What was found
DURING A ROUTINE SCHEDULED C2 INSPECTION, STA 1654 HAS 3 FUSELAGE SKIN CRACKS, ADJACENT TO S3 LENGTH 1.125, 2 BETWEEN S4 & S5 LENGTHS .175 AND .075. REPAIRED USING 0.032, 0.040, 0.063 7075 T6 REF SRM 53-80-01, FIG 201, REPAIR 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A ROUTINE SCHEDULED C2 INSPECTION, STA 1654 HAS 3 FUSELAGE SKIN CRACKS, ADJACENT TO S3 LENGTH 1.125, 2 BETWEEN S4 & S5 LENGTHS .175 AND .075. REPAIRED USING 0.032, 0.040, 0.063 7075 T6 REF SRM 53-80-01, FIG 201, REPAIR 4.