What was found
AT C-CHECK, FUSELAGE SURFACE SKIN REINFORCEMENT ANGLE BROKEN AT STA 970.00 NEAR L-29R11. REMOVED BROKEN REINFORCEMENT ANGLE, FABRICATED NEW ANGLE AND INSTALLED 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 SURFACE SKIN REINFORCEMENT ANGLE BROKEN AT STA 970.00 NEAR L-29R11. REMOVED BROKEN REINFORCEMENT ANGLE, FABRICATED NEW ANGLE AND INSTALLED PER SRM 53-2-0.