What was found
DURING ROUTINE C-CHECK INSPECTION, STA 1342 4H ABOVE ATTACH FITTING, ANGLE IS CRACKED. REMOVED CRACKED ANGLE, FABRICATED REPAIR ANGLE AND SPLICE ANGLE, TREATED, PRIMED AND INSTALLED IAW B727 SRM 51-40-3, 51-10-2 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE C-CHECK INSPECTION, STA 1342 4H ABOVE ATTACH FITTING, ANGLE IS CRACKED. REMOVED CRACKED ANGLE, FABRICATED REPAIR ANGLE AND SPLICE ANGLE, TREATED, PRIMED AND INSTALLED IAW B727 SRM 51-40-3, 51-10-2 AND 51-30-2.