What was found
CRACK FRAME 312 BETWEEN S-5L TO S-6L. REPAIRED THE FRAME UPPER CHORD IAW EA M-22-153-01244; DUE TO CRACK EXCEED ALLOWABLE DAMAGE LIMITS OF SRM 53-00-07-1A-1 DETAIL E, CRACK MEASURED L:0.100'.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FRAME 312 BETWEEN S-5L TO S-6L. REPAIRED THE FRAME UPPER CHORD IAW EA M-22-153-01244; DUE TO CRACK EXCEED ALLOWABLE DAMAGE LIMITS OF SRM 53-00-07-1A-1 DETAIL E, CRACK MEASURED L:0.100'.