N541LN

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.

4 reports on file, 2009-12-11 – 2017-10-05.

OTHER · 2017-10-05 Matched by certificate designator
ATA 5320

Part: STEP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 6,940 hrs · 15,307 cycles

CORROSION WAS DETECTED AROUND THE PERIMETER OF THE LEFT SIDE MAINTENANCE STEP IN THE FUSELAGE.

Source: SDR 2A6R20171005003
SMOKE/FUMES/ODORS/SPARKS · 2016-11-05 Matched by certificate designator
ATA 2120

Part: UNKNOWN — ODOR · airframe 6,524 hrs

INSPECTED ALL AIR CONDITIONER ELECTRICAL BLOWERS, MEDICAL EQUIPMENT, CHARGING BANKS, PELICAN RACK, AND ACCESSIBLE ELECTRICAL COMPONENTS, AS WELL AS RAN AIRCRAFT FOR A FULL 15 MINUTES WITH AIR CONDITIONER ON HIGH AND ALL ELECTRICAL EQUIPMENT PLUGGED IN AND ALL INTERIOR LIGHTS ILLUMINATED AND COULD NOT DUPLICATE SMELL.

Source: SDR QMLA2016110516124
OTHER · 2012-06-25 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (BS 5116-5200) · airframe 3,236 hrs · 7,429 cycles

DURING INSPECTION OF ACFT, CORROSION WAS FOUND UNDER THE GROUND POINT ON THE LT SIDE OF THE FUSELAGE. GROUND POINT WAS REPAIRED IAW RDAS-AE11-0179 AND FAA FORM 8110-3 APPROVED DERT-750020-SW. FABRICATED A FILLER USING 0.20" THICK 2024-T3 ALUMINUM ALLOY. FRABRICATED A DOUBLER USING 0.32" THICK 2024-T3 ALUMINUM ALLOY. POSITIONED DOUBLER AND MATCH DRILLED EXISTING FASTENER HOLES, PILOT DRILLED FOR ADDED FASTENERS. REMOVED DOUBLER AND DE-BURRED, CLEANED, ALODINED AND EPOXY PRIMED ALL BARE ALUMINUM. COATED FRAYING SURFACES OF THE DOUBLER AND ACFT WITH SEALANT AND USING MS20470AD4 FASTENERS IN ALL EXISTING AND NEW LOCATIONS.

Source: SDR QMLA2012062512103
OTHER · 2009-12-11 Matched by certificate designator
ATA 3212

Part: CABLE — CORRODED (EMERGENCY FLOAT) · airframe 1,643 hrs · 3,963 cycles

DURING 18 MONTH INSP OF EMERGENCY FLOAT SYS, FOUND CABLE FOR ACTUATING DEPLOYMENT OF FLOATS CORRODED COMPLETELY THRU. CABLE FOR FLOAT SYS IS PART OF STC NR SR01855LA. SYS WAS INSTALLED ON ACFT 08 MAY 2008. MECHANICS INSTALLING REPLACEMENT CABLE WILL INSTALL WITH CPC AND DROPPING INSP TO 6 MONTHS FOR NOW.

Source: SDR QMLA2009121109047