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.

Back to topBack to topBack to top