If i read correctly, the general notes are not aircraft specific? They also seem to be regarding the airframe rather than the engine, talking about flight handling and g pressure rather than aircraft specific engine limits. Part i) of the introduction looks at the airframe and structural failure, not engine failure. The entirety of part 1, other than flying methods to increase range, is discussing general flying techniques not engine management. The introduction to which this balancing of risk refers is to part 1- 'flying limitations' which discusses g force, trimming the aircraft etc. It is not in reference to part 2, look at the contents and you can see this!
It is in the regards of flying limitations, not engine limitations which is in a different section of the document!
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