What was found
EXTERIOR FUSELAGE HAS TWO SPOTS WITH EXCESSIVE WEAR AT FRAME 34, S43L AND 43R. REPAIRED PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXTERIOR FUSELAGE HAS TWO SPOTS WITH EXCESSIVE WEAR AT FRAME 34, S43L AND 43R. REPAIRED PER SRM.