As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PIT - DURING Q1 CHECK, FOUND 20 INCH BY 24 INCH AREA OF DISBONDED/HEAT DAMAGE SKIN AT LEFT STUBWING FUSELAGE SKIN BETWEEN FRAMES 24011 AND 24611. CUT OUT AREA OF DISBONDED/HEAT DAMAGED SKIN AND INSTALLED EXTERNAL DOUGLAS PER EA 80083A. (M)