Actually i have encountered a presentation which may related to this topic. It includes the checks to verify the parts meet design data. Here is the some of it;
"To enable the certifying staff to exercise their responsibilities adequately an effective release to service procedure should include the following checks either directly or by confirming that they have been addressed within the overall business management system.
- That the subject part number(s) is covered by current POA scope
- That the subject part number(s) is covered by a DOA/POA arrangement
- That the subject part number(s) is permitted for direct delivery to end users if applicable Contract / Purchase Order requirements
- That the subject part number(s) are in compliance with the applicable production documents and applicable design data
- That the applicable design data is approved (e.g. via TC/STC/ETSO or minor change) for airworthiness purposes or will be subject to such an approval for conformity purposes
- Completeness of all specified and executed production operations Approval and execution of concessions - those concessions that affect fit, form or function shall be stated in block 13 of the EASA Form 1
- Valid change status (modification, amendment,…)
- That the part (and packaging where applicable) are appropriately identified
- Compliance with applicable airworthiness directives
- Compliance with specified storage terms and conditions (life limited items/time controls are respected)
- Completeness of specified tests and available test records
- Visual inspection for damage, corrosion, leaks, etc. "