As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TORN KEVLAR CABLE OF SLIDE RELEASE MECHANISM INSIDE TAILCONE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00138: KEVLAR CABLE OF RELEASE MECHANISM INSIDE TAILCONE WAS REPLACED PER B717-200 AMM 53-52-01. (LP #2950442)