What was found
THREE ELONGATED FASTENER HOLES IN FUSELAGE SKIN COMMON TO THE DRAG LINK AT BS 500I+7.5 TO 532.5 ABOVE STRINGER 22 LT. ACCOMPLISHED REPAIR IAW EA B737-53-034624.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THREE ELONGATED FASTENER HOLES IN FUSELAGE SKIN COMMON TO THE DRAG LINK AT BS 500I+7.5 TO 532.5 ABOVE STRINGER 22 LT. ACCOMPLISHED REPAIR IAW EA B737-53-034624.