What was found
DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN IN STA Y=1099 TO 1105 BETWEEN LONGERON 29RT AND 29LT AT AFT CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN IN STA Y=1099 TO 1105 BETWEEN LONGERON 29RT AND 29LT AT AFT CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.