What was found
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE IAW SRM 51-40-02 ;SRM 51-10-02 PARAGRAPH 9 ;DWG 143A5400 SHEET:140 AND SHEET:184 REV:-
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE IAW SRM 51-40-02 ;SRM 51-10-02 PARAGRAPH 9 ;DWG 143A5400 SHEET:140 AND SHEET:184 REV:-