As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING RE- INSPECTION FOUND A TOTAL OF 32 LOOSE/ PULLED FASTENERS. OUT OF LIMITS PER SRM 54-10-01-1A-2.<[01] REMOVED AND REPLACED #1 ENGINE INLET COWL IAW AMM 71-11-01; REF. 71-11-01-JIC TTG8Q00P2JNU ACOUSTIC PANEL AREA LOSS IS LESS THAN 1.