As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LPT REAR FRAME CRACK AT STRUT #16 C1 HAS GROWN TO 1.00" AND NEW CRACK AT STRUT NR 1 C2 MEASURED 0.30" (ENG 01) ENGINE LPT REAR FRAME CRACK AT STRUT #16 C1 HAS GROWN TO 1.00" AND NEW CRACK AT STRUT NR 1 C2 MEASURED 0.30" STURT #16/C1 1.00" STRUT #1/ C2 0.30 COMPLIED WITH EA M-21-172-00812.