<?xml version="1.0" encoding="UTF-8"?><ns2:project xmlns:ns1="http://gtr.rcuk.ac.uk/gtr/api" xmlns:ns2="http://gtr.rcuk.ac.uk/gtr/api/project" xmlns:ns3="http://gtr.rcuk.ac.uk/gtr/api/fund" xmlns:ns4="http://gtr.rcuk.ac.uk/gtr/api/person" xmlns:ns5="http://gtr.rcuk.ac.uk/gtr/api/project/outcome" xmlns:ns6="http://gtr.rcuk.ac.uk/gtr/api/organisation" ns1:created="2026-06-22T07:57:45Z" ns1:href="http://gtr.ukri.org/gtr/api/projects/34134F84-1DC3-4542-909D-4B0BD9DD5F59" ns1:id="34134F84-1DC3-4542-909D-4B0BD9DD5F59"><ns1:links><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/EA957DF8-4FAB-429C-A943-9B6976803C8E" ns1:rel="LEAD_ORG"/><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/EA957DF8-4FAB-429C-A943-9B6976803C8E" ns1:rel="PARTICIPANT_ORG"/><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/E2292F3E-4FDE-4F63-832C-E9BFF3170B6A" ns1:rel="PARTICIPANT_ORG"/><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/6A4FE974-084F-4833-A787-79AB4FE11AE3" ns1:rel="PARTICIPANT_ORG"/><ns1:link ns1:href="http://gtr.ukri.org/gtr/api/organisations/86FAE819-B17F-4FF2-B311-D79728876A1D" ns1:rel="PARTICIPANT_ORG"/><ns1:link ns1:end="2018-08-30T23:00:00Z" ns1:href="http://gtr.ukri.org/gtr/api/funds/D8B06403-8496-4620-968F-D0729A8B7B82" ns1:rel="FUND" ns1:start="2015-12-01T00:00:00Z"/></ns1:links><ns2:identifiers><ns2:identifier ns2:type="RCUK">102376</ns2:identifier></ns2:identifiers><ns2:title>RiviT</ns2:title><ns2:status>Closed</ns2:status><ns2:grantCategory>Collaborative R&amp;D</ns2:grantCategory><ns2:leadFunder>Innovate UK</ns2:leadFunder><ns2:abstractText>RiviT is a collaborative project between leading Aircraft Maintenance Repair &amp;amp; Overhaul companies and NDT equipment specialists to provide a cost-effective solution to investigate the onset of crack propogation at difficult to access doubler repaired aircraft panels. The system will use a niche ultrasonic technique to qualitatively give a rapid indication whether a previously repaired aircraft panel has become defective or not without dissassembly of the entire airframe.</ns2:abstractText></ns2:project>