N14654
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.
11 reports on file, 2000-07-03 – 2011-04-06.
Part: FLOOR SUPPORT — CORRODED (BS 990) · corrosion level 2 · airframe 28,566 hrs · 14,882 cycles
L2 DOOR FLOOR STRUCTURE "Z" SUPPORT ANGLE AT STN 990 HAD LEVEL II CORROSION.
Part: SHEAR WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,566 hrs · 14,882 cycles
L2 DOOR HAS CORROSION AT AFT LOWER DOOR FRAME WEB AT STN NR 1006 LOCALIZED LEVEL II CORROSION NOTED.
Part: WEB — CORRODED (BS 800-845) · airframe 28,566 hrs · 14,882 cycles
AFT CARGO COMPARTMENT, STN 800 - 845 AT RBL 26 DOOR SURROUND SILL WEB HAS LEVEL II CORROSION NOTED. FOUND WHILE ACCOMPLISHING. WIDE SPREAD CORROSION.
Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,566 hrs · 14,882 cycles
AFT CARGO COMPARTMENT AT BS NR 787 FRAME BELOW DOOR SILL AT RBL NR 26 HAS WIDE SPREAD LEVEL II CORROSION NOTED ON FRAME.
Part: FRAME — CORRODED · airframe 28,566 hrs · 14,882 cycles
STRINGER S22R- S 26R, LEVEL II, CORROSION NOTED ON FRAME.
Part: FRAME — CORRODED (BS 994 S17-18R) · corrosion level 2 · airframe 28,566 hrs · 14,882 cycles
MAIN CABIN AT STN 994 ADJACENT TO R2 DOOR OPENING CIRCUMFERENTIAL FRAME CORRODED BETWEEN STRINGERS S17R AND S18R LEVEL II CORROSION NOTED.
Part: FILTER — UNKNOWN (NR 2 ENGINE) · airframe 23,128 hrs · 12,066 cycles
ENGINE SHUT DOWN DUE TO NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. REPLACED SCAVENGE OIL FILTER IAW AMM 79-21-04.
Part: OVEN — INOPERATIVE (AFT GALLEY) · airframe 19,573 hrs · 10,210 cycles
THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE AFT GALLEY AND AN ASSOCIATED ELECTRICAL ODOR WHILE EN ROUTE FROM IAH TO MSP. WHEN THE GALLEY POWER WAS TURNED OFF AND OVEN CIRCUIT BREAKERS WERE PULLED THE SMOKE BEGAN TO DISSIPATE. THE AIRCRAFT WAS DIVERTED TO OKC WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE NR 1 AFT GALLEY OVEN HAD FAILED INTERNALLY. THE OVEN WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 25-00-00. IN ADDITION, THE RECIRCULATION FAN FILTER WAS REMOVED AND REPLACED IAW MM 21-21-23.
Part: FUSE — BLOWN (BATTERY PACK) · airframe 17,515 hrs · 9,185 cycles
THE EMERGENCY EXIT LIGHTS ABOVE L-2 DOOR AND FLOOR PATH LIGHTS ON ROWS 18-21 WERE FOUND INOPERATIVE. THE BATTERY PACK FUSE WAS REMOVED AND REPLACED IAW MM 33-51-02-101.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 16,032 hrs · 8,362 cycles
R2 DOOR JAMB Z-CHANNEL CORRODED AT STA 992.8. REMOVED AND REPLACED CORRODED Z-ANGLE AT R2 DOOR PER SRM 51-40-02.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 7,623 hrs · 3,741 cycles
THE ENTRYWAY OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS WERE FOUND INOPERATIVE. MAINTENANCE FOUND THE BATTERY CHARGER AT FAULT. THE CHARGER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-51-51.