1.1.1 The
                                 Total Load Assessment, TLA, procedure is an optional
                                 procedure that is applied on a voluntary basis when an Owner or designer
                                 who seeks to increase confidence levels in the structural integrity
                                 of a ship. The TLA procedure is illustrated in Figure 3.1.1 Overview of the Total Load Assessment, TLA Procedure
                                 
                              
                              
                              
                              
                              
                                 
                                 
                                 
                                 Figure 3.1.1 Overview of the Total Load Assessment, TLA Procedure
                               
                              
                              
                            
                           
                           
                           
                           
                              
                              
                              1.1.2 The TLA procedure is based on the following concepts:
                                 
                              
                              
                              
                              
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Derive the total
                                       design loads acting on each structural member.
                                    
                                    
                                    
                                  
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Derive the structural
                                       resistance of each structural member.
                                    
                                    
                                    
                                  
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Derive the load
                                       utilisation factors.
                                    
                                    
                                    
                                  
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Ensure the load
                                       utilisation factors are less than the required design factors.
                                    
                                    
                                    
                                  
                              
                              
                              
                            
                           
                           
                           
                              
                              
                              1.1.3 This
                                 Chapter gives the simplified stress analysis methods to be used for
                                 the TLA procedure. Direct calculations or alternative
                                 proven methods of analysis which are more rigorous will be accepted.
                                 
                              
                              
                              
                            
                           
                           
                           
                           
                           
                           
                           
                           
                           
                              
                              
                              1.1.6 The
                                 simplified stress analysis techniques predict the total stresses acting
                                 in the structure as a consequence of the total loads. These techniques
                                 cover the assessment of stresses in the following:
                              
                              
                              
                              
                                 - Primary structure.
 
                                 - Primary/secondary plating systems.
 
                                 - Grillage plating systems.
 
                              
                              
                              
                            
                           
                           
                           
                              
                              
                              1.1.7 The
                                 resulting stresses are then checked against a set of design factors,
                                 which include stress, deflection and buckling requirements.