N14660
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.
7 reports on file, 2002-11-02 – 2007-05-21.
Part: WIRE HARNESS — BURNED (NR 1 ENGINE) · airframe 23,467 hrs · 12,542 cycles
THE LEFT SIDE CABIN LIGHTS QUIT WORKING ACCOMPANIED BY AN ELECTRICAL SMELL SHORTLY AFTER TAKEOFF FROM EWR. THE STAB TRIM QUIT WORKING A SHORT TIME LATER. THE AIRCRAFT WAS RETURNED TO EWR. THE NR 1 BUS OFF LIGHT ILLUMINATED ON FINAL. MAINTENANCE FOUND THE NR 1 TRANSFORMER RECTIFIER CIRCUIT BREAKER POPPED. THE NR 1 ENGINE GENERATOR FEEDER CABLES WERE BURNT AND THE CONNECTOR AND RECEPTACLE WERE SHORTED AT THE FIREWALL. THE NR 1 ENGINE GENERATOR FEEDER HARNESS WAS REMOVED AND REPLACED AND CONNECTORS D410 AND D3024 WERE ALSO REMOVED AND REPLACED IAW SWP 20-30-11 AND 20-61-19. AN OPERATIONAL CHECK OF THE NR 1 ENGINE GENERATOR WAS PERFORMED IAW MM 24-21-00, PAGE 509, ITEM N AND NO FAULTS WERE FOUND.
Part: SILL — CORRODED (FUSELAGE) · airframe 15,307 hrs · 8,299 cycles
INSPECTION FOUND AFT BAGGAGE BIN LOWER SILL CORRODED AT STA 794.3-847, S24R-25R. THE LOWER SILL WAS REMOVED AND REPLACED IAW SRM 51-10-2.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,307 hrs · 8,299 cycles
INSPECTION FOUND A 1.5 INCH CRACK IN ANGLE AT FORWARD BULKHEAD STA 727, RBL 3. A DOUBLER WAS INSTALLED ON THE ANGLE IAW SRM 51-70-11.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 15,307 hrs · 8,299 cycles
INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT BETWEEN STA 312-328, LBL 46. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.
Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 13,709 hrs · 7,464 cycles
INSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE DENTED WITH A SHARP CREASE IN THE CENTER OF THE DENT AT LEADING EDGE STA 184. REPAIRED IAW SRM 55-10-01 AND ECRA 5510-01647.
Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 13,708 hrs · 7,463 cycles
MAINTENANCE REMOVED AN INTERIM REPAIR ON THE RT HORIZONTAL STABILIZER AT THE LEADING EDGE. THE DENT WAS NEAR A RIB AT LEADING EDGE STATION 184.66. THE FINAL TRIM OUT WAS 3.5 INCHES BY 4.5 INCHES. A PERMANENT REPAIR WAS PERFORMED BY INSTALLING A FLUSH REPAIR AT THE RIB.
Part: RING · airframe 12,273 hrs · 6,653 cycles
LH WHEEL WELL FAIRING SUPPORT RING HAS 16" CRACK. REMOVED AND REPLACED FAIRING RING IAW SRM 51-40-02.