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8141
In the reading of aircraft blueprints, the term "tolerance", used in association with aircraft parts or components,
| | A) is the tightest permissible fit for proper construction and operation of mating parts. |
| | B) represents the limit of galvanic compatibility between different adjoining material types in aircraft parts. |
| | C) is the difference between extreme permissible dimensions that a part may have and still be acceptable. |
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