N406TD

BELL 407 · 2006 · Valid Registration

Registered owner: HFS HELI V LLC, NY (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
HELICOPTER FLIGHT SERVICES, INC. (H44A)Certificate holderMatched by certificate designator
HELICOPTER FLIGHT SERVICES, INC. (H44A)Operator2023-09-21 – 2023-09-21Operator named in NTSB report

Accident & incident history

Inc · 2023-09-21 Operator named in NTSB report
Source: NTSB case ENG23LA045

Maintenance disclosures

J · 2017-05-27 Matched by certificate designator
ATA 7320

PILOT REPORTED, CANNOT ROLL DOWN TO IDLE. FADEC DEGRADE AND RESTART FAULT ON CAUTION WARNING PANEL. FOLLOWED PROCEDURE AND CUT OFF FUEL. RESTART FAULT FLASHED 5 TIMES. RETURNED TO BASE, CHECKED PLA ANGLE WHEN IN HANGAR. FADEC FAILURE HAPPENED MULTIPLE TIMES WHEN CHECKING THE PLA ON THE TWIST GRIP AND COMPUTER.

Source: SDR H44R2017053000004 · FAA SDRS
K J · 2015-12-28 Matched by certificate designator
ATA 7261

NOTICED LOSS OF TORQUE METER INDICATION AND FLUCTUATING TRANSMISSION OIL PRESSURE. TURNED BACK, TO RETURN TO PIER. ENGINE CHIP LIGHT CAME ON, WHILE LANDING ON THE PIER TRANSMISSION OIL PRESSURE LOW LIGHT CAME ON.AT ARRIVAL, NOTICED OIL UNDER ACFT, BELOW THE BAGGAGE COMPARTMENT AND OIL DOWN THE SIDE OF THE ACFT AND TAILBOOM. REMOVED THE OIL COOLER COWLING AND FOUND THE SEAMS OF THE ENGINE OIL TANK SPLIT. ABOUT A PINT OF OIL LT IN THE TANK. REMOVED THE ENGINE CHIP DETECTORS AND FOUND MINOR METAL ON THE LOWER DETECTOR, BUT MAJOR ACCUMULATION ON THE UPPER. THE CEFA OIL FILTER BYPASS BUTTON IS EXTENDED. ROTATION OF MAIN DRIVESHAFT PRODUCES GRINDING NOISE FROM TURBINE. MAIN TRANSMISSION, NO OIL SHOWING IN SIGHT GLASS. ALL CHIP DETECTORS ARE CLEAN. ENGINE REMOVAL REPORT; NG, TURNING THE COMPRESSOR IMPELLER WAS DIFFICULT AND FELT ROUGH. NP, TURNING THE PTO GEAR PRODUCED NOISE FROM THE TURBINE SECTION. BOROSCOPE INSPECTION OF THE NR 8 BEARING SHOWED INDICATIONS OF BEARING FAILURE. PTO SEALS APPEARED TO BE INTACT. ENGINE DISASSEMBLY SHOWED THAT THE DOUBLE LIP SEAL, AFT, HAD FAILED, THAT ALLOWED TRANSMISSION OIL TO ENTER THE ENGINE OIL SYSTEM. EXCESS OIL WAS UNABLE TO RETURN TO THE ENGINE CAUSING THE ENGINE OIL TANK TO OVER PRESSURIZE AND BURST AT ITS SEAM, EMPTYING THE TANK OF ITS OIL. LACK OF OIL TO THE ENGINE DESTROYED THE TURBINE SECTION BEARINGS CAUSING THE ENGINE CHIP LIGHT.

Source: SDR H44R2016012000001 · FAA SDRS