N440LX

No registry detail on file · not in current registry

Operators of this aircraft

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

No operator established for this aircraft.

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

3 reports on file, 2010-05-09 – 2012-05-10.

OTHER · 2012-05-10 Unresolved
ATA 2497

Part: WIRE — SHORTED

DURING A D-CHECK INSPECTION, WIRING IN AFT BAGGAGE LT LOWER AREA, IT WAS NOTED THAT THERE WERE SOME BURNED WIRES ON THE P489 CONNECTOR. THESE HAD SHORTED OUT AND HAD BURNED THRU THE INSULATION. THE GROUNDED SHIED WIRE W811 HAD MELTED INSULATION AND FUSED TO ANOTHER GROUNDED WIRE. THE WIRES ALSO AFFECTED WERE: THE 22 BL WHICH GOES TO THE PCB ASSY, WIRE NR 22 WH WHICH GOES TO THE LT GEN CONTROL UNIT. THIS NEEDS TO BE INSPECTED THOROUGHLY AS THIS CAN CAUSE INDICATION PROBLEMS IN THE COCKPIT AND COULD POSSIBLY CAUSE A FIRE. THE DAMAGED WIRES WERE REPLACED.

Source: SDR 2012FA0000340
OTHER · 2012-05-10 Unresolved
ATA 2497

Part: WIRE — SHORTED

DURING A D-CHECK INSPECTION, WIRING IN THE AFT BAGGAGE RT LOWER AREA IT WAS NOTED THAT THERE WERE SOME BURNED WIRES ON THE P490 CONNECTOR. THESE HAD SHORTED OUT AND HAD BURNED THRU THE INSULATION. THE GROUND SHIELD WIRE W812 HAD MELTED INSULATION AND FUSED TO ANOTHER GROUND WIRE. THE WIRES ALSO AFFECTED WERE WIRE NR 22BL WHICH GOES TO THE R PCB ASSY. WIRE 22WH WHICH GOES TO THE R GEN CONTROL UNIT. THIS NEEDS TO BE INSPECTED THOROUGHLY AS THIS CAN CAUSE INDICATION PROBLEMS IN THE COCKPIT AND COULD POSSIBLY CAUSE A FIRE. THE DAMAGED WIRES WERE REPLACED.

Source: SDR 2012FA0000339
VIBRATION/BUFFET; FLT CONT AFFECTED · 2010-05-09 Matched by certificate designator
ATA 5343

Part: FITTING — WORN (MLG)

DURING CLIMB, CREW REPORTED AN UNUSUAL AIRFRAME VIBRATION. AFTER LEVELING OFF, CREW REPORTED THE VIBRATION CEASED AND A LOUD BANG; DECISION TO DIVERT WAS MADE. DURING DESCENT, VIBRATION RETURNED & SECOND BANG HEARD, IMMEDIATELY FOLLOWED BY A SUDDEN YAW MOVEMENT TO RT. ACFT LANDED SAFELY. MX DISCOVERED MID FUSELAGE MAIN LANDING GEAR FITTING ASSY MOUNTING HOLES ELONGATED. THE MLG FITTING WAS REPAIRED WITH DER APPROVAL.

Source: SDR DJFA2010010