N401DC
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.
6 reports on file, 2014-11-28 – 2015-09-12.
Part: ENGINE — MAKING METAL · airframe 8,006 hrs · 22,638 cycles
NR 1 ENGINE CHIP LIGHT ILLUMINATED IN FLIGHT. MADE PRECAUTIONARY LANDING. DISCOVERED SMALL SLIVER ON REAR BEARING SUPPORT HOUSING CHIP DETECTOR. CATEGORIZED AND TYPED AS MINOR FUZZ IAW LTS101-750B-1, MM 72-00-00 PARA 20 C & D. RETURNED TO SERVICE IAW MFG, LTS101-750B-1, MM 72-00-00 PARA. F2A.
Part: CONNECTOR — DIRTY (NR 1 ENGINE) · airframe 7,899 hrs · 22,347 cycles
NUMBER 1 ENG OIL PRESSURE GAUGE WENT TO 0 BAR INDICATION, WITH NO CORRESPONDING WARNING LIGHT. RETURNED TO BASE. CLEANED PRESSURE TRANSDUCER CONNECTOR. OPERATIONS CHECKED NORMAL DURING GND RUN.
Part: DOUBLER — CRACKED (TAIL BOOM) · airframe 7,794 hrs · 21,977 cycles
DURING DAILY PREFLIGHT CHECK, FOUND A 55 MM CRACK ON LEFT HAND TAIL BOOM TO VERTICAL FIN DOUBLER.
Part: SKIN — CRACKED (TAILBOOM) · airframe 7,753 hrs · 21,800 cycles
0.75 INCH CRACK ON FUSELAGE TAIL CONE SKIN UNDER TOP RIVET OF AFT UPPER ECU MOUNT DISCOVERED DURING 6000 HOUR/6 YEAR INSPECTION.
Part: FITTING — CORRODED (TRANSMISSION) · corrosion level 2 · airframe 7,753 hrs · 21,800 cycles
CORROSION FOUND UNDER RT LOWER TORQUE MOUNT FITTING ON MAIN TRANSMISSION CASE.
Part: FLOOR PANEL — CORRODED (CABIN) · airframe 7,753 hrs · 21,800 cycles
CORROSION FOUND ON CABIN FLOOR SKIN AROUND THREADED INSERTS INSTALLED AS PART OF STC SR00346DE.