What was found
INSPECTION TYPE: C1, FUSELAGE EXTERIOR SKIN CRACKED .25 INCH LONG AT STA 1734 L16L-L17L. REPAIRED BY INTALLING FINGER DOUBLER AND DOUBLER IAW SRM 53-2-01, 53-02-01 FIG 007 SHEET 5, 51-1-8, 51-1-20, 51-1-20D, 51-1-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE: C1, FUSELAGE EXTERIOR SKIN CRACKED .25 INCH LONG AT STA 1734 L16L-L17L. REPAIRED BY INTALLING FINGER DOUBLER AND DOUBLER IAW SRM 53-2-01, 53-02-01 FIG 007 SHEET 5, 51-1-8, 51-1-20, 51-1-20D, 51-1-21.