Evaluating aircraft structural damage on a physical inspection against a damage map overview.
The location of the damage is the first item to check, this ensures you can pin point the damage and should the reflect accurate location on the aircraft – this should not be a vague zone (exterior fuselage skin between frames 14-15 and stringers L 12 – L 13 is not acceptable) and typical locations could detail Body Station / Frame / Stringer / Buttock Line etc.
The damage should be noted as a specific “type” and typical examples include “Dent”, “Scratch”, “Delamination”, “Gouge”, “Crack” or other such entry entries. This is an important part of the record, as the limits for damage and required actions can differ based on this assessment.