What was found
PHX - DURING C-CHECK, FUSELAGE FRAME AT FS 218 HAS CORROSION AT LONGERON 30. REPAIRED PER SRM 53-03 FIG 5. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PHX - DURING C-CHECK, FUSELAGE FRAME AT FS 218 HAS CORROSION AT LONGERON 30. REPAIRED PER SRM 53-03 FIG 5. (M)