N397AL

BELL 412 · 1990 · Valid Registration

Registered owner: VERTOL SYSTEMS CO LLC, DE (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
PATHFINDER AVIATION LLC (P3TA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

K · 2012-10-18 Matched by certificate designator
ATA 7261

ON INSPECTION, AN OIL LEAK WAS DISCOVERED IN THE COMBINED GEARBOX AREA. ON FURTHER INSPECTION THE NR 1 ENGINE CHIP DETECTOR HSG ATTACHED TO THE GEARBOX WAS FOUND CRACKED.

Source: SDR EOPA20121022397 · FAA SDRS
O · 2011-02-02 Matched by certificate designator
ATA 5302

FRAME WAS FOUND CRACKED AT APPROX STA 78 IN TAILBOOM ABOVE BAGGAGE COMPARTMENT.

Source: SDR EOPA020211397AL · FAA SDRS
O · 2011-01-28 Matched by certificate designator
ATA 6210

M/R BLADE T/E "WEDGE" CAME DEBONDED. REMOVED REMAINING PORTION OF WEDGE AND TOUCHED UP PAINT IAW MFG PRODUCT SUPPORT ENGINEERING.

Source: SDR 2011F00024 · FAA SDRS
O · 2011-01-28 Matched by certificate designator
ATA 5302

FOUND .5 IN CRACK IN BULKHEAD ASSY LOCATED AT APPROX STA 185 IN TAILBOOM. CRACK WAS IN THE CTR RT PORTION OF THE FRAME.

Source: SDR EOPA012811397AL · FAA SDRS
F · 2010-09-03 Matched by certificate designator
ATA 6710

ON APPROCH, THE COLLECTIVE STUCK AT APPROX 50 PERCENT TORQUE. PILOT WAS ABLE TO FORCE COLLECTIVE TO BREAK IT FREE. PROBLEM WAS CAUSED BT A N2 CONTROL CABLE SEIZEING UP CAUSING THE SHEAR RIVET TO SHEAR.

Source: SDR ALGA2010F00206 · FAA SDRS
O · 1998-08-13 Unresolved
ATA 3213

DURING 12-MONTH INSPECTION, FOUND CORROSION PITTING IN CROSS TUBE BEYOND LIMITS.

Source: SDR 98ZZZX3601 · FAA SDRS
O · 1995-07-06 Unresolved
ATA 5412

DURING REPLACEMENT OF ENGINE DECK/WORK DECK, FOUND SEAL RETAINERS CORRODED. ALUMINUM RETAINERS RIVETED TO STAINLESS STEEL PARTS.

Source: SDR 95ZZZX4098 · FAA SDRS
O · 1995-07-06 Unresolved
ATA 5320

DAILY INSPECTION FOUND WORK DECK PANELS TOP SKIN SEPARATED OVER A LARGE AREA. ALSO, UNDERSIDE OF PANEL IS SWELLED. SUSPECT CAUSED BY PROLONGED EXPOSURE TO HIGH TEMPERATURES.

Source: SDR 95ZZZX4095 · FAA SDRS
O · 1995-07-06 Unresolved
ATA 5412

DURING REPLACEMENT OF WORK DECK/ENGINE DECK, FOUND SEAL RETAINERS CORRODED. ALUMINUM RETAINERS ON STAINLESS STEEL PARTS.

Source: SDR 95ZZZX4097 · FAA SDRS
O · 1995-07-06 Unresolved
ATA 5412

DURING REPLACEMENT OF ENGINE SERVICE DECK, FOUND THE STRAPS ON UPPER FIREWALL WHERE THE AIR MANAGEMENT SYSTEM BOLTS ON, HAD SEVERE CORROSION. CAUSED BY ALUMINUM BEING SANDWICHED BETWEEN STAINLESS STEEL. SUSPECT CAUSED DISSIMILAR METAL CORROSION.

Source: SDR 95ZZZX4096 · FAA SDRS
O · 1995-05-10 Unresolved
ATA 6220

ON DISASSEMBLY FOR REPAIR, FOUND BEARING RACE WORN BEYOND LIMITS. BEARING PN 412010216105, SN RE299. ARM PN 412010263101.

Source: SDR 95ZZZX2792 · FAA SDRS
O · 1995-05-10 Unresolved
ATA 6220

ON DISASSEMBLY FOR REPAIR, FOUND BEARING RACE WORN BEYOND LIMITS. BEARING PN 412010216105, SN RE493. ARM PN 412010263101.

Source: SDR 95ZZZX2791 · FAA SDRS
J · 1995-03-27 Matched by certificate designator
ATA 2822

DURING CRUISE FLIGHT NR 2, ENGINE FUEL BOOST PUMP PRESSURE FLUCTUATED AND THEN PRESSURE WENT TO ZERO. REPLACED BOOST PUMP. CAUSE UNKNOWN.

Source: SDR 95ZZZX1851 · FAA SDRS