N441YX
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.
14 reports on file, 2016-03-23 – 2021-07-06.
Part: SPAR — CRACKED (RT WING TIP) · airframe 16,621 hrs · 11,182 cycles
WHILE IN HEAVY CHECK - RT WINGTIP SPAR 1 CRACKED AT RADIUS AS MARKED. REPLACED SPAR 1 IAW SRM 51-40-08
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 15,605 hrs · 10,509 cycles
COCKPIT EMERGENCY LIGHT DOESN'T WORK. INSPECTED AND FOUND TO BE A BAD CONNECTION OF LIGHT CONNECTOR. RESECURED CONNECTOR.
Earlier reports · 2016–2020 · 12 reports
2020
Part: SKIN — DAMAGED (FRAMES 10-11) · airframe 15,364 hrs · 10,372 cycles
FWD FUSELAGE HAS LIGHTNING STRIKE DAMAGE ON STR CTL BETWEEN FR 10 AND FR 11. REPAIRED IAW ETD2020-170-035769. A/C RETURNED TO SERVICE ON 12-19-20.
2019
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,217 hrs · 8,265 cycles
CABIN NR 5 EMERGENCY CEILING LIGHT INOPERATIVE. R & R EMERGENCY CEILING LIGHT POWER UNIT IAW AMM 33-50-01.
Part: ROLLER — MISSING (L2 DOOR) · airframe 11,725 hrs · 7,927 cycles
L2 DOOR HARD TO OPEN. FOUND ROLLER MISSING ON DECORATIVE COVER. R&R ROLLERS IAW AMM 25-23-09.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,560 hrs · 7,822 cycles
CORROSION-AFT CARGO DOOR LOWER BEAM FLOOR PANEL SUPPORT. REMOVED AND REPLACED AFT CARGO LOWER BEAM FLOOR PANEL SUPPORT. SRM 51-21-01, AMM 20-10-01. SEE W/O H6640 SN 317 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,560 hrs · 7,822 cycles
CORROSION - FWD RT OUTBD FLOOR SILL CORRODED AS MARKED FR 12-14. REMOVED AND REPLACED FLOOR SILL AT FR 12-14 RT. APPLIED SURFACE PROTECTION REF SRM 51-23-04,51-23-05 AND 51-23-06. SEE W/O H6640 SN 299 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,560 hrs · 7,822 cycles
CORROSION - RT SEAT TRACK CORRODED AS MARKED FR 13-18. REMOVED AND INSTALLED NEW RT SEAT TRACK AS MARKED FR 13-18 REF SRM 51-40-08 APPLIED SURFACE PROTECTION REF SRM 51-23-04,51-23-05,51-23-06. SEE W/O H6640 SN 298 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,560 hrs · 7,822 cycles
CORROSION AT FR89 RT OB PANEL SUPPORT AS MARKED. REMOVED AND REPLACED RT OB PANEL SUPPORT FR 89 REF SRM 51-40-08 APPLIED SURFACE PROTECTION REF SRM 51-23-06. SEE EAMS W/O H6640 SN 267 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,560 hrs · 7,822 cycles
CORROSION AT FR90 RT OB GUSSET PLATE AS MARKED. REMOVED AND REPLACED RT OB GUSSET PLATE FR 89 REF SRM 51-40-08 APPLIED SURFACE PROTECTION REF SRM 51-23-05. SEE W/O H6640 SN 268 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,560 hrs · 7,822 cycles
CORROSION AT FR 87-88 RT SHEAR PANEL. REMOVED AND REPLACED AND RESTORED SURFACE PROTECTION RT SHEAR PANEL FR 87-88. SRM 51-40-08, 51-23-04, 51-23-05, AND 51-23-06. SEE W/O H6640 SN 265 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,560 hrs · 7,822 cycles
CORROSION AT FR 88-89 RT INBD BEAM AS MARKED. REMOVED AND REPLACED RT INBD BEAM AT FR 86-89 REF SRM 51-40-08. TOP COATED REF SRM 51-23-06 CIC APPLIED TO RT INBD BEAM AT FR 88-89. REF CPM 51-25-00. SEE W/O H6640 SN 269 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
2017
Part: DOOR — LACK OF LUBE (L1) · airframe 5,984 hrs · 4,239 cycles
L1 DOOR MAKES A LOUD POPPING NOISE WHEN OPENED. LUBRICATED THE DOOR IAW AMM 53-10-21 AND PERFORMED FUNCTIONAL CHECK IAW AMM 52-1-25. NO DEFECTS NOTED.
2016
Part: LIGHT — DAMAGED (CABIN) · airframe 3,172 hrs · 2,308 cycles
MAINTENANCE REPORTED THAT SEVERAL EMERGENCY LIGHT STRIPS WERE SCRATCHED AND DIRTY. MAINTENANCE R & R LIGHT STRIPS IAW AMM AND OPS CHECKED GOOD.