What was found
REPAIRED CRACKED CLIP INSIDE EQUIPMENT BAY ON RH SIDE OF CANTED BULKHEAD PER AQRD ERO-988018, REV. IR, TITLED "N317QS- TAILCONE CANTED BULKHEAD RH CLIP CRACKS", DATED APR 06, 2026. F&DT EVALUATION DUE DATE: MAR 31, 2027. NOTE 1: THE FATIGUE AND DAMAGE TOLERANCE (F&DT) EVALUATION REQUIRED PER 14 CFR PART 25, 25.571 IS NOT INCLUDED AS PART OF THIS ENGINEERING DOCUMENT. PER NETJETS AVIATION, INC. GENERAL MAINTENANCE MANUAL CHAPTER 11 - THE F&DT EVALUATION MUST BE COMPLETED WITHIN 12 MONTHS FROM THE DATE OF ISSUE OF THE ASSOCIATED 8110-3. THE AIRCRAFT AT THE TIME OF REPAIR HAD 15,885.4 FLIGHT HOURS AND 10,738 FLIGHT CYCLES. (ALTERNATE TERMINATING ACTIONS TO THE F&DT EVALUATION REQUIREMENT MUST BE SEPARATELY APPROVED AND ARE NOT INCLUDED IN THIS ERO.)