N404PH
Registered owner: PHI HEALTH LLC, AZ (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
NR 5 BEARING SPALLING ON OUTER RACE SPLIT. INSTALLED A NEW BEARING.
ENGINE REMOVED 6-30-15 DUE TO METAL IN OIL. FOUND SPALLING AT OUTER RACE SPLIT & WORN POCKET AT SEPARATOR ON NR 5 BEARING. INSTALLED NEW NR 5 BEARING. PART WILL BE RETURNED FOR FURTHER EVALUATION.
ENGINE WAS REMOVED 10-24-14 DUE TO METAL IN OIL. NR 5 BEARING EXHIBITED HEAVY SPALLING ON BALLS. PART WILL BE RETURNED TO MFG FOR FURTHER EVALUATION.
LONGERON CRACKED IN HALF AT JUNCTION OF BULKHEAD FWD OF FUSELAGE TAILBOOM RING. REMOVED DAMAGED LONGERON AND REPLACED WITH NEW LONGERON USING 206-031-314-219B.
UNABLE TO BALANCE. REPLACED BEARING 407-340-339-107, S/N ZV16525 DUE TO SCRAPPED WITH HANGER; AFT HOUSING 407-040-322-101, S/N 74613-130 DUE TO BOLT BORE WORN OUT. REPAIRED.
PIN WORN AND STUCK IN GIMBAL RING. REPLACED WITH SERVICEABLE PART.
MAIN ROTOR HEAD BUSHING SET WORN. REPLACED WITH SERVICEABLE PART.
GIMBAL RING WORN. REPLACED WITH SERVICEABLE PART.
ROTOR HORN RELAY STICKING.
LEAKING AT INTERCONNECT FITTING.
MAIN ROTOR UNIVERSAL WORN.
CYCLIC SERVO HAS A WORN BEARING. TO BE SENT TO MFG FOR CREDIT.
TAIL ROTOR SHAFT HAS WORN BEARINGS. REPLACED WITH SERVICEABLE BEARINGS. REPAIRED.
RT AFT CROSSTUBE FITTING DAMAGED WHEN CROSSTUBE SHIFTED. REPLACED FITTING.
STRAP DAMAGED WHEN CROSSTUBE SHIFTED. REPLACED STRAP.
AFT CROSSTUBE SLIPPED IN FITTING, CAUSING DAMAGE TO FITTING, STRAP AND CROSSTUBE. REPLACED FITTING.
RT AFT CROSSTUBE STRAP DAMAGED WHEN CROSSTUBE SHIFTED. REPLACED STRAP.
AFT CROSSTUBE SLIPPED IN FITTING CAUSING DAMAGE TO FITTING.
NO AUTO RELIGHT AND NO IGNITER ON START. CONTACTOR FAILED.
LINE LEAKING THROUGH WALL. TO BE SENT TO VENDOR.
UNABLE TO BALANCE NR 2 BLOWER ASSY SHAFT. REPAIRED.
MGT INDICATOR RANGE BAR FLASHES ON START UP.
TAIL ROTOR DISC PACK CRACKED.
INTERMITTENTLY PILOT UNABLE TO TRANSMIT TO PASSENGERS. FOUND METAL SHAVINGS INSIDE UNIT, BOTH RX KNOBS AND ICS KNOB BAD. REPLACED AND CLEANED METAL SHAVINGS FROM INSIDE UNIT. BENCH CHECK GOOD.
DISPLAY IMAGE BOUNCES AND INTERMITTENTLY DISAPPEARS. IN SHOP REPAIR.
LT PASSENGER DOOR STRUT LOWER BRACKET CRACKED. SCRAPPED.
SWITCH STICKS, NO PRESS LIGHT ON SHUTDOWN.
LOW FUEL WARNING LIGHT ON WITH 300 LBS OF FUEL ABOARD.
FLOAT BAG FAILED 6 MONTH INSPECTION (LEAKING).
MAIN ROTOR GEARBOX MOUNT WORN.
EMERGENCY FLOAT BOTTLE SOLENOID VALVE THERMAL RELIEF BLEW.
EXHAUST STACK CRACKED.
ENGINE BIPOD MOUNT HAS A WORN BEARING.
TAIL ROTOR LINK BEARING WORN.
PEELING PAINT ON TAIL ROTOR BLADES AND HIGH FREQUENCY VIBRIATION. REPAIRED.
FM SUDDENLY WOULD NOT TRANSMIT OR RECEIVE. FOUND BROKEN SOLDER JOINT ON POWER SUPPLY BOARD. REPAIRED. PROBLEM. BENCH CHECK GOOD.
MAIN ROTOR UNIVERSAL HAS BEARING WEAR.
FREEWHEEL UNIT HAS A CRACK BETWEEN 2 BOLT HOLES ON HOUSING. REPLACED FREEWHEEL UNIT.
MAIN ROTOR ENGINE TO GEARBOX SPLINE ADAPTER WORN.
STARTER GEN BRUSHES WORN. REPAIRED.
BEARING SEPARATED FROM ENGINE MOUNT. REPLACED WITH SERVICEABLE PART.
FILTER FOUND IN BYPASS CONDITION. REPLACED WITH SERVICEABLE PART.
ENGINE MAKING METAL. REPLACED WITH SERVICEABLE ENGINE.
OCCASIONAL HIGH MGT WITH POWER CHANGES AND POSSIBLE INTERNAL CONTAMINATION. REPLACED BLEED VALVE.
AFT ENGINE OIL TANK SUPPORT CRACKED.
FWD ENGINE OIL TANK SUPPORT CRACKED AT FWD RT MOUNT BOLT.
MIC ON HEADSET BROKEN. REPAIRED.
DATA BOX SKYWATCH UNRELIABLE.
ADI WON'T CAGE. REPAIRED.
INPUT DRIVESHAFT IS CORRODED.
TRIM PANEL CRACKED.
EMERGENCY FLOAT BOTTLE SOLENOID VALVE LEAKING.
ROTOR BRAKE TRIM IS CRACKED.
TAIL ROTOR GEARBOX TRUNNION WORN.
FUEL CAP SEAL CRACKED.
SLIDING WINDOW TRACK IS DETERIORATED.
FLOAT BAG FAILED 6 MONTH LEAK TEST. TO BE SENT TO BELL HELICOPTER TEXTRON FOR CREDIT AGAINST REPLACEMENT PART PURCHASED.
FLOAT BAG FAILED 6 MONTH LEAK TEST.
HYDRAULIC TUBE PITTED.
WINDSHIELD CRAZED.
WINDSHIELD CRAZED.
SKID TUBE WORN BEYOND LIMITS.
RUST INSIDE GAUGE.
END COVER WORN AND TORN.
END COVER WORN AND TORN.
SKID TUBE WORN BEYOND LIMITS.
PITCH LINK TUBE HAS CORROSION.
FUEL INDICTOR PRESSURE SWITCH WORKS INTERMITTENTLY.
TAIL ROTOR PITCH LINK ASSY SEALS ARE LEAKING, BOOT IS DETERIORATED.
MAIN ROTOR PITCH LINK ASSY ROD END BEARINGS ARE ROUGH.
STRAP ON MLG CHAFED.
TAIL ROTOR BELLCRANK LUG IS CHAFED BEYOND LIMITS.
TAIL ROTOR DISC PACK HAS CORROSION.
LOWER TRIM PANEL ON RT AFT DOOR CRACKED.
CREW DOOR STRIKER COVER CRACKED.
UPPER TRIM PANEL ON RT AFT DOOR CRACKED.
MAIN ROTOR UPPER PC LINK BEARING WORN.
PAX / CREW DOOR CRACKED.
INTERIOR PANEL CRACKED.
MLG ROCKER BEAM BOLT PITTED.
LITTER DOOR WINDOW CRACKED.
UNIVERSAL HAS WORN BEARING.
TAIL ROTOR LINK HAS A WORN BEARING.
MLG CROSSTUBE HAS CORROSION PITS. SCRAPPED AND REPLACED WITH SERVICEABLE ASSY.
FAILED DURING START CAUSING FADEC HORN AND RAPID RISE IN TOT. REPLACED WITH SERVICEABLE PART.
TAIL ROTOR LINK HAS WORN BEARINGS.
OIL COOLER BLOWER HOUSING INLET CRACKED.
STARTER GEN HAS WORN BRUSHES.
MAIN ROTOR UNIVERSAL IS WORN.
TAIL ROTOR COOLER BLOWER HOUSING IS CRACKED.
MAIN ROTOR BEARING IS WORN.
EXHAUST DUCT IS CRACKED.
FRAHM ASSY CAUSING HIGH 4 REV.
MAIN ROTOR BEARING IS WORN.
GOES TO TEST IN FLIGHT.
BEARING OVERHEATED.
RELIEF VALVE KEPT RELEASING PRESSURE DOWN TO 2750 PSI.
ROD END ASSY WORN.
ROD END WORN.
DAMAGED. SCRAPPED LOCALLY.
DOOR PANEL DAMAGED. SCRAPPED LOCALLY.
LABELS DETERIORATING.
LABELS DETERIORATING.
BELLCRANK HAD WORN BEARINGS.
INDEX CARD LOOSE ON PRESSURE GAUGE.
SWITCH INOPERATIVE. SCRAPPED LOCALLY.
VELCRO RIPPING OFF OF FLOAT COVER ASSY. PART SCRAPPED.
UNIVERSAL WORN AND ROUGH.
FLOAT COVER ASSEMBLY TORN.
CRACKS IN ELASTOMER ARE BEYOND LIMITS.
CRACKS IN ELASTOMER ARE BEYOND LIMITS.
CRACKS IN MAIN ROTOR GEARBOX ELASTOMER ARE BEYOND LIMITS.
CRACKS IN MAIN ROTOR GEARBOX ELASTOMER ARE BEYOND LIMITS.
UNABLE TO BALANCE OIL COOLER BLOWER.
HOSE ASSY COLLAPSED.
DEEP SCRATCH IN WEB OF YOKE EXCEEDS ALLOWABLE LIMITS.
FLYWHEEL HAD WORN SPLINES.
CHANNEL CRACKED.
FLOAT COVER TORN AND TATTERED.
RIVETS PULLED AND BROKEN OUT FROM METAL ON BLOWER HOUSING.
EXHAUST STACK CRACKED.
DUCT FOUND CRACKED.
DUCT FOUND CRACKED.
PRESSURE GAUGE NEEDLE STICKS.
MGT INDICATOR WILL NOT INDICATE.
LINK HAD WORN BEARING. SERIAL NUMBERS REMOVED ARE NHFS-2980 AND NHFS-2547. REPLACED WITH SERIAL NUMBERS NHFS-4509 AND NHFS-4458.
DAMPENER HAD RUBBER SEPARATION. SERIAL NUMBERS REMOVED ARE LK-5791, LK-5801, LK-5793 AND LK-5826. REPLACED WITH SERIAL NUMBERS LK-7331, LK-7357, LK-7324 AND LK-7326.
BEARING SEPARATION. SERIAL NUMBERS REMOVED ARE LK-3751, LK-3800, LK-3811 AND LK-3746. REPLACED WITH SERIAL NUMBERS LK-4768, LK-4833, LK-4382 AND LK-4709.
SKID TUBE ASSY WORN ON BOTTOM. REFERENCE: DMR NR 686116.
SKID TUBE ASSY WORN ON BOTTOM. REFERENCE: DMR NR 686115.
TRANSMISSION ASSY MAKING METAL.
MGT INDICATOR ERRATIC AND INTERMITTENT. REFERENCE: DMR NR 686109.
MAIN ROTOR GEARBOX RUBBER MOUNT DETERIORATED.
UPPER RUBBER DETERIORATED ON MAIN ROTOR GEARBOX MOUNT.
BIPOD MOUNT HAS LOOSE BEARINGS.
LEFT FLOAT BAG LEAKING.
CLOCK/OAT/VOLTS SWITCH OVER BUTTON.
UNIVERSAL HAS WORN BEARINGS.
PRESSURE SWITCH HAS NO LIGHT.
BEARINGS WORN AND CORRODED.
TRANSPONDER REPLY LIGHT BLINKS CONSTANTLY.
COOLER HAS METAL CONTAMINATION.
MGT INDICATOR READS 4 DEGREES HIGH.
STARTER/GENERATOR REMOVED FOR 300 HOUR INSPECTION. FOUND THERE WAS NO BELL HELICOPTER PART NUMBER 206-062-200-112 ON THE I.D. PLATE. AS PER BELL, PART NUMBER 23081-018 ALONE IS NOT AUTHORIZED FOR THEIR 407 AIRCRAFT.
GROOVES WORN INTO T/R FILTER HOUSING.
SWITCH INOPERATIVE.
TRANSMISSIONMAKING METAL.
TRANSPONDER WEAK OUTPUT.