N14601
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.
10 reports on file, 1998-07-16 – 2009-01-17.
Part: CABLE ASSY — FRAYED (EVAC SLIDE) · airframe 41,334 hrs · 21,521 cycles
R-2 DOOR EMERGENCY ESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS. REMOVED AND REPLACED R-2 DOOR SLIDE LATCH CABLE PER 25-61-35.
Part: CABLE ASSY — FRAYED (EVAC SLIDE) · airframe 41,334 hrs · 21,521 cycles
L-2 DOOR EMERGENCY ESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS. REMOVED AND REPLACED L-2 DOOR SLIDE LATCH CABLE PER 25-61-35.
Part: CARGO TRACK — CORRODED (BS 794-827) · airframe 36,326 hrs · 18,904 cycles
INSPECTION FOUND AFT CARGO COMPARTMENT RT FLOOR TIEDOWN TRACK CORRODED AT STA 794-827, RBL 13.8. INSTALLED NEW TIEDOWN TRACK IAW SRM 53-60-53.
Part: SHEAR WEB — CORRODED (BS 482) · airframe 36,326 hrs · 18,904 cycles
INSPECTION FOUND C-1 COMPARTMENT BELTFRAME LOWER SHEAR CLIP CORRODED AT STA 482, S27R TO S27L. THE CORROSION WAS REMOVED AND A REPAIR SHEAR TIE WAS INSTALLED IAW SRM 53-00-07, REPAIR 3.
Part: SHEAR WEB — CORRODED (BS 482 S26-27L) · airframe 36,326 hrs · 18,904 cycles
INSPECTION FOUND C-1 COMPARTMENT BELTFRAME LOWER SHEAR CLIP CORRODED AT STA 482, S26L TO S27L. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-07, REPAIR 10.
Part: SLIDE — DISCHARGED (L-2 DOOR) · airframe 31,677 hrs · 16,475 cycles
INSPECTION FOUND THE L-2 DOOR EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE LOW. THE SLIDE ASSEMBLY WAS REPLACED IAW MM 25-61-35.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,921 hrs · 15,597 cycles
INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 42. THE CORROSION WAS REMOVED AND A STRAP WAS INSTALLED IAW ECRA 5321-01196.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,983 hrs · 15,113 cycles
THE EMERGENCY AISLE PATH LIGHTING IN FIRST CLASS CABIN FAILED AFTER 30 SECONDS OF TESTING. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-51 AND OPERATION OF THE EMERGENCY LIGHTS CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (ROW 10 - 17)
INSPECTION FOUND EMERGENCY LIGHTS OUT FROM SEAT ROW 10-17. THE BATTERY PACK AND CHARGER WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD.
Part: FAN BLADE — FRACTURED (NR 1 ENGINE)
WHILE EN ROUTE, AN EMERGENCY LANDING WAS REQUIRED FOR FUEL STOP (DUE TO A COMBINATION OF LONG TAXI TIME IN EWR AND WEATHER EN ROUTE). THE AIRCRAFT WAS DIVERTED TO JAX AND WHILE ON FINAL APPROACH THE NR 1 ENGINE FAILED. THE AIRCRAFT LANDED AT JAX WITHOUT INCIDENT. MAINTENANCE FOUND INTERNAL DAMAGE TO THE NR 1 ENGINE NOSE COWL, BELIEVED TO BE CAUSED BY SEPARATION OF A FAN BLADE. THE NR 1 ENGINE WILL BE REMOVED AND REPLACED. *S/D* INVESTIGATION CONCLUDED THAT THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO SEPARATION OF A FAN BLADE CAUSED BY FOD.