N415PR
Registered owner: DLH N415PR LLC, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Jet Linx Aviation, LLC (9JLA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
8 reports on file, 2013-05-07 – 2021-10-31.
Part: IGNITER BOX — DEFECTIVE (NR 2 ENGINE) · airframe 6,302 hrs · 3,551 cycles
THE FLIGHT CREW REPORTED RECEIVING A "RIGHT FADEC MINOR" MESSAGE. THE MAINTENANCE TEAM DETERMINED THE RIGHT NO2 ENGINE IGNITOR BOX WAS DEFECTIVE. THE UNIT WAS REMOVED AND REPLACED WITH AN OVERHAULED IGNITOR. OPS CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: ACTUATOR — DEFECTIVE (THRUST REVERSER) · airframe 4,489 hrs · 2,470 cycles
THE CREW REPORTED THAT THEY RECEIVED RT THRUST REVERSER FAIL CAS MSG ILLUMINATED DURING LANDING. THE THRUST REVERSER WOULD NOT FULLY DEPLOY. TROUBLESHOOTING FOUND THE RT SECONDARY LATCH ACTUATOR PN 288D0487-511 DEFECTIVE. THE LATCH ACTUATOR WAS REPLACED WITH REPAIRED UNIT. FOUR EACH THRUST REVERSER GUIDE RAIL RODS WERE BENT BECAUSE OF THE FAILURE OF THE SECONDARY LATCH & WERE REPLACED.
Part: SHUTOFF VALVE — FAILED (FUEL SYSTEM) · airframe 4,480 hrs · 2,465 cycles
THE CREW REPORTED THAT DURING PREFLIGHT CHECKS IT WAS DISCOVERED THAT THE LT ENG FIRE SHUTOFF VLV NOT INDICATING CLOSED. THE DEFECTIVE VLV SN 001273 WAS REMOVED FROM SERVICE & AN OVERHAULED UNIT WAS INSTALLED. LEAK & FUNCTIONAL CHECKS WERE SATISFACTORY.
Part: DUCT — CRACKED (LAVATORY) · airframe 4,460 hrs · 2,454 cycles
DURING POST FLIGHT CHECKS, BLUE WATER WAS NOTED DRIPPING FROM ACFT BELLY PANEL. INVESTIGATION FOUND THE LAVATORY WASTE DRAIN DUCT CRACKED INBD OF THE LAVATORY SERVICE PANEL. THE LAVATORY DRAIN DUCT WAS REMOVED & IT WAS NOTED THAT THERE WERE SEVERAL ATTEMPTS TO REPAIR CRACKS IN THE WALL OF DUCT. THE DUCT WAS REPLACED WITH NEW.
Part: CABLE — BROKEN (PAX DOOR) · airframe 4,281 hrs · 2,343 cycles
FLIGHT CREW REPORTED THAT THE MAIN ENTRY DOOR LIFTING SYSTEM WAS INOPERATIVE. TROUBLESHOOTING IDENTIFIED THE DOOR LIFT CABLE BROKE. THE SYSTEM WAS DISABLED WHILE MFG SEARCHED THE WORLD FOR A REPLACMENT CABLE. POOR PARTS SUPPORT, 6 WEEKS FOR REPLACEMENT CABLE TO BE DELIVERED.
Part: REGULATOR VALVE — DEFECTIVE (DEICE PRESSURE) · airframe 4,265 hrs · 2,335 cycles
EICAS DISPLAYED DE-ICE SYS AND DE-ICE SYS ALT, WHEN PNEUMATIC BOOT DEICING SYS WAS SELECTED ON NORM AND ALTERNATE. MX TROUBLESHOOTING IDENTIFIED THE PRESSURE REGULATOR VALVE AS DEFECTIVE. VALVE WAS REMOVED AND REPLACED WITH NEW VALVE. FUNCTIONAL CHECKED SATISFACTORY. ACFT RETURNED TO SERVICE.
Part: SENSOR — DEFECTIVE (APU OIL TEMP) · airframe 4,183 hrs · 2,284 cycles
CREW REPORTED APU HAD AN UNCOMMANDED SHUTDOWN. TROUBLESHOOTING IDENTIFIED THE APU OIL TEMP SENSOR AS DEFECTIVE. A NEW SENSOR WAS INSTALLED, FUNCTIONAL AND LEAK CHECKS WERE SATISFACTORY.
Part: FMS — FAILED (NR 1) · airframe 4,182 hrs · 2,283 cycles
DURING CRUISE, CREW REPORTED THE NR 1 FMS SHUTDOWN, AUTOPILOT DISENGAGED AND VISIBLE SMOKE APPEARED FROM THE LT SIDE OF THE INSTRUMENT PANEL. AFTER EVALUATION, DIVERTED. AN EMERGENCY WAS DECLARED, & LANDED. THE NR 1 FMS WAS FOUND TO BE DEFECTIVE AND WAS REPLACED WITH AN INSPECTED UNIT. OPS CHECKED SATISFACTORY.