What was found
FRAME IS CRACKED AT CEILING SUPPORT CHANNEL ATTACH POINT BS 1070, RBL 33.5, WL 294. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-4 FIG 2 & EA 7-5310-56293.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FRAME IS CRACKED AT CEILING SUPPORT CHANNEL ATTACH POINT BS 1070, RBL 33.5, WL 294. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-4 FIG 2 & EA 7-5310-56293.