N433PH

BELL HELICOPTER TEXTRON CANADA 407 · 2000 · Valid Registration

Registered owner: PHI AVIATION LLC, LA (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
PHI AVIATION, LLC (HEEA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

O · 2019-07-10 Matched by certificate designator
ATA 5300

FORWARD SHELL ASSEMBLY OUTER SKIN WAS FOUND TO BE CORRODED -LOCAL TO AN EXISTING INSERT LOCATION. THE REPAIR DOCUMENTATION WILL BE SUBMITTED FOR FAA APPROVAL. THE FORWARD SHELL ASSEMBLY WILL THEN BE REPAIRED IN ACCORDANCE WITH THE FAA-APPROVED REPAIR DATA.

Source: SDR HEER20190710093 · FAA SDRS
O · 2019-01-11 Matched by certificate designator
ATA 7250

ENGINE REMOVED 12-25-18 DUE TO METAL IN OIL. DETERMINED CAUSE TO BE TURBINE NR 5 BEARING SPALLING. INSTALLED NEW BEARING. PART WILL BE RETURNED FOR EVALUATION ON SHIPPING NUMBER 4904011120191.

Source: SDR HEER20190111515 · FAA SDRS
O · 2016-09-12 Matched by certificate designator
ATA 7250

ENGINE REMOVED 8-20-16 FOR NR 5 BEARING UPGRADE. NR 5 BEARING EXHIBITED SPALLING AT OUTER RACE SPLIT. REPLACED BEARING.

Source: SDR HEER20160912130 · FAA SDRS
O · 2015-08-11 Matched by certificate designator
ATA 7250

ENGINE REMOVED DUE TO A CRACKED EXHAUST COLLECTOR. NR 5 BEARING PROBABLE SPALLING ON OUTER RACE SPLIT. RETURNED TO MFG FOR FURTHER EVALUATION.

Source: SDR HEER20150811578 · FAA SDRS
O · 2014-12-11 Matched by certificate designator
ATA 7250

ENGINE REMOVED 11-25-14 DUE TO TURBINE OVERHAUL. NR 5 BEARING EXHIBITED SPALLING BALLS. PART RETURNED TO ROLLS ROYCE FOR FURTHER EVALUATION.

Source: SDR HEER20141211552 · FAA SDRS
R J · 2007-08-16 Matched by certificate designator
ATA 7250

APPROXIMATELY 5 MINUTES AFTER TAKEOFF, THE ENGINE FAILED AND AUTOROTATION WAS COMPLETED TO THE WATER. ENGINE WAS REMOVED DUE TO ENGINE SHUTDOWN. SUSPECT 3RD STAGE WHEEL FAILURE, 3RD STAGE WHEEL FOUND WITH ALL BLADES FRACTURED AT ROOT. TURBINE WAS SHIPPED TO MFG FOR FAILURE ANALYSIS.

Source: SDR HEEA116968 · FAA SDRS
O · 2006-11-25 Matched by certificate designator
ATA 6320

METAL, THE CHIP LIGHT WAS CAUSED BY SLIVER OF METAL CREATED WHEN MFG INSTALLED BEARING 406-040-037-103 INTO THE LOWER MAST HOUSING 407-040-054-101. REPLACED TRANSMISSION. REQUESTS FOR WARRANTY CREDIT FOR PARTS AND LABOR DUE TO METAL SLIVER BEING CREATED DURING ASSEMBLY AT MFG.

Source: SDR HEEA113076 · FAA SDRS