What was found
DURING HMV, A CRACK WAS FOUND ON THE FUSELAGE SKIN AT STA 1640 AT THE UPPER FWD CORNER OF THE OUTFLOW VALVE CUTOUT. THE DAMAGE WAS REPAIRED WITH A REPAIR DOUBLER PER BOEING REPAIR INSTRUCTIONS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV, A CRACK WAS FOUND ON THE FUSELAGE SKIN AT STA 1640 AT THE UPPER FWD CORNER OF THE OUTFLOW VALVE CUTOUT. THE DAMAGE WAS REPAIRED WITH A REPAIR DOUBLER PER BOEING REPAIR INSTRUCTIONS.