Failure analysis is the process of collecting and analyzing data to determine the cause of a failure. It is an important discipline in many branches of manufacturing industry, such as the electronics industry, where it is a vital tool used in the development of new products and for the improvement of existing products.

Fatigue Failure

It relies on collecting failed components for subsequent examination of the cause or causes of failure using a wide array of methods, especially microscopy and spectroscopy. The NDT or nondestructive testing methods are valuable because the failed products are unaffected by analysis, so inspection always starts using these methods.

Failure analysis and prevention are important functions to all of the engineering disciplines. The materials engineer often plays a lead role in the analysis of failures, whether a component or product fails in service or if failure occurs in manufacturing or during production processing. In any case, one must determine the cause of failure to prevent future occurrence, and/or to improve the performance of the device, component or structure.

Rupture Failure

A failure analysis engineer often plays a lead role in the analysis of failures, whether a component or product fails in service or if failure occurs in manufacturing or during production processing. In any case, one must determine the cause of failure to prevent future occurrence, and/or to improve the performance of the device, component or structure.

Methods of analysis :

  • Sample Preparation
  • Spectroscopic Analysis
  • Microscopes and Surface Analysis
  • Chemical Verification
  • Coating Contamination
  • Corrosion Analysis
  • Fiber Identification
  • Fractography
  • Macro Etching
  • Microstructure Evaluation
  • Photo Documentation
  • Physical TestingScanning Electron Microscopy (SEM) and EDS
  • Surface Contamination
  • Weld Evaluation
  • Laser Signal Injection Microscopy
  • Semiconductor Probing
Stress Corrosion Cracking

Case Study : Crane Bolt Failure


One of two bolts supporting a load of 16 200 lbs failed while in service causing eight hours of downtime on an essential machine to production. The bolts were in operation on a crane used to transfer anodes into the machine. Figure 1.1 shows a drawing of the set-up and the location of fraction Just above the nut. The crane cycled 600 time a day 7 days a week.

Figure 1.1. Drawing of the bolt and crane set-up.

Figure 1.2. Photograph of broken bolt

Figure 1.3. Photograph of fracture surface.

The broken bolt (Figure 1.2) and a new unused bolt, recommended by the supplier for the application, were supplied to conduct the investigation. The original designers of the crane specified a bolt that conforms to SAE standards grade 5. The supplier of the new bolt confirmed that it was made to conform with ASTM standard A 193 grade B7.


Observations Examination of the fracture surface revealed characteristics such as a beachmarks associated with fatigue (Figure 1.3). The zone of final fracture was located between two areas of fatigue propagation suggesting the presence of bending forces. The surface area of final fracture was approximately 12% of the total fracture surface suggesting that the bolt was not overloaded. Cracks where also found between threads near the fracture surface indicating that the bolt was highly susceptible to fatigue initiation.

Results from chemical analyses (Table 1.1) show that the original broken bolt had a carbon content slightly below those required by the SAE standards for a grade 5 bolt. This lower carbon content would have acted to decrease the material properties. The chemical composition of the new sample bolt conformed to the ASTM standard A193/A grade B7 that requires an AISI-SAE 4140 composition.

Figure 1.4. Micrograph of flaking found at the base of a thread in the fractured bolt. 2% nital 100X

Microscopic examination of the bolts where done using longitudinal and latitudinal mounts for each. The sections taken from the fractured bolt were taken close to the fracture surface. Examination before etching of the two bolts showed no cracking or unusually large inclusions. The original broken bolt did show some flaking at the base of the threads (Figure 1.4) but this is expected for a bolt that has been in service. Etching the sections revealed a microstructure of coarse pearlite in a matrix of ferrite (Figure 1.5).

Figure 1.5. Micrograph of fractured bolt. Ferrite matrix with pearlite. 2% nital 200X

The SAE grade 5 standard requires that the bolt be quenched and tempered to conform and therefore should have a tempered martensite structure. Martensite has higher material properties such as yield strength and hardness, which increases its resistance to fatigue initiation. The ferrite matrix of the original bolt has low yield strength, which in turn reduces its resistance to fatigue initiation.

Figure 1.6. Micrograph of new bolt. Tempered martensite. 2% nital 500X

The new bolt was found to be quenched and tempered as required by the ASTM standard (Figure 1.6). However rolling seems where found at the tips of the treads (Figure 1.7). This is not a serious defect because of the defects location in a low stress area however, if the bolt was placed in a corrosive atmosphere these seams would corrode and then act as fatigue initiation sites.

Figure 1.7. Micrograph of the new bolt thread showing a rolling seam. 2% nital 200X

Tensile tests were done on the bolts to test their material properties in comparison with the standards. The results (Table 1.2) show that the yield strength and ultimate tensile strength of the original bolt are only two thirds that required by the standards. This conforms to the microstructural observations. The properties of the new bolt conformed to the standard even though they were slightly elevated.

Conclusions and Recommendations :

Examination revealed that the bolt failed as a result of high cycle low load fatigue. Chemical analysis and tensile tests confirmed that the bolt did not meet the SAE grade 5 standards required by the original design of the crane. The major cause for this lack of conformity is because the bolt was not quenched and tempered. Since the resistance of steel to fatigue initiation in proportional to its yield strength, the low properties of the steel in this case left it open to fatigue initiation.

Examination of the new bolt revealed that it conformed with the ASTM standards A 193 for a grade B7 bolt, as the supplier specified. However, rolling seams were found in the thread tips. Due to the relatively low loads this area is subjected to this is not a major problem but if the bolt is subjected to a corrosive environments these seams could grow and become fatigue initiation sites. The SAE grade 5 bolt specified by the original designers should continue to be used in future and the upgrade to the ASTM B7 is unnecessary.

References :



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