| 摘要 |
A load indicator comprising a probe 18 adapted to be responsive to a load condition and to slide axially within a guide, and an impressionable member 30 which is located to be impacted by the probe when it slides axially so as to record the impact as an impression in its surface for subsequent inspection. The load indicator may be included within an overload detection assembly, and is suitable for use in the landing gear of aircraft.
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