What was found
TWO CRACKS ON INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE. THE ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TWO CRACKS ON INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE. THE ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01.