Do your export 8130-3 tags have the right language on them? If they don’t then you run the risk that they may be rejected in Europe.
The Bilateral Aviation Safety Agreement (BASA) between the United States and the European Union specifies that the documentation that accompanies a PMA part bound for the European Union must include specific language in order to be acceptable to the European Union’s airworthiness authority, EASA.
The BASA Technical Implementation Procedures (TIP) direct that PMA parts being exported from the United States to the European Union bear appropriate language in block 12 (the remarks block) of the export 8130-3 tag. In order to meet this requirement properly, the export 8130-3 tag must identify the part as falling into one of these three categories (by using the authorized language):
1. For a PMA part which is not a critical component, the remarks block of the 8130-3 should state:
“This PMA part is not a critical component.”
But if the PMA part is a critical component, then there are two options for the language in the remarks block.
2. In the first option for critical components, if the PMA holder also holds an EASA STC design approval which incorporates the PMA part into an EASA certified or validated product, then the language should say:
“Produced by the holder of the EASA STC number [INSERT THE FULL REFERENCE OF THE EASA STC INCORPORATING THE PMA].”
3. In the second option, if the PMA holder holds a licensing agreement from the TC or STC holder (giving the PMA holder the rights to use the TC/STC design for the PMA parts), then the following statement should be written in the remarks block:
“Produced under licensing agreement from the holder of [INSERT TC or STC NUMBER].”
These options 2 and 3 are the only two options for exporting FAA-PMA critical components from the US to the EU.
The PMA “criticality statement” is something that is requested under the technical implementation procedures (TIPs) that accompany the US-EU bilateral aviation safety agreement (BASA).
Under the US-EU TIP, a “Critical Component” is defined as:
“a part identified as critical by the design approval holder during the product type validation process, or otherwise by the exporting authority. Typically, such components include parts for which a replacement time, inspection interval, or related procedure is specified in the Airworthiness Limitations section or certification maintenance requirements of the manufacturer’s maintenance manual or Instructions for Continued Airworthiness.”
The determination of whether a PMA part is critical is made by the design approval holder (the FAA-PMA holder) and confirmed as part of the FAA approval. Section 4.4(c) of Order 8130.21H states that “The determination of a PMA article’s criticality, as required to be entered in Block 12 when exported, can only be determined by the actual design approval holder (that is, the FAA-PMA holder).” This is important language because certain parties (foreign governments and competitors) have attempted to gainsay the FAA-approved “critical part” decisions of the FAA-PMA holders.
we have heard of DARs who thought that this language meant that only the PMA holder could obtain the export 8130-3 tag. This is not so. This language is not meant to prevent a designee issuing an export 8130-3 tag from making a PMA “criticality statement” on the 8130-3 tag that is consistent with the determination of the design approval holder. Thus, any designee issuing an export 8130-3 tag for any FAA-PMA part may rely on the (PMA) design approval holder’s determination as to whether the PMA part is a critical component.
This critical parts language generally does not appear to apply to most bilateral airworthiness agreements – it is a special nuance of the US-EU Agreement. Adding the “criticality” language does not hurt the 8130-3 tag (and may be useful if the end-user is not yet known), but the criticality language generally remains unnecessary unless the part is destined for Europe.