As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TAIL-CONE RELEASE SYSTEM. FAILED STEP 2.G.(5). CLAMP (ITEM 28) TO CONDUIT (ITEM 29) CLEARANCE WAS BELOW 0.5 IN. WITH LATCH LEVERS IN FULL OPEN POSITION. TASK CARD 5352-2001, FIG. 5, SHEET 4. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE ADJUSTED LOCK CABLE CLAMP TO BE WITHIN CLEARANCE LIMIT OF THE CONDUIT AS PER B717 AMM 53-52-01 STEP E(1)(J) FIG 504. (LP #1855352)