N905LX

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, 2006-04-12 – 2009-06-17.

OTHER · 2009-06-17 Matched by certificate designator
ATA 3397

Part: WIRE HARNESS — BURNED (LAV LIGHTS) · airframe 5,824 hrs · 3,187 cycles

DURING A SCHEDULED MX, MX PERSONNEL DISCOVERED THE LAVATORY UPWASH LIGHTS INOPERATIVE. UPON FURTHER INSPECTION, THE WIRE HARNESS FROM ONE OF THE POWER SUPPLIES WAS FOUND BURNED. THE BURNED AREA WAS LOCALIZED AND ATTRIBUTED TO ITS PROXIMITY TO THE POWER SUPPLY WHICH TENDS TO REACH VERY HIGH TEMPERATURES. THE WIRES WERE REPAIRED AND THE HARNESS WAS SECURED AND ROUTED SUCH THAT EXPOSURE TO THE HEAT FROM THE LIGHTING POWER SUPPLY WOULD BE REDUCED.

Source: SDR DJFA2009020
OTHER · 2008-11-26 Matched by certificate designator
ATA 2530

Part: DRAIN MAST — FROZEN (FWD GALLEY)

FWD GALLEY ICE DRAWER DRAIN FROZEN, INSPECTED AND FOUND FWD GALLEY HEATED DRAIN MAST OVERHEATED AND WIRES BURNED OFF. THIS UNIT WAS REPLACED DUE TO AD2007-17-10 IAW SB145LEG-38-0013, 648.8 HRS PRIOR TO FAILURE. RECOMMEND THAT MFG TEST PARTS FOR POSSIBLE SHORTING OR OVERHEAT PROBLEMS.

Source: SDR DJF2008F00017
FLUID LOSS; WARNING INDICATION · 2006-04-12 Matched by certificate designator
ATA 2810

Part: VALVE — LEAKING (WING) · airframe 2,021 hrs · 1,105 cycles

FOLLOWING DEPARTURE, CREW WAS ADVISED BY TOWER THAT A FUEL TRAIL BEHIND ACFT. AN EMERGENCY WAS DECLARED & ACFT RETURNED. CFR RESPONSE GIVEN FOLLOWING AN UNEVENTFUL LANDING. MX REPLACED THE LT AND RT WING VENT VALVES. NO LEAKS WERE NOTED AFTER THE AIRCRAFT WAS REFUELED. WING VALVE NR 2 FOUND TO BE CLOSED AFTER ACFT REFUELED. DEFUEL VALVE REPLACED & SATISFACTORY OPS & LEAK CHECKS PERFORMED. AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED AND THE DATA WAS REVIEWED FROM THE FLT DATA RECORDER DOWNLOAD. RT OUTBOARD SUMP DRAIN VALVE REPLACED AFTER IT WAS FOUND TO BE LEAKING WHEN THE OVERWEIGHT LANDING INSPECTION WAS BEING PERFORMED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR DJFA2006229