The application of more efficient and optimized combustion systems in internal combustion engines generally leads to higher pressure rise rates of the in-cylinder pressure caused by combustion. This for example is the case when gasoline controlled auto-ignition is introduced. The affected engine structure then in turn responds not only with higher amplitude of noise in certain frequency ranges, also the frequency-time structure of the noise changes. One such noise is the so-called 'impulsive noise' that can be perceived from compression ignition (CI) engines, often characterized as 'clatter noise', too. Research for the root cause of impulsive or clattering noise characteristics of the noise of CI engines identified either piston slap noise or shock waves in the connecting rod as the main cause for such noise characteristics. Also the impact of high pressure rise rates on piston slap has been studied. However, this paper shows that the natural frequencies of piston and connecting rod can influence the characteristics of the clattering-noise, too. This was done by carrying out a modal analysis of piston, connecting rod, and the piston -connecting rod assembly. Based on the results gained by the modal analysis of the assembly a simple forced response model was developed. In contrast to current published research into the root cause of the clattering noise characteristics it was demonstrated that the consideration of the piston, pin, and connecting rod assembly leads to another modal behaviour of the system than considering the parts in isolation. Subsequently parametric studies while using cylinder pressure data with constant amplitude but different pressure rise rates were carried out with the forced response model containing the modal data of the assembly. It was revealed that the forced response of the model is influenced significantly by eigenfrequencies of the assembly above a certain pressure rise rate. Finally, structure borne noise measurements under different combustion excitations were carried out. The measurement results, gained under two different combustion excitation modes, showed similar frequency response characteristic of the fired engine under certain pressure rise rates as the model.