What was found
AT C-CHECK, FUSELAGE EXTERIOR ACCESS DOOR CORNER CRACKED 4 INCHES AT FS 37, AT L-39 AND L-40. INSTALLED DOUBLER PER SRM 53-2-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, FUSELAGE EXTERIOR ACCESS DOOR CORNER CRACKED 4 INCHES AT FS 37, AT L-39 AND L-40. INSTALLED DOUBLER PER SRM 53-2-0.