As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD PIT R/H TRANSITION PANEL HAS CORROSION FROM STA 500F TO 500L. GROUNDED - YES. REMOVED CORROSION FROM FWD PIT TRANSTION PANEL FROM STA 500F-STA 500L IAW B737-900 SRM 53-00-53-1A-2. ORIGINAL THICKNESS IS 0.040 IAW B737-900 SRM 53-30-53-0I-2. REMOVED 0.040, 0.0 REMAINS. FOUND TO BE OUT OF LIMITS FROM STA500F -STA500I AND STA500J -STA500L FOUND TO BE WITHIN LIMITS IAW B737-900 SRM 53-00-53-1A-2. ALODINED, PRIMED AND INSTALLED REPAIR PARTS IAW B737-900 SRM 53-00-53-2R-5.