What was found
CHAFING MARK ON THE INNER FLANGE OF FRAME 38.2 BETWEEN STRG 14-15 LT. REPAIR PERFORMED BY BLEND OUT AND INSTALLING A REPAIR ANGLE AS PER SRM 53-10-13/FIG 202 IAW EA 6-5310-103329 AND RAS/DABRE/7006981/2006 ISS "A".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CHAFING MARK ON THE INNER FLANGE OF FRAME 38.2 BETWEEN STRG 14-15 LT. REPAIR PERFORMED BY BLEND OUT AND INSTALLING A REPAIR ANGLE AS PER SRM 53-10-13/FIG 202 IAW EA 6-5310-103329 AND RAS/DABRE/7006981/2006 ISS "A".