What was found
FUSELAGE SKIN CRACK AT BS 536 AT STRINGE R15R. VERIFIED CRACK AND CRACK ENDS USING HIGH FREQUENCY EDDY CURRENT. REPAIRED PER SRM 53-30-3 FIG 1. AIRCRAFT RETURNED TO SERVICE. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACK AT BS 536 AT STRINGE R15R. VERIFIED CRACK AND CRACK ENDS USING HIGH FREQUENCY EDDY CURRENT. REPAIRED PER SRM 53-30-3 FIG 1. AIRCRAFT RETURNED TO SERVICE. (M)