N152PH
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.
9 reports on file, 2016-01-19 – 2024-06-28.
Part: CONNECTOR — CONTAMINATED (OIL SUMP) · airframe 9,470 hrs
AFTER TAKE-OFF DURING CLIMB OUT MAIN GEAR BOX CHIP SUMP KEEP CAME ON AND OFF NONSTOP. RTB. FOUND OIL & WATER IN SUMP CHIP PLUG CONNECTOR. CLEANED CONNECTOR.
Part: ENGINE — INOPERATIVE (NR 2) · airframe 9,024 hrs · 13,519 cycles
DURING TAKEOFF, BUT PRIOR TO DP, PIC NOTED LARGE TORQUE SPLIT AND#2 ENGINE OPERATING OUT OF LIMITS. ABORTED TAKEOFF.
Part: DAMPER — DEPARTED (TAIL ROTOR) · airframe 8,412 hrs · 12,799 cycles
ON A NORMAL APPROACH TO THE H AT THE NORTH RAMP, AT ABOUT 150 AGL, WE SUDDENLY FELT A STRONG VIBRATION. WE PROCEEDED TO LAND AND SHUT DOWN ON THE H (NO TAXI). POST FLIGHT REVEALED THAT ONE TAIL ROTOR DAMPER DEPARTED THE AIRCRAFT.
Part: MODULE — LEAKING (HYD SYSTEM) · airframe 5,834 hrs
DURING BEFORE LANDING CHECK, MAIN GEAR FAILED TO LOCK DOWN. EMERGENCY PROCEDURE PERFORMED, GEAR LOCKED DOWN WITH BUTTON. NR 2 HYDRAULIC MODULE LEAKING INTERNALLY. MODULE TO BE REPLACED WITH SERVICEABLE.
Part: CONTROL PANEL — ODOR (COCKPIT) · airframe 5,473 hrs
ON SHORT FINAL, A WAFT OF SMOKE ENTERED THE COCKPIT ACCOMPANIED BY ELECTRICAL BURNING SMELL. LIGHT CONTROL PANEL HAS SMOKE SMELL. CONTROL PANEL WILL BE REPLACED.
Part: STRUCTURE — SEPARATED (TAILBOOM) · airframe 4,430 hrs
LEFT SIDE BONDED PANEL SEPERATED ON SIDE SKIN AT BOOM STATION FROM 9970 TO 10.149 ON INSIDE SKIN TWO PLACES BOOM STATION 9817 TO 9868 AND 9970 TO 10.274. REPLACED TAIL STRUCTURE.
Part: STRUCTURE — SEPARATED (TAILBOOM) · airframe 4,430 hrs
SEPERATION INSIDE BOOM IN VERTICAL PYLON AREA BOOM STATION 11,951 TO 12,052. REPLACED WITH NEW TAIL STRUCTURE.
Part: EROSION SHIELD — BROKEN (TAIL ROTOR) · airframe 3,803 hrs
AFTER REVIEW OF HUMS DOWNLOAD, FOUND HIGH TAIL ROTOR AND TAIL ROTOR GEARBOX READINGS. INSPECTED TAIL ROTOR AND FOUND RED TAIL ROTOR BLADE BONDING STRIP BROKEN OFF. REPLACED.
Part: BLADE — DAMAGED (MAIN ROTOR) · airframe 2,484 hrs
AFTER LANDING POST FLIGHT INSPECTION REVEALED DAMAGE TO UNDERSIDE NEAR TIP OF WHITE MAIN ROTOR BLADE. FOUND YELLOW TAIL ROTOR BLADE EROSION SHIELD EXTENSION BROKE OFF AT ATTACHMENT LOCATION.