Getting Training to Support Your DAR-56 8130-3 Tag Privileges

Still haven’t started applying for the DAR 56 program?  This is the program that allows employees of accredited distributors to issue 8130-3 tags for parts that meet certain FAA-defined airworthiness criteria.  If you are having trouble getting started, then the best way to start is to take the FAA’s online DAR course about how to issue an 8130-3 tag.

We’ve previously published the details about how to apply for the program.  ASA member Jay Rosenberg has provided us with detailed instructions on navigating the FAA’s 8130-3 training class.  Jay is the Director of Operations and Quality for United Aerospace Corp.  He also served as the Chairman of the ASA Quality Assurance Committee and as an ASA Board member.  Here are his guidelines:

I mentioned that I would send you some instructions on clarifying the registering process for the DAR-56 online training site.

  1. You need to setup an account profile: https://av-info.faa.gov/DsgReg/login.aspx
  1. After enrolling you need to sign in and choose the course (“Issuance of 8130-3 for Domestic and Export Approvals of Engines, Propellers & Articles Only”)
  1. Pay for the course ($100.00)
  1. After enrolling and choosing the course you will see a page with your course enrollments which show two courses. One is on the DMS system and the other one is about 8130-3 for domestic and export.
  1. When you click the schedule tab you have to go thru a few pages and choose the right course:
    1. Designee and Delegated Organization training
      1. Designated Airworthiness Representatives
        1. Issuance of 8130-3 for Domestic and Export Approvals of Engines, Propellers & Articles Only

    After doing all this then you get to web link:

    https://av-info.faa.gov/DsgReg/Sections.aspx?CourseInfoID=395

  1. After reading all the material you will be required to take an exam.

You only have only one shot at it to pass…!

If you pass the certificate will be listed on your enrollment screen to download.

We’ve heard from a number of members that one problem is that the DAR-56 program only supports a small number of the parts that need 8130-3 tags, and that most of the parts that now need the tags are not eligible under the program.  That may be true, but it is not a reason to eschew the program.  A partial solution is better than no solution – and ASA is working with the FAA on other partial solutions to try to better resolve the issues facing the industry.

Remember – there is only a limited time to take advantage of this program, so you need to get each of your eligible employees qualified as soon as possible in order to get the maximum benefit from the program.  The first step to that DAR-56 qualification is to get the eligible employees trained!

DAR-56 Advice: Apply Under Your Current AC 00-56 Revision Number (even if you are still under “00-56A”)

We have received word that many ASA members are expeditiously pursuing DAR-56 credentials.  This is the temporary program that delegates limited 8130-3 privileges to individuals working in AC 00-56 environments.  It is great to hear that so many individuals in AC 00-56 companies are pursuing these credentials.

In a recent call with the ASA members, they pointed out that a significant portion of the AC 00-56 community is still accredited under AC 00-56A (not “B”).  The cancellation clause of AC 00-56B explains that a distributor can maintain its accreditation under the “A” revision until it runs out and is renewed under the normal renewal schedules:

“Distributors already in the database of accredited distributors under AC 00-56A may maintain their accreditation under the AC 00-56A standard until their accreditation expires, is superseded upon renewal, or is cancelled or removed by the distributor’s accreditation organization.”

So some accredited distributors could retain the “A” accreditation as late as August 2018 (90 days after the publication of the “B” revision + three years, when their accreditation expires).  The community continues to roll from “A” into “B” between now and 2018.

The cancellation clause of the “B” revision incorporates-by-reference and grandfathers the then-existing “A” revision accreditees.  Therefore, it seems logical that we should read the language of the DAR-56 memo to include the remaining accredited distributors who are still under the “A” revision.  There was nothing added by the “B” revision that would be necessary to the structure of the DAR function code 56 program – the “A” revision provided the structure necessary to manage the DAR FC 56 functions.

The problem, of course, is that the sample letter requires confirmation that “The organization listed in the letter is an Accredited Distributor in accordance with FAA Advisory Circular 00-56B.” This appears, on its face, to possibly exclude those companies that are still accredited under the “A” revision.

We asked the FAA how they want applicants who are still under the “A” revision to handle this?  They responded by explaining that it is acceptable for applicants to state “The organization listed in the letter is an Accredited Distributor in accordance with FAA Advisory Circular 00-56A.”  The response came from Scott Geddie, who leads the branch that is processing DAR-56 applications (so he can speak authoritatively on how the FAA will process DAR-56 applications).  Here is the text of the FAA’s response:

Jason

It was certainly not our intent to restrict those that are currently accredited under the “A” revision given the revision “B” guidance that says:  “Distributors already in the database of accredited distributors under AC 00-56A may maintain their accreditation under the AC 00-56A standard until their accreditation expires, is superseded upon renewal, or is cancelled or removed by the distributor’s accreditation organization.”

I believe the best course of action is for the Limited DAR-F applications and their corresponding letters of endorsement to reference the applicable revision of AC 00-56 that they are currently under.  My office will process emailed applications that include the reference to the “A” revision of the AC.

Thanks,
Scott Geddie
Manager, AIR-160, Delegation and Organizational Procedures Branch
Ph: (405)954-6897

Do you have questions about the DAR-56 program? Let us know your questions – we will work with the FAA to try and get answers that can benefit the entire distribution community.

Obtain 8130-3 Tags For Your Inventory – Limited Time Only!

Have you ever wished that there was an easy way to obtain 8130-3 tags for the obviously airworthy articles in your inventory?  Now, you can become a DAR and issue your own 8130-3 tags!  ASA has worked with the FAA to develop a limited program that will allow employees of accredited distributors to obtain DAR privileges to tag certain items in existing inventory.
The program creates a new function code 56 (because of the association with AC 00-56).  This is a limited function code for employees of accredited distributors that permits issue of 8130-3 tags for parts with certain types of clear evidence of production under FAA production approval.  The program can be found in this attached file.
This program is necessary because of the new emphasis on 8130-3 tags created by the FAA-EASA Maintenance Annex Guidance (MAG).  Many FAA inspectors have required repair stations in the US to adopt receiving requirements that only permit receipt of aircraft parts with 8130-3, EASA Form One or TCCA Form One.  Parts with traditional manufacturer’s certificates of conformity (for example) are excluded from the MAG guidance!  This temporary ability to obtain 8130-3 tags permits some existing inventories of good parts to be tagged in order to meet the new standards created by the Maintenance Annex Guidance

What Can be Tagged?

A DAR with Function Code 56 privileges will be able to issue an 8130-3 tags for parts manufactured by an FAA production approval holder (PAH) if the part and its documentation meets one of the criteria below:
1. Certificate of Conformity/Statement of Conformity from the PAH.  The part number and serial number, if applicable, must match any marking on the part.
2. Certificate of Conformity/Statement of Conformity or shipping document from a PAH supplier and verification of that supplier’s direct ship authorization.
3. Part markings made under 14 C.F.R. § 45.15 that include the PAH’s name or identifier (including PMA markings, TSOA markings and critical part markings).  If the PAH name or other identification is not included in the part marking, then you will need a Certificate of Conformity/Statement of Conformity as described in paragraphs (1) or (2) above.

Qualifications

An applicant for the DAR-56 program must meet all five of the minimum qualifications:
1. AGE: Be at least 23 years of age.
2. EMPLOYMENT: Be employed by an accredited distributor at the location(s) from which the 8130-3 will be issued.  The FAA has not clarified whether this needs to be full-time or part-time nor have they excluded contract employment.  In the absence of clarification, applicants should assume that all categories of employment are acceptable.
3. INDEPENDENCE: Be assigned to a position in the business with sufficient authority to allow the DAR to administer the delegated function effectively without undue pressure or influence from others.
4. EXPERIENCE: Have a minimum of 12 months actual working experience for the accredited distributor under the distributor’s quality system, specifically:
a. Experience in either receiving inspection and/or quality assurance processes; and,
b. Experience reviewing documentation which can be used to verify that the article is traceable to the PAH, such as a FAA Form 8130-3 and Certificate of
Conformity/Statement of Conformity from a PAH.
5. TRAINING: Must have successfully completed FAA course: Issuance of 8130-3 for Domestic and Export Approvals of Engines, Propellers, & Articles Only.

Application Process

Scan and submit the following three documents by email to 9-AIRI60-LimitedDARF@faa.gov:
1. FAA training certificate of completion from the required class [FAA course: Issuance of 8130-3 for Domestic and Export Approvals of Engines, Propellers, & Articles Only]
2. FAA Form 8110-14, Statement of Qualifications (should be signed by the individual employee).
3. A letter of endorsement signed by a management representative from the accredited distributor location where that individual employee is requesting to exercise the authorization.
  • Where the accredited distributor has more than one accredited location, the applicant may apply to exercise privileges at each accreditation location
    under a single management endorsement letter.  The Memo includes a sample letter and explains what must be in the letter.

The applicant is expected to retain the original application materials in his/her records.  FAA Headquarters will review the application.  When an applicant is selected, the FAA will email the applicant a Certificate of Authority.

Limits

There are many categories of airworthy parts without 8130-3 tags that will not be covered by this DAR-56 program.  This is not a solution to all of the problems caused by the implementation of the Maintenance Annex Guidance.  many ASA members will still need to rely on traditional DARs.
The DAR-56 program is limited in time.  All Limited DAR-56 appointments under this program will be terminated on September 30, 2017.  We have discussed with the FAA that there will be a continuing need for the program, because some FAA-PAH manufacturers continue to produce parts without 8130-3 tags.  ASA intends to petition for an extension of the program if it appears that the program remains necessary, but ASA members should not plan on the FAA granting that petition (they have already told us that they will reject such a petition).

Advice

The FAA intends that this DAR-56 program be used to tag existing inventory in order to make it saleable under the new documentation standards of the MAG.  The FAA has stated that they intend to issue privileges to all eligible applicants, in order to facilitate this process (note that this does not give you a legal right to the privileges – the FAA retains the discretion to limit or terminate the program at its discretion).
Many of our members have a substantial existing inventory that is eligible to be tagged under this program.  We have spoken with members who have said that some inventories could take YEARS in order to tag the entire inventory.  We advise accredited members to seek DAR-56 privileges for EACH eligible employee, in order to maximize your potential for issuing 8130-3 tags.  Accredited members should also apply as early as possible.
Once employees have received their certificate of authority, they should start to review existing inventory and issue tags for eligible parts immediately, in order to maximize the documentation of the inventory.
We also advise unaccredited ASA members to seek AC 00-56 accreditation in order to be eligible for the DAR-56 program.  ASA can discuss the process with you and can accommodate members who need AC 00-56 audits in order to participate in the program.

As the MAG 6 Implementation Date Looms, Repair Stations Adopt MAG 6 Documentation Limits

We have received multiple copies of an email from AAR from a number of ASA members. It is obvious that the letter has just gone out today (based on the number of ASA members forwarding it to us).

The AAR letter concerns “expectations around MAG 6.”  It confirms that AAR’s understanding is that they need FAA 8130-3 or EASA Form One with anything that is not a standard part.  The letter permits no deviations.

AAR is a leading company in the aviation repair station industry so their interpretation of the MAG 6 provisions is quite important.

The FAA issued FAA Notice 8900.380 to temporarily reopen the safety valve that was closed by MAG 6.  It specifically authorizes dual-certificated repair stations in the United States to accept parts without 8130-3/Form One and to inspect the parts to ensure airworthy condition (and then use them).

ASA has expressed concern to the FAA that efforts like FAA Notice 8900.380 could be ineffective because (1) repair stations already submitted their changes months ago at the behest of their PMIs and they may be unable to once again change their systems, and (2) many industry participants view the MAG as operating at a “higher level” than the Notice and therefore discounted the Notice’s effect (right or wrong – this is still a popular industry perception).

There are parts that are necessary to safe operation of aircraft, but that will not have 8130-3 tags, despite the fact that they are susceptible to airworthiness determination under normal FAA Part 43 standards.  Remember – it only takes one small part to interfere with an entire maintenance function.  I fear that firm documentation positions like those expressed by AAR could lead to one of two possible resolutions:

  • Air carriers will have to ground aircraft because the airworthy part does not have an 8130-3 tag (or Form One), and therefore can’t be accepted and installed by the repair station; or,
  • Repair stations will circumvent their own written systems in order to bring in parts without 8130-3 tags, despite language in the system requiring such a tag.

Neither of these options is desirable.  I am afraid that the (B) option will be the one that occurs most in the real world.  I fear that this will occur because the parts are thought to be good and the maintenance needs to be performed.  I am afraid of this occurrence because once companies start circumventing their written systems, those written systems start to lose their integrity.  At a time when the industry and FAA are examining greater reliance on Safety Management Systems, anything that undermines the safety culture of following the company’s written system is detrimental to the future of aviation safety.

Distributors who are supporting dual-certified (FAA/EASA) repair stations should remind those customers that FAA Notice 8900.380 explicitly permits receipt of parts without 8130-3/Form One when the repair station inspects them for airworthiness (as has always been the case); and guidance like FAA Advisory Circular 20-62E still is effective in recommending reliance on other indicia of airworthiness, such a manufacturer’s certificate of conformity.  The Notice is temporary but we are still working with FAA to establish a better resolution to the issues facing the industry.  Ask your affected business partners to ensure that their systems are consistent with FAA Notice 8900.380, and ask them to announce their willingness to accept parts for inspection when those parts bear other indicia of airworthiness.

FAA Notice 8900.380 is CHANGED and this Affects How Repair Stations May Receive Parts

Immediately after the FAA issue Notice 8900.380, they reissued it with small, but significant, edits to the original language. This information was sent two weeks ago to ASA members by e-mail but I just realized that I forgot to include it in the blog!

The changed language seems to help the situation faced by distributors, by explicitly recognizing that repair stations may inspect and receive parts without 8130-3 or Form One – but only for a one-year interval, and only when the repair station’s inspection is consistent with its manuals.   A repair station rated to perform maintenance on a top assembly is also rated to inspect any component part to determine its eligibility for installation in the next higher assembly, so this one year inspection permission will be useful.

The new Notice isn’t numbered differently nor does it have change markers.  So it is important to ensure you have the most recent version of the Notice, and it is very easy to have the wrong version.

While this is unusual (re-issuing a notice with changes, but with no way to distinguish the changed version from the original), we will accept the change as it expands the type of parts that a 145 can inspect. These edits are beneficial to the industry.

Remember the below information only deals with 1) confirming that a 145 can inspect a part without an 8130-3, 2) tagging that part as inspected and 3) bringing it into the 145’s system (allowing a dual-certificated 145 to buy an aircraft part without an 8130-3 tag and use it in their work).

This does not change the NOTE section dealing with grandfathered parts.  This area is still being discussed with the FAA and EASA, but the grandfather clause has been confirmed by FAA to extend only to parts in the repair station’s inventory by October 1, 2016.

The edits to Notice 8300.380 are:

(b) Inspections. For the purposes of this notice, inspections may be performed on:

(1)  New parts received in inventory before October 1, 2016, that are not accompanied by FAA Form 8130-3, a dated certificate of conformance, or similar documentation issued by a U.S. PAH or supplier with direct ship authority in accordance with the notes in MAG CHG 6, Section B,Appendix 1, subparagraph 10k)(1)(a) and Section C, Appendix 1, subparagraph 7c)(1)(a); and

(2)  New parts released by a U.S. PAH received on and after October 1, 2016, that are not accompanied by FAA Form 8130-3.

The Notice clarifies a few points and provides no relief on several areas:

  • Effective date for MAG 6 parts documentation section is October 1, 2016.
  • Although MAG CHG 6 does not prohibit repair stations from inspecting an article or subcomponent that they are rated and approved to work on for return to service, the notice imposed certain limits on what parts are permitted to be inspected in this way. Repair station can issue an 8130-3 for any part received without the documentation required by the MAG and issue an 8130-3 with a dual release statement if the part meets one of these two conditions:
    • New parts in inventory prior to October 1, 2016 that do not have an 8130-3, dated C of C; or similar document issued by the PAH or supplier with direct ship authority.
  • So a repair station can purchase/inspect a new part from a distributor even if that part doesn’t have an 8130-3, before or after October 1, 2016. The 145 would inspect the part and issue an 8130-3 as part of the 145’s system.  This doesn’t apply if the part does not qualify for an 8130-3.
  • A repair station can also purchase/inspect a new part from a distributor before October 1, 2016, if that part does not have do not have an 8130-3, dated C of C; or similar document issued by the PAH or supplier with direct ship authority.
  • There are still some limitations to these privileges, so be sure to analyze your transactions carefully!

QUESTIONS AND ANSWERS

Q: What about new parts in a distributors inventory that were manufactured  before October 1, 2016 and that do not have an 8130-3?

A: After October 1, 2016, these parts need an 8130-3 to sell them to an FAA EASA dual certified repair station. ASA sought a re-interpretation of some language that would permit distributors to sell these parts to repair stations after October 1, 2016, and this lead to the new language of Notice 8900.380.  THE NEW NOTICE OFFERS SOME MORE OPTIONS TO DISTRIBUTORS.  One significant option is that for the limited one-year time period of the Notice, dual-certificated repair stations in the US may receive parts that do not conform to the MAG and inspect them for suitability.

 

Q: What if my parts don’t qualify for an 8130-3?

A: There are a number of categories of parts that do not qualify for an 8130-3 or Form One. One example is military surplus parts, which are permitted for use in civil aviation under conditions described in AC 20-62 and AC 20-142. For parts that are not permitted under the MAG and its interpretive notices, there may be no path to sell such parts to an FAA EASA dual certified repair station.

 

Q: What if my parts were made by a foreign PAH?

A: Although the FAA has signed bilateral aviation safety agreements in which the US has agreed to accept certain foreign-produced parts, if there is no mechanism in the MAG for accepting these parts, then this may inhibit repair stations from accepting these parts.  There appears to be no mechanism under the MAG for receiving a part made under production approval from a jurisdiction other than US, EU or Canada (like an Embraer part from Brazil).

 

Q: How do you get an 8130-3 when one does not exist?

A: For parts with evidence of airworthiness and that were produced under a US production approval, you can apply through a designated airworthiness representative (DAR).  We understand that the expense of a DAR may be too much in some cases.  If there are no DARs available, notify the FAA.  Please send a copy of your notification to ASA, so we can track these issues.

 

Q: What other remedies may be available?

A: ASA has pending litigation against the FAA but please know that there is no mechanism to force them to review this situation before October 1, 2016, and the actual resolution date is going to be sometime in 2017.  The US government opposes our appeal.  It is always possible that the court will rule against the industry.  ASA is also working directly with the FAA to achieve some reasonable resolution that will permit safe aircraft parts to be sold to the installers who need them, on an ongoing basis.

Update on MAG issue and ASA Efforts

What is the Issue?

The latest revision of the Maintenance Annex Guidance [“MAG”] creates a new system in which existing industry documentation (which is acceptable under current EU and US regulations) becomes unacceptable within US repair stations. It is objectionable because it imposes new documentation standards that do not exist in either US or European regulations, and in doing so creates a documentation requirement for aircraft parts that will render worthless significant portions of existing aircraft parts inventories.

Under current US standards, no documentation is required in order to receive an aircraft part into a repair station’s inventory. See, e.g., FAA Chief Counsel’s Opinion Letter (August 6, 2009) (stating “there is no Federal Aviation regulation that requires traceability of an aircraft part to its origin” and explaining that parts may be found airworthy based on documentation, markings, or inspection and testing).  The repair station may install the part as long as it confirms that the article will return the product to a condition “at least equal to its original or properly altered condition.” 14 C.F.R. § 43.13.

The European system is a bit different. The European system distinguishes parts into six different categories, but for purposes of this analysis only two are relevant.

The first is serviceable parts – those in a satisfactory condition. Serviceable parts must be accompanied by the European manufacturer’s document known as the EASA Form One, or an equivalent document. EASA 145.A.42(a)(1).  EASA has recognized that the FAA 8130-3 tag is an equivalent document for receipt purposes (when signed on the left side).  EASA AMC M.A.501(a) ¶ (5)(a) (documents under the terms of a bilateral agreement); Technical Implementation Procedures for Airworthiness and Environmental Certification Between the FAA and EASA, ¶ 5.1.10 (Rev. 5 Sept. 15, 2015) (the bilateral agreement).

Because there are many articles produced by US manufacturers that do not bear 8130-3 tags, a ‘safety valve’ provision allows European repair stations to accept articles without such documentation.

There is a second provision in the EASA regulations that permits “unserviceable parts” to enter into a repair station without documentation when they are intended to be maintained. EASA 145.A.42(a)(2).  The European definition of “unserviceable” includes articles that are missing “necessary information to determine the airworthiness status or eligibility for installation.” EASA M.A.504(a)(3).  Thus, any new aircraft part that is missing an EASA Form One or 8130-3 (whichever is appropriate) is deemed unserviceable and can enter a repair station without documentation. Such an article may then be inspected to serviceable condition and installed if it passes inspection. See, e.g., EASA AMC M.A.501(a) (Installation); EASA AMC M.A.613(a) (Component certificate of release to service).  It cannot be treated as serviceable until it undergoes that inspection.

The problem with the MAG is that it closes the safety valve that allows acceptance of new parts without an 8130-3 or EASA Form One. It does this by establishing two different categories that are inconsistent with the “serviceable/ unserviceable” categories established under European law. The two categories are “new” and “used.” Under existing European law, a new part without the correct documentation can be received as unserviceable, and subsequently inspected to serviceable condition, but under the MAG, a new part is required to have an 8130-3 or EASA Form One. There is no exception under the MAG for new parts without the designated documentation – they are simply excluded.

So How Does this Affect Members?

Actual implementation has already shown that the language of the MAG is being enforced by FAA field inspectors as mandatory even though there is no regulatory basis under US or EU law for such enforcement. Thus, the real implementation has been that all US repair stations with EASA credentials are required to have a written manual (known as a Supplement) requiring them to exclude new parts without 8130-3 documents or EASA Form One documents – even though both US and EU regulations permit acceptance of these new parts.

This is starting to have a real world effect that will be expanded with the October 1, 2016 implementation.  Distributors are finding that parts that they could sell with manufacture’s trace (or other reasonable trace) are no longer “good enough.” Repair stations are starting to demand 8130-3 tags on everything (including parts that are not eligible for 8130-3 tags).

What is ASA Doing About It?

ASA continues to work with the FAA to achieve a solution.  FAA management recognizes that this is a potential problem, and they have been optimistic about finding a solution.

Our first efforts were to find a way to “grandfather” existing aircraft parts inventories.  FAA supported this solution, but EASA opposed it.

We have also asked for guidance explaining that repair stations can apply US standards to parts destined for US registered aircraft, but early implementers have shown that this idea is not consistent with what FAA inspectors are requesting so it is likely to be ineffective.  In addition, it creates a logistical problem for component repair stations who may not know the ultimate destination of the components on which they are working.

We are now looking at new ways to obtain 8130-3 tags for good inventory.  This will not be a 100% solution to the impediment created by the documentation requirements, but it should help preserve the value of some inventories.  We expect to continue discussions of this proposal with the FAA, next week.

On the legal front, we continue to pursue a halt to the MAG documentation requirements.  This would not affect the EASA regulations – they still apply where appropriate – but to the extent that the MAG imposes additional standards that would be enforced by the FAA, we have asked the DC Circuit Court to issue a “Stay” that would prevent the FAA-enforcement of these new documentation requirements.

Today, as part of this effort, we filed this Motion for a Stay.  We would like to thank the many ASA members who worked with us to develop  affidavits explaining the factual situation of 8130- 3tags and aircraft parts inventories.

Do NOT state “domestic shipment only” or “not an export approval” on an 8130-3 tag

On June 28 the FAA issued a policy memo (AIR100-16-110-PM04) that forbade parties from stating “domestic shipment only” or “not an export approval” on the 8130-3 tag.

“This memorandum provides clarification on the use of “domestic shipment only” and “not an export approval” in block 12 of FAA Form 8130-3 (hereafter, tags). Inspectors, designees, delegated organizations, and persons authorized in accordance with a production approval holder’s approved quality system to issue tags are directed to not add “domestic shipment only” and “not an export approval” to block 12.”

This language tended to impede subsequent exports.  Many people mistakenly thought that this language was meant to prevent a subsequent export.

History

Use of this sort of language also ignored the original purpose of the “domestic tag.”  It was originally meant to create a kludge that made 8130-3 tags available to exporters.  It was called a “domestic” tag because it only certified compliance to domestic US standards, and not to any special import requirements of an importing nation.

Years ago, distributors were unable to obtain an export tag for parts. The reason for this began in 1963, the FAA published a Notice of Proposed Rulemaking (NPRM) to establish the rules for export airworthiness approvals (Subpart L of 14 C.F.R. Part 21).   They classified the world of aircraft assets into three classes:

(1) A Class I product is a complete aircraft, aircraft engine, or propeller, which—

(i) Has been type certificated in accordance with the applicable Federal Aviation Regulations and for which Federal Aviation Specifications or type certificate data sheets have been issued;
or
(ii) Is identical to a type certificated product specified in paragraph (b)(1)(i) of this section in all respects except as is otherwise acceptable to the civil aviation authority of the importing state.

(2) A Class II product is a major component of a Class I product (e.g., wings, fuselages, empennage assemblies, landing gears, power transmissions, control surfaces, etc), the failure of which would jeopardize the safety of a Class I product; or any part, material, or appliance, approved and manufactured under the Technical Standard Order (TSO) system in the ‘‘C’’ series.

(3) A Class III product is any part or component which is not a Class I or Class II product and includes standard parts, i.e., those designated as AN, NAS, SAE, etc.

This can be found today in older versions of the Code of Federal Regulations.  But this distinction no longer exists in the modern regulations.

The original 1963 NPRM suggested that export airworthiness approvals would be available for Class I and Class II products. It explained that export airworthiness approvals would not be necessary for Class III products, and that exporters could self-certify airworthiness with respect to those units.   This dramatically limited the impact of the proposed rule, because most articles fell into class III.

During the comment period for this new rule, a manufacturer wrote to the FAA and said that it could foresee a possible need in the future to apply for Class III export airworthiness approvals for its own articles.  The stated purpose of the rule was to facilitate trade, so when the Final Rule was published in 1964, the FAA added a clause stating that manufacturers could also apply for Class III export airworthiness approvals in order to meet the request of the commenter.  This was 30 years before ASA existed, so ASA was not around to broaden the language to include non-manufacturer exporters.

Years later, as the export 8130-3 tag became more popular in international commerce, and the FAA signed international agreements promising to provide the 8130-3 tags with exports,the distribution community began to see a need for the tags to facilitate their trade.  But the regulatory language only permitted manufacturers to apply for the export 8130-3 tag.  So the “domestic tag” was born in order to provide a tag that distributors could seek.  The “domestic tag” only certified compliance to US domestic standards – it did not certify compliance to any special import standards of any importing nation (it was up to the exporter to address such conditions, and at the time foreign trading partners were happy to take this tag).

The domestic tag also quickly became popular among domestic users in the US (notably, Northwest Airlines in the late 1990s was an early proponent of the use of the 8130-3 tag for domestic transactions).

For a short time, this limiting language (“domestic shipment only”) actually appeared in an earlier version of Order 8130.21. ASA sought clarification from FAA Management at the time.  We pointed out that the original purpose was to facilitate export for distributors, and FAA Management agreed that this language was inappropriate.   FAA Management confirmed that the inclusion of that language had been a mistake, because it contradicted the original purpose of the domestic tag.

In order to discern the reason for this errant language, FAA Management called in the employee who was responsible for the text of the Order and asked “why did you include this language?”  The FAA employee’s reply was to shrug his shoulders and say “I don’t know … it seemed like a good idea at the time.”  The language was removed from the next revision of 8130.21, but it continued to find its way into 8130-3 tags.

Over the years, the FAA has recognized that this language impeded export transactions without offering any redeeming value.  The policy memo closes the loop on this language by forbidding it.

ASA members who encounter parties who want to print “domestic shipment only” or “not an export approval” in block 12 of FAA Form 8130-3, should draw the issuing party’s attention to this FAA policy memo.

New FAA MAG Guidance Corrects Some Problems; But Documentation Challenges Remain

Revision Six of the Maintenance Annex Guidance (MAG)  has been released.  ASA has been working with both FAA and EASA contacts to make changes to the prior revision (rev. 5), because it included unnecessary restrictions that were not based on either US-FAA or EU-EASA regulations.

Many will remember that the MAG rev. 5 language included a number of unacceptable requirements.  Unacceptable provisions included a requirement that the part number be found in the TC holder’s parts catalogue (which would have excluded many PMA and TSOA parts, as well as OEM parts issued in advance of IPC changes) as well as a requirement limiting 8130-3 tags to those issued by PAHs (discounting 8130-3 tags issued by the FAA itself through its designees).  Most of the unacceptable language has been removed and/or remedied in revision 6.  The replacement language for new parts in MAG rev. 6 looks like this:

(a) New components must be traceable to the Production Approval Holder
(PAH) and be in a satisfactory condition for installation. An authorized
release document, as detailed below, must accompany the new
component.

This language is found in sections 10(k)(1)(a) (for US-based Repair Stations) and 7(c)(1)(a) (for EU-based Repair Stations) of the appropriate Sample Supplements in the MAG.  It explicitly requires traceability, without defining what sort of traceability is acceptable.   This is a potential problem: the FAA is taking an industry term for which there is no set meaning (and about which industry experts disagree) and is trying to use it as if it were an objective standard.  They have done this in other guidance, like FAA Order 8130.21H, and it has resulted in disagreements and confusion.  The traceability requirement also belies the various FAA Chief Counsel Opinion letters which have repeatedly asserted that there is no FAA regulation that requires traceability of an aircraft part to its origin.

Repair Station Experience

At the ASA Quality Committee meeting last Fall, members with repair stations expressed that their local FAA FSDO inspectors were requiring strict compliance with the exact language of the MAG Supplement (despite the fact that the language is explicitly labelled as a sample).  Repair station representatives also explained that they were being required by their FAA inspectors to have a single receiving inspection system.  This means that all of the parts that they receive would have to meet the EASA requirements and the MAG requirements (including parts ultimately destined for installation in FAA-registered aircraft).  They would NOT be permitted to receive parts that met FAA requirements (but not EASA requirements) for installation on FAA-registered aircraft (despite the fact that the regulations still permit this).

FAA headquarters has said that these are misinterpretations by the field offices and that they reflect unintended consequences; but when pressed about how they plan to remedy this, the FAA Headquarters representatives could only  suggest that we bring these situations to their attention on a case-by-case basis.  They had no plans to remedy these “unintended consequences.”

In light of this experience, ASA members should expect that most repair stations will be pressured by the FAA to strictly comply with the MAG language as if it were a regulation.  This means that the normal protections of the law may not apply to your transactions, and an appeal to the regulations may fall upon deaf ears!  If you encounter a repair station customer that has been pressured to limit their receiving inspection system in a manner that is more narrow than required by the regulations, then please talk to ASA and we will put you in touch with the right people at the FAA.

A New Source of 8130-3 tags

Last Fall, the FAA promulgated a new rule that permits production approval holders to issue their own 8130-3 tags. The MAG changes are meant to reflect this new privilege.  There are a lot of problems with this:

  1. The 8130-3 privilege was an option – not a requirement – so many manufacturers might choose not to issue 8130-3 tags (and this makes it difficult for distributors to economically and conveniently obtain those forms).
  2. While the EU has agreed to accept manufacturer’s 8130-3 tags, all of the other the US bilateral agreements require FAA 8130-3 tags.  This means that other trading partners might reject manufacturer 8130-3 tags as unacceptable.  When ASA met with the Civil Aviation Administration of China (CAAC) in March, CAAC expressed reservations about manufacturer 8130-3 tags and reminded us that the China-US bilateral agreement did not authorize acceptance based on manufacturer 8130-3 tags.
  3. The MAG rev. 5 language failed to adequately address the significant existing inventory that was not documented according to the new standards.
  4. Even if the other hurdles had not existed, the governments did not permit enough time to ramp-up 8130-3 tag issuance in order to meet the new demand imposed by the MAG revision.

The limits and burdens associated with this privilege have cause some manufacturers to decide that they are not going to issue these tags.  Large manufacturers like Boeing have said that they feel more comfortable sticking with their ODA program as a source of 8130-3 tags.  Smaller manufacturers fear that their local MIDO inspectors may impede them from issuing 8130-3 tags, and plan to stick with issuing their traditional commercial certificates of conformity.

The reason this new source of 8130-3 tags is important is because it was supposed to be a driving force behind the MAG rev. 5 changes.  And the fact that some manufacturers will not issue manufacturer-8130-3 tags on components means that the the FAA and EASA are operating under false assumptions as they manipulate the receiving requirements of repair stations.

Existing Inventory Problem – Grandfather Clause Failure

A significant disappointment in all of this is that the FAA and EASA recognized the need for a grandfather clause for existing inventory, but they failed to create a grandfather clause with enough breadth to reflect the realities of existing inventory.

In recognition of the fact that the new manufacturer-based 8130-3 tag-privilege was supposed to remedy a past lack of 8130-3 tags, the FAA and EASA agreed upon a grandfather clause that would apply to parts produced before October 1, 2016.  The grandfather clause was meant to apply to demonstrably airworthy parts without 8130-3 tags, that were produced before the October 1 date.  In order to take advantage of the grandfather clause, the parts were supposed to bear (1) evidence of airworthiness and (2) evidence of manufacturer before October 1.

Evidence of airworthiness is well understood and necessary in the industry. But the new grandfather clause requirement is that the evidence must consist of “a document or statement (containing the same technical information as an FAA Form 8130-3) issued by the PAH or supplier with direct ship authority.”  So common documents that would be excluded might include (but not be limited to):

  • Airline trace for new surplus parts (not issued by the PAH);
  • OEM C of C (typically does not contain all of the technical information contained in an FAA Form 8130-3);
  • OEM inventory list for a lot purchase (typically does not contain all of the technical information contained in an FAA Form 8130-3);
  • Spec 106 Form from the OEM-authorized distributor (even if it includes all of the technical information contained in an FAA Form 8130-3, it was not dated by the PAH).

This creates an initial challenge but there is some good news.  In an earlier publication of the guidance, found in FAA Notice 8900.360, the PAH documentation needed to have been dated prior to October 1, 2016.  This meant that undated PAH documentation was not usable.  This has been changed in the new version of the language.  This is important because it means that a distributor who possesses adequate evidence of airworthiness (meeting the guidance of the MAG) can produce their own evidence of manufacturer before October 1 by specifying that the article was released before October 1.

We wish that the FAA had been explicit that this was meant to ‘fix’ 8900.360, because we fear that some people will not realize that the later language of MAG rev. 6 was meant to be a remedy to incorrect language in the earlier Notice.  Based on our discussions with the FAA, the change in the date language was explicitly intended to remedy the earlier flaw in the Notice 8900.360 language.  Today, anyone ought to be able to look at a calendar, see that the date is before October 1, and certify that an existing article was manufactured by that date.  And distributors ought to be able to do this for their entire inventories by flagging those parts received by September 30, 2016 (a secure flag in the electronic inventory system ought to be adequate to serve as a basis for a distributor’s C of C that states that the part was received before October 1, 2016 and was therefore released prior to October 1, 2016).

More Unintended Consequences?

An interesting effect of this is that the United States may be somewhat increasing the US trade deficit in the near future.

Let’s say that we have two identical parts that were both produced by the same US production approval holder.  One of them was sold to a new parts distributor in the United States and it bore a standard Certificate of Conformity (which does not include all of the same technical information as an 8130-3 tag).  The other one was sold to a new parts distributor in Europe and it bore an export 8130-3 tag.  Now, a US repair station needs that part.  Existing inventory held by new parts distributors in the United States may not bear the right documentation to receive it under the MAG.  Even if the part is needed for a US-registered aircraft, FAA FSDO norms of requiring repair stations to apply the MAG to all received parts would preclude the part from entering the repair station’s system.  The new parts distributor in Europe, with the export 8130-3 tag on the part, will be the only one who can make the sale to the US repair station!

The FAA’s role is to protect aviation safety.  They do not have responsibility for protecting US competitiveness.  But this change appears to do nothing to enhance safety.  It does not address any known safety issue – it merely adds de facto documentation requirements that appear to circumvent the formalities of the Paperwork Reduction Act.  It is a little shocking that the FAA continues to publish documents that chip-away at US competitiveness without doing anything to enhance safety.

So What Does it All Mean?

EASA has approved about 1480 repair stations in the United States.  That is a very significant chunk of the US domestic repair station market, and it probably represents a substantially high percentage of the commercial aircraft repair market in the US.  This means that a substantial percentage of the commercial aviation repair stations in the US will be affected by this guidance (approaching all of them).  For US distributors, it is important to understand how to navigate through this.

If you have repair station customers that have written their manuals and supplements to require EASA-documentation for all parts received – including those destined for installation on US-registered aircraft – then you should counsel the repair station to revisit its procedures.  But for component repair stations who may not always know the final installation destination of the components on which they work, they may be stuck with applying EASA documentation standards.  Because the FAA is enforcing these EASA standards, the 8130-3 tag (and the EASA Form One) now become a transaction requirement in the commercial aviation market – including for purely domestic transactions where the FAA inspector has insisted on a single receiving system.

US distributors should be particularly aggressive in seeking out 8130-3 tags for inventory.  For inventory without 8130-3 tags, distributors need to ensure that they have access to a DAR (and also a back-up DAR) in order to ensure that they will be able to obtain 8130-3 tags as necessary.  If there are not enough DARs in your area, then please let ASA know so we can bring this fact to the attention of FAA Headquarters.

Due to commercial norms, non-US distributors typically obtain export 8130-3 tags when they receive parts from the United States.  This may give those distributors an advantage over their US counterparts who find it difficult to obtain 8130-3 tags for existing inventory.  Non-US distributors should take advantage of this while they can!

Finally, let us know what you think the effect of this guidance will be.  Will you be able to sell you inventory or does this threaten to devalue or block your inventory?  We would like to hear from the members about the real-world effects in order to judge our next steps.

FAA Delays MAG rev. 5 Provisions to Permit 8130-3 Revisions

As many of you know, the FAA issued a revision (rev # 5) to the US-EU Maintenance Annex Guidance (“MAG”) last September.  This revision was met with much resistance in the aviation community because it seemed to impose new documentation requirement that did not exist in either FAA or EASA regulations.  This could have become a problem for the ASA community because it would have imposed new documentation requirements that could have severely affected the value of existing inventories.

ASA has been working with FAA and EASA (as well as other trade association) to revise some of the language of the MAG.  Late in 2015, we reported some success when the FAA and EASA issued a letter to ARSA verifying that parts released by the production approval holder before April 1, 2016 would be ‘grandfathered,’ and would not be subject to the new documentation requirements.  In response to this decision, ASA has been advising members to record all parts in their inventories as of midnight on March 31, 2016.  A simple flag in the parts inventory should be enough to meet this requirement, and should serve as evidence that the part was produced and released by the PAH before that point.

Working Toward MAG rev. 6.

But the core problem remained – the ‘sample supplement’ in the MAG still had language about acceptance of components that was inconsistent with both regulatory requirements and normal industry practice.

We have been working with FAA and EASA personnel to develop new language for the component acceptance section of the ‘sample supplement’ in the MAG.  The authorities have been both responsive and receptive to our proposals to revise the MAG language.

The revision five language included requirements not found in either set of regulations, so we worked with both authorities to develop replacement language that would be published in a MAG rev. 6.  This language is more consistent with regulatory requirements, and it also supports the changes that permit Production Approval Holders to issue their own 8130-3 tags under 14 CFR 21.137(o) [this change was one of the drivers for some of the new requirements].

The draft language would still accept PAH 8130-3 tags that are issued under the new authority, but it would also reopen the standards to permit acceptance of DAR 8130-3 tag, and other forms of FAA-issues 8130-3 tags.  It would also remove unnecessary provisions, like linkage to the OEM IPC, which would only inhibit transactions (reliance on the IPCs would inhibit transactions in third-party approved parts like those produced under TSOA or PMA, and it would also inhibit transaction in replacement OEM parts where the IPC has not yet been updated to reflect the new part number).

Postponement

But getting such a change approved through both authorities takes time.  In order to buy some more time, the FAA plans to postpone by six months the parts receiving inspection provisions of the MAG.  This was announced earlier today in an internal FAA email (as reported by ARSA).  The text of the email reads like this:

From: Logan, Cindy (FAA)
Sent: Friday, April 01, 2016 7:23 AM
To: 9-AWA-AFS-300-Maintenance (FAA)
Subject: FYI from the AFS-300 Management Team — April 1, 2016 >> FAA Notice 8900.336 FAA Form 8130-3 requirements <<

Good Morning Everyone…

This email is provided as interim notification.

Since the release of the Maintenance Annex Guidance (MAG) Change 5,  between the United States and the European Union (EU), many concerns were raised by U.S. repair stations regarding changes contained in Section B, Appendix 1, paragraph 10: “Release and Acceptance of  Components,” and the timelines established.  Industry stakeholders recommended that the MAG be aligned with the changes in part 21 set forth in Amendment 21-98, which became effective on March 29, 2016.  The alignment would allow PAHs in the U.S. to establish a process in their quality systems to issue an authorized release using FAA Form 8130-3 for new parts.  Other concerns include what provisions could be made regarding components received prior to that date.

On November 17, 2015, the FAA issued FAA Notice 8900.336, aligning the requirements of MAG CHG 5, Section B, Appendix 1, paragraph 10, with the effective date of the part 21 Amendment 21-98.  Unfortunately, implementing the changes to part 21 set forth in Amendment 21-98, i.e. 21.137(o) is taking longer than stakeholders expected. Both FAA and EASA were asked by several industry stakeholders to extend the implementation date of MAG CHG 5 requirements specified above (specifically Section B Appendix I, Paragraph 10).

To allow implementation of the privileges under 21.137(o) to the greatest extent possible, FAA and EASA agreed to extend the implementation deadline specified in FAA Notice 8900.336 from April 1, 2016 to October 1, 2016.  All other provisions of MAG CHG 5 remain in effect.

FAA Notice 8900.336 is undergoing revision and will address this change and will be issued as soon as coordination procedures are complete.

This message was sent to Principal Maintenance and Avionics inspectors and Office managers. While our list is extensive it may not touch everyone, please distribute as necessary.

Have a GREAT weekend!

Cindy Logan,
Management and Program Analyst, AFS-310

Stakeholder FeedbackOR AFS300 Group Mailbox >>9-AWA-AFS-300-MAINTENANCE@FAA.GOV

The provision referenced in the email – “Section B Appendix I, Paragraph 10” – is the section of the sample supplement that addresses acceptance of components.  The extra six months of delay will allow the FAA and EASA to publish rev. 6.  It will also allow more production approval holders to start issuing their own 8130-3 tags (a process that is delayed for some production approval holders due to the fact that other trading partners have not yet agreed to accept PAH 8130-3 tags for parts from the United States).

Conclusion

If a repair station tells you that they cannot accept your parts due to new (and unusual-seeming) documentation requirements, then ask them for the source of these requirements.  If the new requirements come from the MAG rev. 5, then it is possible that the new provisions may not be appropriate, and your repair station customer may need to change its receiving inspection criteria back to the pre-MAG requirements due to the facts that (1) MAG rev. 5 acceptance criteria have been tolled until October 1, 2016 and (2) we expect the FAA and EASA to publish MAG rev. 6 that realigns the MAG language with the regulatory requirements of both authorities, and therefore removes some of the unaligned criteria currently found in the sample supplement.  The result should be a sample supplement that achieves the goals of the authorities without imposing undue burden on the industry.

Got more questions?  ASA will have a booth at MRO Americas next week – come and join us for a chat on the trade floor.  We will be in booth 3445.

Leading Zeros in a Serial Number and the FAA Form 8130-3

An ASA member asked whether leading zeros have any meaning in a serial number.

The situation where this question most often arises for members is the situation where the aircraft part is marked with a serial number that has leading zeros, but the FAA Form 8130-3 lists the serial number without the leading zeros.  The serial number is typically listed in block 10 of the form – this can be either a required serial number (e.g. for a critical part required to be serialized under part 45 of the FAA’s regulations – serialization permits tracking of the unique part in order to ascertain life totals relevant to life-limited parts or other time-controlled parts) or a non-required serial number (e.g. a serial number added for the convenience of the manufacturer that was not required by the regulations).

I am not aware of any FAA guidance that specifically addresses this question about leading zeros; however, FAA Order 8130.2D (which has since been superseded) advised that in registry numbers, a leading zero should never be used (so “N1” instead of “N00001”).  This shows an understanding by the FAA that leading zeros occur, and a preference for dropping the unnecessary zeros.

From a practical point of view, there is a general understanding in the industry that leading zeros are not necessary, and add no additional value to the serial number.  This is because they do not change the value of the number.  But that doesn’t mean they aren’t used.  Some of the most famous leading zeros belong to James Bond (“007”).  But we all recognize that his ‘license to kill’ was just the next one issued after license number 6.

Leading zeros are enough of an issue that there are computer programmers who’ve shared methods for removing them (the trick is to account for zero itself, so that you do not leave an empty string).

Nonetheless, there may be practical reasons why a manufacturer might include them in a serial number.  One such reason could be to maintain an efficient tooling mechanism (without the need to insert spaces instead of zeros in order to fill the space in the stamping machine) or to maintain an automatic stamping mechanism with auto-increment (the zeros would be sequenced as part of the auto-increment system).  None of these practical reasons give the leading zeros any special meaning.  They are merely placeholders in each of these scenarios.

There is no reason why the leading zeros would be required on the 8130-3 tag; however a customer may have a particular preference for the leading zeros to be retained.  In such a case, the seller may need to explain to the customer that the leading zeros are mere placeholders.  When designing computer software for aircraft parts inventories, it may be necessary to design the system to recognize that a serial number with leading zeros is the same as the the otherwise-identical number without the zeros; otherwise the system might read the identical serial number as being non-identical (e.g. in a repair station environment, if a part has come into the system more than once for service).

I would be interested in knowing whether any of our members have any different experiences with leading zeros!