N592PH
Registered owner: PHI AVIATION LLC, LA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| PHI Aviation, LLC (HEEA) | 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.
10 reports on file, 2006-04-29 – 2024-06-13.
Part: GENERATOR — INOPERATIVE (APU) · airframe 13,786 hrs
APU FAIL CAUTION IN FLIGHT DURING BEFORE LANDING CHECKS. ATTEMPTS TO RESET THE GENERATOR WERE NOT SUCCESSFUL AND AIRCRAFT WAS RETURNED TO HMA.
Part: GENERATOR — INOPERATIVE (NR 2) · airframe 13,353 hrs
DURING CRUISE, #2 AC GENERATOR FAILED CAUTION ILLUMINATED, AS WELL AS AP#2. EMERGENCY PROCEDURE PERFORMED PER THE CHECKLIST, #2 AC GENERATOR CAME BACK ONLINE. #2 AC GENERATOR CAUTION ILLUMINATED AGAIN, PERFORMED EMERGENCY PROCEDURE ONCE AGAIN. RETURN TO HOUMA.
Part: DETECTOR — INOPERATIVE (ENG OIL TEMP) · airframe 13,176 hrs
DURING CRUISE, #1 ENGINE OIL TEMPERATURE WENT INTO THE YELLOW. RTB VIA OEI PROFILE TERMINATING AT HBP
Part: FIRE DETECTOR — FALSE ACTIVATION (NR 2 NACELLE) · airframe 10,816 hrs
INTERMITTENT ENGINE NR 2 FIRE LIGHT ON CLIMBOUT OFF OF HBP. REPLACED FLAME DETECTOR/HARNESS ASSY.
Part: DETECTION SYS — MALFUNCTIONED (NR 1) · airframe 4,736 hrs
NR 2 ENGINE FIRE LIGHT AND AUDIO CAME ON IN FLIGHT. SECURED ENGINE IN COMPLIANCE WITH EMERGENCY CHECKLIST. WHEN ENGINE LEVER MOVED TO OFF POSITION, LIGHT AND AUDIO WENT OUT WITH NO SECONDARY INDICATIONS. PROCEEDED DESTINATION. NORMAL SINGLE ENGINE LANDING, FIRE EQUIPMENT ON SITE PRIOR TO LANDING. MAINTENANCE REPLACED THE NR 1 ENGINE FORWARD FLAME DETECTOR WIRING HARNESS PN 9255204112041 AND THE FLAME DETECTOR PN 92310-04802-104. NOTE: PREVIOUSLY SUBMITTED ON 6/17/09.
Part: FIRE DETECTOR — INOPERATIVE (NR 2 NACELLE) · airframe 4,460 hrs
NR 2 ENGINE FIRE LIGHT AND AUDIBLE WARNING ON DURING INITIAL TAKEOFF. LANDING UNEVENTFUL. REPLACED OTBD NR 2 ENGINE FIRE DETECTOR.
Part: STRINGER — CRACKED (BS 292) · airframe 2,484 hrs
J-STRINGER FOUND CRACKED ACROSS FWD 5 FASTENERS IN RT CABIN OVERHEAD AT STATION 292, BL 10.5. FIRST FASTENER ON STRINGER ATTACHES TO HAT SECTION SUPPORT FOR TRANSFER MODULE ON ROOF. REMOVED STRINGER, CONTACTED TECH REP FOR MATERIAL SPECS AND PN. ALSO DID NDT ON ROOF. CRS GRANTED PERMISSION TO LOCALLY FABRICATE. STRINGER FOUND NOT TO BE DEBURRED AT ALL FASTENER HOLES.
Part: BYPASS VALVE — INOPERATIVE (MAIN ROTOR) · airframe 2,336 hrs
MGB OIL BYPASS LIGHT CAME ON IN CRUISE FLIGHT. RETURNED TO DEPARTURE. MAINTENANCE REPLACED THE OIL BYPASS VALVE.
Part: FUEL FILTER — UNKNOWN (NR 2 ENGINE) · airframe 1,268 hrs
NR 2 ENGINE FUEL PRESSURE LIGHT INTERMITTENT IN FLIGHT, RETURNED TO DEPARTURE. MAINTENANCE REPLACED THE NR 2 ENGINE FUEL FILTER AND PRESSURE SWITCH 3066T64P01.
Part: BONDING JUMPER — LOOSE (SAS ACTUATOR) · airframe 651 hrs
AFTER DEPARTURE FROM HMA-BP HAD AFCS DEGRADE - AP1 & AP2 FAILED - WOULD NOT RESET. FOUND BONDING JUMPER LOOSE ON PITCH SAS ACTUATOR.