5.1 Fatigue design condition as described in section
4.18.2 of this Code shall be complied with as applicable depending
on the cargo containment system concept. Fatigue analysis is required
for the cargo containment system designed under section 4.27 of this
Code and this standard.
5.2 The load factors for FLS shall be taken as
1.0 for all load categories.
5.3 Consequence class factor γC
and
resistance factor γR
shall be taken as
1.0.
5.4 Fatigue damage shall be calculated as described
in sections 4.18.2.2 to 4.18.2.5 of this Code. The calculated cumulative
fatigue damage ratio for the cargo containment systems shall be less
than or equal to the values given in table 3.
Table 3 Maximum allowable
cumulative fatigue damage ratio
|
|
Consequence class
|
|
Cw
|
Low
|
Medium
|
High
|
|
|
1.0
|
0.5
|
0.5footnote
|
5.5 Lower values may be fixed by the Administration
or recognized organization acting on its behalf, for example for tank
structures where effective detection of defect or crack cannot be
assured, and for ships carrying more hazardous cargo.
5.6 Crack propagation analyses are required in
accordance with sections 4.18.2.6 to 4.18.2.9 of this Code. The analysis
shall be carried out in accordance with methods laid down in a standard
recognized by the Administration or recognized organization acting
on its behalf.