Ed Haywood
En-Route
I am currently doing a bare frame restoration of my '78 Decathlon, which is basically an exercise in parts gathering. I am leveraging multiple sources for parts, including TC/PC, PMA, TSO, STC, Standard, and Owner Fabricated. That has pushed me to learn the regs in greater detail, so that I don't waste my supervising IA's time.
AC 20-62 has been a huge help in clarifying terminology. Discussion forums and articles on the internet are rife with vague terms like "aircraft grade" which are meaningless for actually determining whether parts are eligible. The AC lays out the different categories of eligible parts and provides information on how to verify them.
Take electrical crimp terminals, for example. Now I know that crimp ring terminals are a standard part which is produced to a published specification. Checking AC 43.13-1B tells me that terminals should meet MIL-T-7928. Now I can check the manufacturer and product line to verify that the terminals I am buying meet that specification. If I really wanted to dig, I could read the identification requirements in the specification, which probably specifies some sort of stamp on the terminals and/or label on the packaging. If I really really wanted to be fussy, I could request traceability documents to prove the terminals I bought were actually made by the labeled manufacturer.
So here is my question: now I know how to find out if a part is eligible to install. But I'm still unclear on the process for determining whether an eligible part can be installed on a particular TC aircraft. Is there a similar product that rolls up all the regs into an easy to understand summary or flow?
Right now my general understanding is that step 1 is determining whether an alteration or repair is minor or major.
If major, then approved data must be used. That approved data could come from a TC, STC, field approval, or other (what?). Approved data would normally include a parts list with instructions and drawings necessary to comply. Any deviation from the parts list would not be approved data.
If minor, then acceptable data must be used. The primary source of acceptable data would be AC 43.13-1B, which is probably not titled "acceptable methods" by accident. So if I use acceptable methods to install approved or acceptable parts, then I am in compliance with regulations.
But obviously there are a lot of holes in my understanding. A big one concerns installation of TSO products. I understand that a TSOA is a production approval, and establishes that the product meets performance specifications in the TSO. I also understand that a TSO is not an installation approval. So where does the installation approval come from?
Not so hypothetical example: I want to replace my fuel pressure gauge. The FP gauge is required equipment per my AFM. The TC holder has approved specifications for several gauges such as the EI FP-5. The EI also is produced under TSOA, and has an STC with AML. So I see that I have 3 possible paths to justify installation:
1. Approved data via TC specification.
2. Approved data via STC AML.
3. Determination of minor alteration and use of acceptable data. (?????)
The 3rd one is the most confusing. The EI FP installation instructions say the following:
I assume what they are saying is that the TSO plus AC 23.955-1 provides acceptable data?
So in general terms, what is the process for obtaining acceptable data on whether a TSO gauge (or other product) can be installed as a minor alteration? Is it a matter of comparing the TSO performance specifications meet the requirement? If 2 gauges meet the same TSO, would that be acceptable data to replace one with the other?
AC 20-62 has been a huge help in clarifying terminology. Discussion forums and articles on the internet are rife with vague terms like "aircraft grade" which are meaningless for actually determining whether parts are eligible. The AC lays out the different categories of eligible parts and provides information on how to verify them.
Take electrical crimp terminals, for example. Now I know that crimp ring terminals are a standard part which is produced to a published specification. Checking AC 43.13-1B tells me that terminals should meet MIL-T-7928. Now I can check the manufacturer and product line to verify that the terminals I am buying meet that specification. If I really wanted to dig, I could read the identification requirements in the specification, which probably specifies some sort of stamp on the terminals and/or label on the packaging. If I really really wanted to be fussy, I could request traceability documents to prove the terminals I bought were actually made by the labeled manufacturer.
So here is my question: now I know how to find out if a part is eligible to install. But I'm still unclear on the process for determining whether an eligible part can be installed on a particular TC aircraft. Is there a similar product that rolls up all the regs into an easy to understand summary or flow?
Right now my general understanding is that step 1 is determining whether an alteration or repair is minor or major.
If major, then approved data must be used. That approved data could come from a TC, STC, field approval, or other (what?). Approved data would normally include a parts list with instructions and drawings necessary to comply. Any deviation from the parts list would not be approved data.
If minor, then acceptable data must be used. The primary source of acceptable data would be AC 43.13-1B, which is probably not titled "acceptable methods" by accident. So if I use acceptable methods to install approved or acceptable parts, then I am in compliance with regulations.
But obviously there are a lot of holes in my understanding. A big one concerns installation of TSO products. I understand that a TSOA is a production approval, and establishes that the product meets performance specifications in the TSO. I also understand that a TSO is not an installation approval. So where does the installation approval come from?
Not so hypothetical example: I want to replace my fuel pressure gauge. The FP gauge is required equipment per my AFM. The TC holder has approved specifications for several gauges such as the EI FP-5. The EI also is produced under TSOA, and has an STC with AML. So I see that I have 3 possible paths to justify installation:
1. Approved data via TC specification.
2. Approved data via STC AML.
3. Determination of minor alteration and use of acceptable data. (?????)
The 3rd one is the most confusing. The EI FP installation instructions say the following:
If your aircraft is not covered on our STC (found at the back of this manual), you must perform the flow and pressure tests in FAA document A.C. 23.955-1 (Substantiating Flow Rates and Pressures in Fuel Systems of Small Airplanes) to insure safe and proper operation.
I assume what they are saying is that the TSO plus AC 23.955-1 provides acceptable data?
So in general terms, what is the process for obtaining acceptable data on whether a TSO gauge (or other product) can be installed as a minor alteration? Is it a matter of comparing the TSO performance specifications meet the requirement? If 2 gauges meet the same TSO, would that be acceptable data to replace one with the other?
Attachments
Last edited: