Gas turbine engine cross-section with magnifying glass and text

Aircraft engine maintenance demand is rising, but capacity isn’t keeping pace.

As Aviation Week reported in January 2026, a combination of factors, including durability challenges in newer engine programs, continued operation of aging fleets, and increasing overhaul volumes, is putting pressure on maintenance, repair, and overhaul (MRO) facilities.

The result is more engines moving through inspection cycles with less time available per inspection.

This increasing pressure is not affecting all parts of the workflow equally. It is concentrated in inspection, where time, visibility, and coverage requirements must all be met before repair can proceed.

Where the Bottleneck Emerges

Inspection occurs between disassembly (if required) and repair, directly determining the next steps.

As volumes increase, it can become the limiting step, especially for:

  • Turbine shafts, drums, and spools
  • Combustion and hot section components
  • Internal passages and restricted geometries
  • Surface flaw detection using FPI and MPI
Gas turbine engine on wing with panels open and picture-in-picture of trubine cross-section

Image: an on-wing, partially-disassembled gas turbine engine.

These inspections require complete coverage, controlled viewing, and documented indications, even as time per inspection decreases.

Why Inspection Slows Down

Inspection bottlenecks tend to be less procedural, but more maneuverability, access, and visibility limitations:

  • Complex internal geometries with inconsistent viewing angles
  • Limited access to internal surfaces & components
  • Difficulty distinguishing true indications
  • Friction in capturing and documenting results
Cross-section of a gas turbine engine

Image: a cross-section of a gas turbofan engine

 

At larger sizes and higher volumes, these inefficiencies compound and begin to constrain MRO throughput.

 


UV-Based Inspection: Still Essential, Now Under Pressure

Fluorescent penetrant inspection (FPI) and magnetic particle inspection (MPI) remain foundational methods for detecting surface-breaking defects. In these processes, a fluorescent dye is applied to the surface, where it collects in indications such as small cracks or pitting. After excess dye is removed, any remaining material trapped in these areas emits a bright green glow under ultraviolet light.

UV-based imaging enables inspectors to:

  • Detect fine cracks and discontinuities
  • Differentiate indications from background noise
  • Maintain repeatability and consistency across inspection cycles
The SeeUV Shaft and Coupler Inspection System going into a gas turbine engine shaft

Image: The SeeUV® Shaft and Coupler Inspection System (SCIS) fluorescing UV penetrant dye inside the shaft.

 

The requirement is no longer just detection. It is a repeatable, documented detection performed efficiently.

 

Two Inspection Realities

Large Components: Coverage and Repeatability

For shafts and spools, the challenge is complete and verifiable coverage.

SeeUV® large component systems support this by combining:

  • UV and white light illumination
  • Camera-based visualization
  • Controlled positioning for repeatable inspection paths

The objective is to ensure every required surface is inspected consistently and can be verified.

Internal Areas: Access and Visibility

For turbine sections and internal passages, the primary constraint is access. UV video borescopes from Yateks and iShot® Imaging extend inspection into confined areas by delivering:

  • Direct UV illumination at the inspection surface
  • Clear visualization within restricted geometries
  • Durable and maneuverable scope tips
iShot Model E and Yateks P+ UV Video Boresopes with UV illumiation graphic

Yateks P+ Video Borescopes and iShot® Model E UV Video Borescopes, both with UV LEDs.

 

The Converging Requirement

Across both inspection types, the requirement is consistent: increase inspection throughput without reducing inspection quality.

This includes reducing setup and repositioning time, improving the clarity of indication detection, standardizing inspection workflows, and supporting reliable documentation and traceability.

Inspection is no longer just a step in the process. It directly influences overall MRO throughput.

 

SeeUV® in Engine Inspection Workflows

Within aircraft engine MRO environments, SeeUV® systems are used to address complementary inspection needs.

Large Component Inspection

  • Shafts, drums, and structural assemblies
  • Controlled, repeatable coverage
SeeUV WebViewer extended into a spool cross-section with picture-in-picture of drawing of same

Image: The SeeUV® WebViewer® Camera Inspection System extended in a spool cross-section with a 0-degree, or direct view, lens. The smaller image within is a drawing representation of a spool being inspected.

Internal Inspection

  • Turbine and combustion sections
  • UV borescopes for confined access

Together, these approaches address both coverage and access constraints across engine inspection workflows.

 

 


See It at MRO Americas 2026

InterTest will be exhibiting:

Front of conference center in Orlando, FL with palm tree

InterTest at MRO Americas, Orlando, FL
April 21–23, 2026

Focused on enabling inspectors to see clearly, cover completely, and document reliably across aircraft engine inspection workflows.