What was found
LT FUSELAGE SKIN BETWEEN FRAME 40 AND FRAME 41 AT STRINGER 39 TO STRINGER 40 EXTERNAL SURFACE FOUND WITH SKIN REWORKED. REWORKED AS PER EA 6-5310-149618 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT FUSELAGE SKIN BETWEEN FRAME 40 AND FRAME 41 AT STRINGER 39 TO STRINGER 40 EXTERNAL SURFACE FOUND WITH SKIN REWORKED. REWORKED AS PER EA 6-5310-149618 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.