What was found
CRACKS ON EXTERNAL SKIN CUTOUT OF OUTFLOW VALVE LOCATED BS 360+19" AND BL 0. REPAIRED SKIN BETWEEN BS 360 AND BS 403 FROM S-26L TO S-26R IAW EA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKS ON EXTERNAL SKIN CUTOUT OF OUTFLOW VALVE LOCATED BS 360+19" AND BL 0. REPAIRED SKIN BETWEEN BS 360 AND BS 403 FROM S-26L TO S-26R IAW EA.