N520UW
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.
38 reports on file, 2009-11-25 – 2015-08-06.
Part: ACTUATOR — LOW PRESSURE (R2 DOOR) · airframe 23,269 hrs · 7,891 cycles
2R DOOR, FLIGHT ATTENDANT CIDS PANEL SHOWS AMBER LIGHT WHEN DOOR IS ARMED. ALSO CHECK PRESS. SERVICED 2R DOOR IAW AMM 52-10-00-614-001-A. CHECKED GOOD, OK FOR SERVICE.
Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 23,238 hrs · 7,879 cycles
CIDS DISPLAY CHECK 2R DOOR PRESS. SERVICED 2R DOOR DAMPER CYLINDER IAW AMM 52-22-00. OPERATIONS NORMAL.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 22,490 hrs · 7,589 cycles
1S CHECK, CABIN FLOOR PANEL 221EF HAS DELAMINATION. REPLACED FLOOR PANEL 221EF IAW IRM 9701 REV G.
Part: SLIDE — UNSERVICEABLE (R4 DOOR) · airframe 22,490 hrs · 7,589 cycles
1S CHECK, DURING THE REPLACEMENT OF THE R4 DOOR ESCAPE SLIDE THE REPLACEMENT SLIDE GIRT BAR LACING CABLE WAS FRAYED & COVER CABLE BROKEN & CONSEQUENTLY COULD NOT BE INSTALLED ON THE ACFT. THE DEFECTIVE SLIDE WAS RETURNED TO STORES & A SERVICEABLE SLIDE WAS INSTALLED ON THE ACFT.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,490 hrs · 7,589 cycles
1S CHECK, R4 DOOR SILL PLATE IS CORRODED AROUND AFT 2 SCREW HOLES AT FRAME 68 & Y -1250. REPAIRED SILL IAW SRM 51-43-14 REPAIR 5.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,490 hrs · 7,589 cycles
1S CHECK, CORROSION ON THE LT AFT DOOR CUT OUT LOWER SILL PLATE AT FRAME 68 & Y1292. REPAIRED THE LT AFT DOOR CUT OUT LOWER SILL PLATE AT FRAME 68 & Y1292 IAW SRM 53-41-14-201.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,490 hrs · 7,589 cycles
1S CHECK, CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT BETWEEN FRAME 56 & 58 AT STRINGER 38L. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,490 hrs · 7,589 cycles
1S CHECK, CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT BETWEEN FRAME 58 & 59, STRINGER 38L. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,490 hrs · 7,589 cycles
1S CHECK, CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT BETWEEN FRAME 53 & 56 AT STRINGER 38L. REPLACED FLOOR SUPPORT IAW SRM 51-72-00 & EA 251100.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,490 hrs · 7,589 cycles
1S CHECK, CORROSION ON AFT CARGO FLOOR SUPPORT AT FRAME 52 & STRINGER 38L. REPLACED FLOOR SUPPORT IAW EA 251100.
Part: CONNECTOR — BROKEN (CABIN) · airframe 21,797 hrs · 7,298 cycles
EMERGENCY LIGHT AT ROW 27 INOPERATIVE. FOUND A BROKEN CONNECTOR. REPLACED EMER LIGHT CABLE ASSEMBLY F1001430-48 IAW IPC 33-51-09-24N. OPERATIONAL CHECKED GOOD.
Part: LENS — MISSING (CABIN) · airframe 21,465 hrs · 7,159 cycles
EMERGENCY LIGHT LENS COVER MISSING AT DOOR 4R. INSTALLED 4R DOOR EMER LIGHT LENS COVER.
Earlier reports · 2009–2014 · 26 reports
2014
Part: LENS — MISSING (CABIN) · airframe 20,842 hrs · 6,928 cycles
ROW 9 RT EMER LIGHT LENS MISSING. REPLACED EMER LIGHT LENS AT ROW 9 RT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,842 hrs · 6,928 cycles
EMERGENCY AISLE LIGHTS AT ROW 3 LT & 6 LT ARE INOPERATIVE. REPLACED EMER AISLE LIGHTS AT ROW 3 LT & 6 LT IAW JOB CARD 26C00033004.
Part: CONNECTOR — MISWIRED (CABIN) · airframe 18,741 hrs · 6,104 cycles
EMERGENCY PATH LIGHT AT ROW 14 LT INOPERATIVE. REPINED WALL DISCONNECT PLUG AT ROW 14 EMERGENCY PATH LIGHT IAW ESPM 20-44-24.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 18,557 hrs · 6,036 cycles
PILOT REPORT, DELAMINATION ON CABIN FLOOR PANEL 221DF AT FR 17A, BL 0. REPLACED CABIN FLOOR PANEL 221DF IAW A321 AMM 53-12-12-400-001-A.
Part: LENS — MISSING (CABIN) · airframe 18,337 hrs · 5,962 cycles
ROW 1C MISSING EMERGENCY EXIT LIGHT CLEAR LENS. REPLACED EMERGENCY EXIT LIGHT CLEAR LENS AT ROW 1C.
2013
Part: FILTER — DIRTY (SMOKE DETECTOR) · airframe 17,911 hrs · 5,812 cycles
A SMOKE LAVATORY DETECTOR FAULT MESSAGE AFTER SHUTDOWN. REPLACED ALL LAVATORY SMOKE DETECTOR FILTERS. PERFORMED SDCU BITE TEST IAW AMM 26-10-00. SYS TEST PASSED, NO MESSAGE AT THIS TIME.
Part: LENS — MISSING (CABIN) · airframe 17,814 hrs · 5,777 cycles
DOOR 4R EMERGENCY EXIT LIGHT COVER IS MISSING. REPLACED DOOR 4R EMERGENCY EXIT LIGHT COVER.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 16,962 hrs · 5,482 cycles
EMERGENCY LIGHT LENS MISSING. REPLACED EMERGENCY LIGHT ASSY.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,734 hrs · 5,082 cycles
BATTERY PACK ON EMERGENCY LIGHT ASSY WILL NOT HOLD CHARGE. R & R BATTERY PACK ON EMERGENCY LIGHT ASSY.
Part: LENS — MISSING (CABIN) · airframe 15,652 hrs · 5,059 cycles
LENS COVER MISSING ON LOWER EMERGENCY EXIT LIGHT DOOR 1R. INSTALLED LENS COVER ON LOWER EMERGENCY EXIT LIGHT AT DOOR 1R.
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 14,626 hrs · 4,714 cycles
AFT CARGO FLOOR PANEL FORWARD OF CARGO DOOR (151DF), IS DELAMINATED. REPLACED AFT CARGO FLOOR PANEL 151DF IAW A321 AMM 53-42-14.
Part: WIRE — DAMAGED (CABIN) · airframe 14,626 hrs · 4,714 cycles
EMERGENCY PATH LIGHT WIRES DAMAGED AT TOP OF DOOR FRAME LAV H. (ALSO REQUIRED TERMINAL ENDS TO BE REMOVED FOR WALL REMOVAL). MAINTENANCE RECONNECTED TERMINAL ENDS TO EMERGENCY PATH LIGHT AT LAV H DOOR FRAME. OPERATIONAL CHECK GOOD.
Part: POWER SUPPLY — FAULTY (CABIN) · airframe 14,623 hrs · 4,713 cycles
EMERGENCY TRACK LIGHTING AT SEAT ROWS 20, 22 & 23 INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT AND BATTERY IAW AIRBUS MAINTENANCE MANUAL 33-51-38.
2012
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 14,112 hrs · 4,543 cycles
FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FORWARD F/A FLASHLIGHT BATTERY AND SAFETY STRAP.
Part: LENS — MISSING (CABIN) · airframe 14,016 hrs · 4,511 cycles
LENS COVER MISSING ON EXIT LIGHT AT DOOR 3L. MAINTENANCE INSTALLED NEW LENS.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 13,906 hrs · 4,471 cycles
AFT CABIN MEGAPHONE INOPERATIVE. REMOVED AND REPLACED AFT CABIN MEGAPHONE.
Part: BEAM — CRACKED (FUSELAGE) · airframe 13,182 hrs · 4,245 cycles
C11 CHECK - CRACK ON FORWARD CARGO LOWER BEAM AT FR35, -Y692. REPLACED FORWARD CARGO LOWER BEAM AT FR35, -Y692 IAW A321 SRM 51-42-11 PAR 6B & D FIG 2, 3 & 8.
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 1,212 hrs · 3,896 cycles
C7 CHECK - DELAMINATION ON AFT CARGO FLOOR PANEL BETWEEN FR56 TO FR58, S37R. REPLACED AFT CARGO FLOOR PANEL BETWEEN FR56 TO FR58, S37R IAW A321 SRM 53-42-14-400-001-A.
Part: LENS — BROKEN (CABIN) · airframe 12,006 hrs · 3,858 cycles
EMERGENCY EXIT LIGHT COVER (LENS) ON AFT RIGHT DOOR IS BROKEN AND DETACHED. REPLACED EMERGENCY EXIT LIGHT LENS COVER AT AFT RIGHT 3R DOOR.
2011
Part: COVER — MISSING (R4 DOOR) · airframe 8,287 hrs · 2,548 cycles
FLT 481 - PHL-DEN - EMERGENCY LIGHTS - EXIT LIGHT MISSING COVER AT DOOR 4R. LOCATED EMERGENCY LIGHT LENS AND SECURED LENS. (NOTE: LENS FELL OFF)
2010
Part: KNOB — MISSING (MEGAPHONE) · airframe 5,882 hrs · 1,745 cycles
FLT 250 - PHX - EE - FORWARD FLIGHT ATTENDANT MEGAPHONE MISSING VOLUME KNOB. MAINTENANCE REPLACED MEGAPHONE.
Part: TIRE — BLOWN (MLG) · airframe 5,660 hrs · 1,676 cycles
FLT 256 PHX-PHL - EMERGENCY LANDING - CREW REPORTED A LOUD NOISE AND VIBRATION ON TAKEOFF UNTIL GEAR WAS RETRACTED. FLIGHT CONTINUED TO PHL WHERE CAPTAIN DECLARED AN EMERGENCY - AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINED NR 3 MLG TIRE WAS BLOWN. REPLACED NR 3 AND NR 4 MLG TIRES IAW AIRBUS MAINTENANCE MANUAL 32-41-11 AND NR 3 BRAKE ASSEMBLY IAW AMM 32-42-27.
Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 5,265 hrs · 1,562 cycles
FLT 404 - CLT - EES - FORWARD FLIGHT ATTENDANT PANEL INDICATES DOOR 1L SLIDE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED THE 1L DOOR SLIDE.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 3,964 hrs · 1,154 cycles
FLT 257 PHX - EEL - CEILING EMERGENCY LIGHTS AT ROWS 23, 29 & 33 WERE INOPERATIVE WHILE PERFORMING EMERGENCY LIGHT TEST. MAINTENANCE RE-INSTALLED CONNECTORS AT LIGHTS, OPERATIONAL CHECK GOOD.
2009
Part: LENS — MISSING (CABIN) · airframe 2,413 hrs · 703 cycles
FLT 198 - SAN - EEL - LT ROW 9 SIDEWALL EMERGENCY LIGHT LENS COVER MISSING. MAINTENANCE INSTALLED NEW EMERGENCY LIGHT LENS COVER.
Part: O-RING — BROKEN (APU OIL FILTER) · airframe 2,192 hrs · 639 cycles
FLT 36 LAX - PHL - CABIN ODOR - DIRTY / MUSTY ODOR THROUGHOUT ENTRE AIRCRAFT ON GROUND WITH PACKS ON WHICH WORSENED AFTER TAKEOFF AND CLIMB. ODOR SLOWLY DISSIPATED DURING CRUISE BUT RETURNED ON DESCENT. ODOR CAUSED EYE AND THROAT IRRITATION TO ALL CREW MEMBERS. MAINTENANCE FOUND O-RING BROKEN AT APU OIL FILTER MODULE - REPLACED O-RING, FILTER AND CLEANED APU INLET. ALSO REPLACED ALL OZONE AND RECIRCULATION FILTERS.