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During the assembly of Teledyne Continental Motors TSIO-520 M engine s/n 291531R, a number of twelve point nuts (p/n 652541) were found fractured 14 hours after they had been tightened by applying the specified torque (65.8 67.5 ft lbs). The engine assembly process had not been completed.

It was reported that the nuts had been replated with cadmium in accordance with MAF Aviation Services Engineering Order 0071-00 E1. One failed nut and a serviceable nut from the same batch were made available to the ATSB for examination.

Fracture of the failed nut occurred on several longitudinal planes. Fracture initiated from regions of intergranular cracking in the increased section created by the nut flange. Final fracture occurred in a ductile manner.

These features are typical of hydrogen-induced delayed cracking (hydrogen embrittlement), a condition resulting from the presence of hydrogen in the steel and a sustained tensile stress. The effect of thread shape creates a sustained tensile hoop (circumferential) stress in a tightened nut. A particular hazard of cadmium plating high strength steels is the absorption of hydrogen into the base metal. This hazard is countered by baking the parts after plating.

In order to prevent recurrence it is necessary to establish:

  • If the hydrogen-removal baking heat treatment had been applied to the nuts.
  • If the baking process was controlled in accordance with process specifications. For example was the temperature distribution throughout the batch uniform, and was the time of exposure to the specified temperature the same for all nuts in the batch.
  • If the engineering work order had taken into consideration that the twelve-point nuts are heat treated to a higher strength than the six-point nuts they replace. Longer baking periods may be required to eliminate the hazard of hydrogen embrittlement in higher strength steels.

 

 

R20040054

The ATSB recommends that the Civil Aviation Safety Authority review MAF Aviation Services Engineering Order 0071-001 E1 and the cadmium plating and baking process controls employed by the plating subcontractor to determine if the process and process controls prevent the occurrence of hydrogen-induced delayed cracking in high-strength steel engine through-bolt nuts.

FIGURE 1: Fractured nut as received with an intact nut for comparison. FIGURE 2: Fracture surface showing the brittle cracking region in the centre of the photograph and the surrounding ductile fracture features
FIGURE 1: Fractured nut as received with an intact nut for comparison. FIGURE 2: Fracture surface showing the brittle cracking region in the centre of the photograph and the surrounding ductile fracture features.
FIGURE 3,4: Scanning electron micrographs of the brittle cracking region. FIGURE 3,4: Scanning electron micrographs of the brittle cracking region.
FIGURE 3,4: Scanning electron micrographs of the brittle cracking region.
figure 5 Scanning electron micrographs showing the features of the ductile fracture region figure 6 Scanning electron micrographs showing the features of the ductile fracture region
FIGURE 5,6: Scanning electron micrographs showing the features of the ductile fracture region.

1 Pratt & Whitney Canada Engine/Component Investigation Report, Report No. TO28252.

 
General details
Date: 01 February 2004 Investigation status: Completed 
  
 Investigation type: Occurrence Investigation 
 Occurrence type: Miscellaneous - Other 
Release date: 01 February 2005 Occurrence class: Operational 
Report status: Final Occurrence category: Technical Analysis 
 
 
 
 
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Last update 13 May 2014