N14664
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, 2003-06-22 – 2004-05-11.
Part: SLEEVE — CRACKED (THRUST REVERSER) · airframe 15,631 hrs · 8,276 cycles
INSPECTION FOUND A 1.6" CRACK IN I/B THRUST REVERSER SLEEVE. THE SLEEVE WAS REPAIRED IAW SRM 51-70-17.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 15,630 hrs · 8,276 cycles
R2 DOOR CUTOUT THRESHOLD Z-ANGLE CORRODED. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-02.
Part: ANGLE — WORN (LT WING) · airframe 15,630 hrs · 8,276 cycles
LEFT WING TRAILING EDGE PANEL WORN JUST INBOARD OF NUMBER 3 FLAP TRACK FAIRING. REMOVED AND REPLACED ANGLE PER SRM 51-10-02.
Part: WIRE HARNESS — BURNED (BOOST PUMP) · airframe 13,701 hrs · 7,251 cycles
THE AFT FUEL BOOST PUMP LOW PRESSURE LIGHT LEFT SIDE ILLUMINATED AFTER LANDING AT DFW. WHILE TROUBLESHOOTING THE PUMP THE WIRE BUNDLE AT STA 254 IN COCKPIT WAS FOUND BURNED. OVERHEATING OF THE PUMP WAS SUSPECTED TO BE THE CAUSE OF THE BURNT WIRING. THE FUEL BOOST PUMP WAS REPLACED AS A PRECAUTIONARY MEASURE. THE DAMAGED WIRING WAS SPLICED IAW STANDARD WIRING PRACTICES MANUAL 20-30-12. THE WIRING BUNDLES WERE REROUTED, SECURED, AND ATTACHED TO AFT CLAMP. OPERATIONAL CHECKS WERE GOOD.