What was found
BULGE BY 1.0 X 0.8 X 0.025" ON EXTERNAL FUSELAGE SKIN BS 320-340 ABOVE S-39R (BULGE FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1A.)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
BULGE BY 1.0 X 0.8 X 0.025" ON EXTERNAL FUSELAGE SKIN BS 320-340 ABOVE S-39R (BULGE FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1A.)