API 571 Clause 4.2. 16
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At openings only
At notches or stress raisers
Underneath reinforcement pads only
None of the above
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Coarse grained microstructures - finer grained
Medium grained microstructures - coarse grained
Finer grained microstructures - coarse grained
All of the above
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Large bore piping systems
Coker drumÂ
High pressure drop control valves
Small bore piping systems
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SWUT, RT and MT
PT, MT and SWUT
RT, PT and MT
None of the above
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Carbon steels
Stainless steels
Low alloy steels
All of the above
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Higher than average stresses at high temperatures
Constant stresses occurring at low temperatures
Cyclic operating conditions of bird poop then rain, bird poop then rain, etc.
Cyclic stresses occurring over a long period of time.
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Transition limit.
Endurance limit.
Hardening limit.
Speed limit.
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Only carbon steel
Only carbon steel, and high nickel alloys
Only carbon steel and chromes
All materials
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Low temperature
High Temperature
Not a factor
None of the above
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Dirty Steel
Clean Steel
Not a factor
None of the above
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Smooth surface
Notches
Not a factor
None of the above
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Non-normalized carbon steel
Normalized carbon steel
Stainless Steel
Titanium
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10-20% of a material’s ultimate tensile strength
10-20% of a material’s yield strength
40-50% of a material’s yield strength
40-50% of a material’s ultimate tensile strength
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The cracks are extremely tight
Predicting the location of cracking is difficult
Once the crack begins, only a few cycles are needed for the crack to lead to failure
Often the equipment is vibrating making non-destructive evaluations difficult
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Clam shell appearance
Snail shell appearance
Turtle shell appearance
None of the above
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Minimize grinding marks, nicks and gouges on the surface of components
Insure good fit up and smooth transitions for welds
Remove any burrs or lips caused by machining
Avoid placement of welds in areas of high stress or locations with known cyclic stresses.
All the above
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Material properties (Strength, Hardness, microstructure)
Shear wave frequency
Stress level
Geometry
Corrosion fatigue
Vibration Induced Fatigue
Thermal Fatigue
Frequency stress fatigue
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Single clam shell fingerprint with vertical straight lines directly below the crack initiation site
Single clam shell fingerprint with rings called beach marks coming from a crack initiation site
Concentric lines throughout the entire cross-sectional area
None of these are correct
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Material
Design
Operation
Time
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Within the elastic limit of the material
Above the elastic limit of a material
Well below the yield strength of the material
Stress is not a factor
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True
False
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Aluminium
300 series SS
400 series SS
None of the above
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50-100 cycles
100-105 cycles
106 to 107 cycles
104-105 cycles
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Cracks nucleating from a surface stress concentration
Microstructure of a material
All of the above
None of the above
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Single "calm shell" fingerprints
Multiple "calm shell" fingerprints
All of the above
None of the above
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