Proposed CM-S-005

Bonded Repair Size Limits in accordance with CS 2x.603 and AMC 20-29

This CM includes  harmonised content, as agreed  with FAA, and has been released for comment in parallel with the equivalent FAA document.
Notes: Although the policy and supporting content is similar in intent, some differences exist in the supporting content throughout the documents due differences between EASA and FAA document formats and processes.

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