimensions, and tested the already-destroyed part to determine alloy and heat treating (none), would that be drawings enough?
Or is the real answer that I'm ah, up a creek without a paddle if the world runs out of old spares, because there are no drawings, no processes, no factory support, and no designs - leaving me with the choice of scrapping the airplane for lack of a single part, installing an unapproved new part or declaring my plane experimental and putting in the same new part?
Many months ago the foundation was working on making these drawing available to members. I think most of us are interested in assembly drawings showing rib locations, assembly notes, etc. We do not need drawings to re-produce every part.
I have not seen this disscussed in a while, where does all of this stand?
A wing rib is a simple part. It is made out of standard materials so all you need is a log book entry by a A&P signed off by an IA I believe because it is a major not a minor repair.
I will have more on this by tonight I hope.
By the way I make ribs for Cessna's quite often. It is just considered a repair.
I was going to build a Bellanca Viking into an experimental a few years back but did not get it started before the rule change. Now I do not get credit for any work I perform on the fuselage as long as I am using a certified fuselage. Everything is considered a repair.
Just got off the phone with the FSDO very nice guy. He is going to get back to me this morning. So far he says I do not need to do anything other than just install the owner manufactured part. No approval is needed through him. He is making sure that if I manufacture the strut as a nonvented strut that I will get rid of the AD repetativeness.
You wont need any PMA or all that garbage...PMA stands for Parts Manufacturing Approval...as long as you're not going to sell these to anyone, you don't need a PMA.
John
Just got word back from FSDO. Owner manufactured part OK no need to have anything approved. Catch is you still need to do the AD unless you get alternative method of complience. This should not be too hard if the strut you made was a sealed strut like the new ones.
One other thing that I thought about is no need to even make a new strut if this is the case. All we have to do is come up with an alternate method of complience. and send it in for approval.
Sorta like this; After initial inspection if there is no sign of corosion fill the strut with linseed oil and drain. At each annual fill strut with linseed oil and drain. After ten years from initial inspection do another inspection. Another way would be to inspect, linseed treatment then seal. I will look into getting someone who is more of an engineer to give a better example. It could be that all we have to do as a group is find someone who can come up with a viable alternative to the repet. inspection.
I was wrong in post#2...Indeed, for owner produced parts there is of course an established FAA system, and I apologise for any confusion, because I am one who has repeatedly promoted the owner-produced parts process on this forum.
find someone who can come up with a viable alternative to the repet. inspection.
To be honest, new struts from the already approved manufacturers is the only practicable way to accomplish this, for the money...but I'm willing to be corrected again.
I was wrong in post#2...Indeed, for owner produced parts there is of course an established FAA system, and I apologise for any confusion, because I am one who has repeatedly promoted the owner-produced parts process on this forum.
To be honest, new struts from the already approved manufacturers is the only practicable way to accomplish this, for the money...but I'm willing to be corrected again.
Rob
I don't think so.
Just for argument look back on the SB and you will see a couple of feeble attempts to get the repetative action extended. No data was submitted. Now lets revisit that and give the FAA some hard data from an engineer or DAR. For argument lets say that the DAR gives recomendation that as long as the original strut was in servicable shape and filled with oil then sealed the strut would then perform for the next 10 years? 20 years? in the condition it was when sealed. Now subit that to the FAA as an alternative method of compliance. Now if you need new struts you need new struts, but if yours are in great shape why buy new struts just to get the AD removed. If the FAA approves it, it will save the owners of Taylorcraft that have servicable struts the hassle and cost of inspection not to mention $3,500.00 for new struts that they do not need. The FAA already removed the AD if the struts were sealed so now it is more of a paperwork thing.
The FAA already removed the AD if the struts were sealed so now it is more of a paperwork thing.
Dan
You hit the magic "paperwork" word. Someone had to come up with an approved method for "teminating action" of the AD.
Three companies did, but only two (Univair and Airframes) came up with the goods at the time (later Wag Aero did too), mostly based upon the old Piper AD terminating action (mistaken reasoning in the background, in my view). They profited from it (as I would have done in their shoes, so no slur there).
It might have cost them a bunch to persuade the FAA, possibly more than a private individual could afford.
if yours are in great shape why buy new struts just to get the AD removed
No practicable reason...just the law.
Individuals on this forum (they know who they are) were instrumental in getting not only the XRay AMOC approved, but also the extension from 2 to 4 years.
In summary, Dan, we all know it's a load of hogwash...so few have failed the AD inspection (if any), but we have to comply with the regs, and unless we are in the regulation-making business, then we have to go along with the rule-makers. It's silly, but it's life.
I wish you well with your endeavours; let us know how you get on.
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