What was found
CRACK ON INNER FUSELAGE SKIN AT BS 1414 BETWEEN LONGERONS 1 AND 2LT IN AFT ACCESSORY COMPARTMENT. CRACK WAS CUTTING OUT IAW SRM 53-04, FIG 23 AND REPAIRED IAW SRM 53-04, FIG 23. 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON INNER FUSELAGE SKIN AT BS 1414 BETWEEN LONGERONS 1 AND 2LT IN AFT ACCESSORY COMPARTMENT. CRACK WAS CUTTING OUT IAW SRM 53-04, FIG 23 AND REPAIRED IAW SRM 53-04, FIG 23. 3.