What was found
R/W I/B FIXED L/E UPPER SKIN ANGLE FASTENER HOLE IS CRACKED AT KRAS 221<[01] REMOVED AND REPLACED ANGLE IAW SRM 51-40-02-0G-0 AND DWG. 116A4008.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
R/W I/B FIXED L/E UPPER SKIN ANGLE FASTENER HOLE IS CRACKED AT KRAS 221<[01] REMOVED AND REPLACED ANGLE IAW SRM 51-40-02-0G-0 AND DWG. 116A4008.