What was found
CORROSION AT STRG 50, BETWEEN FRAME 39-43 RT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRINCIPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION AT STRG 50, BETWEEN FRAME 39-43 RT. REMAINING THICKNESS OUT OF LIMIT. STRINGER REPAIR PERFORMED WITH PRINCIPLE DESCRIBED IN SRM 53-10-14/FIG 201A, APPROVED BY EA 6-5315-103260 AND RAS/046453/012/2006 ISS "A".