What was found
DURING CHECK-C MAINT THE LEFT SIDE MOST FORWARD CABIN DOOR JAMB, 2 ANGLES HAD CORROSION AT STA 180 TO 200. FABRICATED AND INSTALLED PER SRM 1-10-02, 1-10-03, 51-30-02, 51-14-01, AND SPM 6-10-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT THE LEFT SIDE MOST FORWARD CABIN DOOR JAMB, 2 ANGLES HAD CORROSION AT STA 180 TO 200. FABRICATED AND INSTALLED PER SRM 1-10-02, 1-10-03, 51-30-02, 51-14-01, AND SPM 6-10-01.