N467PH
Registered owner: PHI HEALTH LLC, LA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| PHI HEALTH,LLC (VE7A) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
REMOVED 1-11-18 DUE TO A CRACKED ON FUEL CONTROL OIL PUMP GEAR SHAFT FORWARD SPLINES. REPLACED GEAR WITH NEW GEAR PART NUMBER M250-10454.
FUEL PRESSURE SWITCH STICKS CLOSED. REPLACED SWITCH.
GYRO PRECESSING. UPON REMOVAL HEARD PART RATTLING INSIDE. REPLACED WITH SERVICEABLE PART.
TAIL ROTOR DISC PACK CRACKED. REPLACED WITH SERVICEABLE PART.
SEAT BELT WORN.
FUSIBLE PLUG BLOWN.
FUSIBLE PLUG LEAKING.
FLOAT BOTTLE DISCHARGED THROUGH FUSIBLE PLUG.
ADI, WILL NOT CAGE WHILE ENERGIZED. REPAIRED.
T/R DRIVESHAFT BEARING ROUGH. REPLACED BEARING 407-040-339-101, S/N ZV15304 DUE TO ROUGH. REPAIRED.
TAIL ROTOR DISC PACK CRACKED.
PAINT PEELING OFF BLADES. REPAIRED.
MAIN ROTOR UNIVERSAL WORN.
BATTERY TEMP CONNECTOR CRACKED. REPAIRED.
BLEED VALVE PRODUCING HIGH TOT. REPLACED.
MAKING BLACK GREASE. REPLACED WITH SERVICEABLE BEARING.
EXCESSIVE CRACKING IN LEXAN SHROUD.
ENGINE OIL TEMP INDICATOR DISPLAYS ERRATIC READINGS.
LIGHTED PANEL ON COLLECTIVE STICK CHIPPED ALONG LOWER EDGE.
TAIL ROTOR DISC PACK PITTING ON DISC.
PA SYSTEM SIREN INOPERATIVE, BURNS FUSE.
HEADLINER CRACKED.
INTERIOR PANEL CRACKED.
MLG HYD SYSTEM LINE HAS CORROSION.
HEADLINER CRACKED.
CABIN TRIM PANEL CRACKED.
AFT CABIN TRIM PANEL CRACKED.
DOOR STRIKER COVER CRACKED.
HAT BIN STRUCTURE CRACKED.
TAIL ROTOR LINK BEARING WORN.
ENGINE BAY DOOR SUPPORT HAS ELONGATED MOUNT HOLE.
ENGINE BAY DOOR SUPPORT BRACE MOUNTING HOLE ELONGATED.
ENGINE BAY DOOR BRACE MOUNTING HOLE ELONGATED.
SPRING ELASTOMER IS DETERIORATED AND TORN.
SPRING ELASTOMER IS DETERIORATED AND TORN.
MAIN ROTOR HEAD LOWER PLATE HAS CORROSION BEYOND LIMITS. CORROSION ON LOWER PLATE NEAR STAINLESS STEEL LOCK PLATE ON RED ARM.
EMERGENCY FLOAT COVER TORN.
SUMP DRAIN VALVE STAYS OPEN.
ENGINE OUTER CLIP RUSTED. SCRAPPED.
FLUCTUATING OIL PRESSURE. REPAIRED.
GYRO CARD ROTATES - WILL NOT STABILIZE. REPAIRED.
BATTERY WEAK AND NEGATIVE PIN CORRODED. REPAIRED.
ENGINE OUTER CLIP RUSTED. SCRAPPED.
ENGINE INNER CLIP RUSTED. SCRAPPED.
WINDSHIELD CRAZED.
WINDSHIELD CRAZED.
CROSSTUBE CORRODED BEYOND LIMITS..
EMERGENCY FLOAT GUARD CRACKED.
EMERGENCY FLOAT GUARD CRACKED.
MAIN ROTOR BLADE TIP AREA CORRODED.
STEP HAS SEVERAL SPOTS OF EXFOLIATION.
LT SKID TUBE DAMAGED BEYOND LIMITS.
EMERGENCY FLOAT COVER TORN.
EMERGENCY FLOAT COVER TORN.
EMERGENCY FLOAT COVER TORN.
COWLING SEAL TORN.
EMERGENCY FLOAT COVER TORN.
MLG BOLT CORRODED BEYOND LIMITS.
DAMAGED AT BUSH AREA. TO BE SENT TO VENDOR.
TAIL BOOM HAS CORROSION AT TOP CAP AND LOWER STRINGER MOUNT AREAS.
ROTOR BRAKE IS DAMAGED AND LEAKS.
FOGGED OVER. CANNOT READ AMOUNT OF PRESSURE IN FLOAT BOTTLE.
NUMBERED DIAL MOVES. UNABLE TO VERIFY EXACT AMOUNT OF PRESSURE IN FLOAT BOTTLE. T
ROTOR BRAKE IS DAMAGED AND LEAKS.
SOLENOID VALVE FOR FLOAT BAG LEAKING.
START LIGHT WILL NOT ILLUMINATE.
WORN ON INNER DIAMETER.
PRESSURE READS LOW.
RUMBLING NOISE AROUND 30 PERCENT N1 DURING START. SENT TO STANDARD AERO FOR EXCHANGE.
RT BOOST PUMP LIGHT DOES NOT ILLUMINATE WITH CIRCUIT BREAKER PULLED. TO BE RETURNED TO VENDOR.
OVERHEATED. TO BE RETURNED TO VENDOR. (J0164213-WA)
ROUGH VIBRATION ON TAILBOOM. TO BE RETURNED TO VENDOR. (J0162310-WA)
DISCOLORATION OF BEARING GREASE. SERIAL NUMBERS REMOVED ARE B01-0810 AND B01-0817.
VIBRATION ON TAILBOOM. BEARING ROUGH. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR#71513300. LABOR CREDIT ACCOMPLISHED ON J0162309-WA (INVOICE AND DMR NO. 687029).
CAUSES FLIGHT TIME MODE OF CLOCK TO NOT WORK.
WORN SPLINES.
WORN SPLINES.
MAKING METAL. SCRAPPED LOCALLY.
INLET CRACKED; WORN.
OIL LEVEL INDICATOR HAZED. SCRAPPED LOCALLY.
FREEWHEEL UNIT SEAL LEAKING.
CARBON SEAL LEAKING.
LINK BOLT FROZEN IN BEARING.
WORN. SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED. REFERENCE: DMR#715175.
FLOAT COVER IS WORN.
NUT PLATES BAD.
TAIL ROTOR HUB BEARINGWORN.
TAIL ROTOR HUB BEARING WORN.
TAIL ROTOR HUB BEARING WORN.
CHIP LIGHT HISTORY, POSSIBLY MAKING METAL.
SHEARED DRIVE SHAFT PIN.
LINK HAD WORN BEARINGS. SERIAL NUMBERS REMOVED ARE NHFS-2385 AND NHFS-2833. REPLACED WITH SERIAL NUMBERS NHFSA-4778 AND NHFSA-4380.
MGT INDICATOR STUCK ON ZERO DURING START-UP FOR 10 TO 15 SECONDS.
COVER WORN/CRACKED.
CREW PANEL DOOR CRACKED AND WORN. PART SCRAPPED.
SEAL LEAKING.
MOUNT RUBBER DEBONDED, OIL FOULED.
MOUNT RUBBER DEBONDED, OIL FOULED.
MAIN ROTOR BLADE CRACKED FORWARD AND AFT OF THE TRIM TAB.
N2 OVERSPEED TO 118.35 PERCENT, UNINITIATED ON GROUND.
N2 OVERSPEED TO 118.35 PERCENT, UNINITIATED ON GROUND. SUBMITTER SUGGESTED POSSIBLE SYSTEM FAILER. S
N2 OVERSPEED TO 118.35 PERCENT, UNINITIATED ON GROUND. SUBMITTER SUGGESTED POSSIBLE SYSTEM FAILER.
CARBON SEAL LEAKING.
PAD ASSEMBLY WORN.
WORN BEARINGS.
TAIL SKID ASSY BROKEN AT BOLT HOLE.
LINK BEARINGS WORN.
BYPASS VALVE INDICATOR BUTTON WEAK.
SWITCH HAD BROKEN CONTACT.
SEAL ASSY LEAKING BETWEEN CARBON RING AND MATING SURFACE.
PIN SLOTS WORN.
PLAY BETWEEN HUB SET AND PIN.
WORN, PLAY IN DRIVE LINK.
EXHAUST STACK CRACKED. REFERENCE: DMR NR 686437.
NP NEEDLE IS INTERMITTENT.
BUSHINGS WORN ON LEVER ASSY. SERIAL NUMBERS REMOVED ARE A-2028 AND A-2037. REFERENCE: DMR NR 686315. REPLACEMENT PART SERIAL NUMBERS ARE A-2636 AND A-2627.
DISC COUPLING CRACKED. REFERENCE: DMR NR 686433.
PIN WORN, PLAY IN DRIVE LINK.
STARTER/GENERATOR'S DATA TAG INCORRECT.
WORN BEARINGS ON HUB.
CARBON SEAL LEAKING.
HMU FAILED DRIVE SHAFT BACKLASH CHECK. REPLACED WITH SERVICEABLE PART.
ENGINE ANTI-ICE ON WARNING LIGHT COMES ON INTERMITTENTLY. REPLACED WITH SERVICEABLE ASSY.
SHAFT SPLINES WORN, EXCEEDING PROPER LIMITS.
DISK COUPLING CRACKED.
ELASTOMER BEARING SEPARATED.
BYPASS BUTTON POPPED.
FAILED 300 HOUR INSPECTION. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES WORN BEYOND LIMITS
T/R PITCH CHANGE CONTROL ROD HAS WORN BEARINGS AND IS BINDING.
INDICATION SHOWS 100 FOOT DIFFERENCE BETWEEN ALTIMETER SETTING AND FIELD ELEVATION.
HIGH OIL TEMP (ENGINE).
OIL COOLER LEAKING.
PRESSURE SWITCH WILL NOT ILLUMINATE LIGHT.
FLOAT COVER HAS TORN END COVERS.
FLOAT COVER TORN.
FLOAT COVER TORN.
LEFT AND RIGHT MIDDLE FLOAT COVERS TORN.
ENGINE OIL COOLER HAS HIGH OIL TEMPERATURE.
SPACERS WORN.
MAIN ROTOR BEARING WORN.
MAIN ROTOR BEARING WORN.
DRIVE PIN WORN.
FADEC FAIL HORN AUDIO EXTREMELY WEAK.
LED LIGHTS ON TRANS. OIL PRESSURE SIDE OF GAUGE INTERMITTENTLY GO OUT. (TEST GOOD, YET WHEN CIRCUIT BREAKER IS PRESSED, PSI SIDE BARS LIGHT UP THEN FADE AWAY).
OIL FILTER BYPASS INDICATED TWO TIMES. SCRAPPED OIL FILTER.
TRANSMISSION PRESSURE LIGHT WILL NOT GO OUT WHEN OIL PRESSURE GOES THROUGH 38 PSI.
RADIO TRANSMISSION WEAK AND DISTORTED.
DISK COUPLING HAS CORROSION.
VOID AT STATION 144 ON UPPER SURFACE.
OIL COOLER CORE LEAKING.
DISK COUPLING CRACKED.
CLOCK WILL NOT MAINTAIN TIME WHEN AIRCRAFT BATTERY IS TURNED OFF.
MAIN ROTOR GEARBOX INDICATOR LIGHT FLICKERS.
BATTERY INDICATOR GAUGE HAS INOPERATIVE LCD SEGMENT ON THE Y10 VOLT NUMBER, LT LOWER VERTICAL LCD SEGMENT.
MLG RELAY STUCK CLOSED.
CRACKED DISC ON T/R DISC COUPLING.
ROUGH BEARINGS. SERIAL NUMBERS REMOVED ARE H96-0267 AND H96-0325.
DISK COUPLING CRACKED.
DISK COUPLING CRACKEDCRACKED.
ENG OIL TEMP WILL NOT ALREADY TEST ON LCD INST. CHECK.
STOP ELASTOMER WORN.
CORROSION BETWEEN DISC.
DISC COUPLING CRACKED.
DISK COUPLING CRACKED.
BEARINGS WORN. SCRAPPED BEARINGS.
FAN SHAFT HAS ROUGH BEARINGS.
NO PRESSURE INDICATION POWER. XMSN OIL TEMP/PRESS
PILOT REPORTED AIRSPEED INDICATOR READS 10 KNOTS LOW, BASED ON GPS READINGS.
DISC COUPLING CRACKED.
DISC COUPLING CORROSION BEYOND LIMITS.
FIN ASSY HAS LOOSE STRINGER.
POSSIBLE SALTWATER INGESTION.