FAA Aviation Mechanic Powerplant (AMP)Engine InspectionHard

During overhaul, a turbine engine disk is inspected using fluorescent penetrant inspection (FPI), and a linear indication is found at a bolt hole in the disk rim. Why is this finding treated with particular concern compared to a similar indication on a non-rotating case component?

  1. ADisks are inexpensive to replace, so any indication automatically results in scrapping the part
  2. BFPI indications on rotating parts are always false positives due to residual magnetism
  3. CThe disk is a life-limited rotating part subject to high centrifugal stress, and a crack can lead to catastrophic uncontained failure
  4. DThe disk material does not respond well to FPI, making the indication unreliable
Show answer & explanation

Correct answer: C. The disk is a life-limited rotating part subject to high centrifugal stress, and a crack can lead to catastrophic uncontained failure

Turbine disks are life-limited rotating components that experience very high centrifugal stress in service; a crack propagating from a stress riser such as a bolt hole can lead to sudden, uncontained disk failure, which is far more catastrophic than a crack in a static case. For this reason, any crack indication in a disk is treated as unacceptable and the part is rejected, unlike some allowable indications on static structure.

Why the other options are wrong

  • A. Cost is not the reason for rejection; the safety-critical rotating nature of the part is.
  • B. FPI is a dye penetrant method, not affected by magnetism; magnetic particle inspection is the one affected by residual magnetism.
  • D. FPI is a standard and reliable method for detecting surface cracks in turbine disk materials.

Turbine Disk FPI Crack Indication

Fluorescent penetrant inspection is used to detect surface cracks in turbine disks; any crack indication in a rotating, life-limited disk is cause for rejection due to the risk of uncontained failure.

  • Disks are life-limited rotating parts subject to high centrifugal stress
  • Bolt holes and rim areas are common crack initiation (stress riser) sites
  • Uncontained disk failure can penetrate the engine case and aircraft structure

Memory trick: A cracked disk is a bomb spinning at thousands of RPM

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