N110UW

Service difficulty reports · 301

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N110UW' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR USAA2011082300017Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM BETWEEN FR16 TO FR20, -Y254. REPLACED LONGITUDINAL BEAM BETWEEN FR16 TO FR20, -Y254 IAW A320 SRM 53-11-14 FIG 104 & SRM 51-42-11.Aug 8, 2011 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011082300008Longeron · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LONGERON BEAM BETWEEN FR12 TO FR16, -Y81. REPLACED LONGERON BEAM BETWEEN FR12 TO FR16, -Y81 IAW A320 SRM 51-42-11.Aug 8, 2011 · N110UW · Airbus A320214 · Fuselage Main, Longeron/StringerSDR USAA2011082300007Longeron · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LONGERON BEAM BETWEEN FR18 TO FR20, Y1292. REPLACED LONGERON BEAM BETWEEN FR18 TO FR20, Y1292 IAW A320 SRM 51-42-11.Aug 8, 2011 · N110UW · Airbus A320214 · Fuselage Main, Longeron/StringerSDR USAA2011082300023Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR65 TO FR66, -Y1732. REPLACED LONGITUDINAL BEAM BETWEEN FR65 TO FR66, -Y1732 IAW A320 SRM 53-00-14 FIG 102 & 51-42-11.Aug 7, 2011 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011082300022Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR66 TO FR70, Y765. REPLACED LONGITUDINAL BEAM BETWEEN FR66 TO FR70, Y765 IAW A320 SRM 53-00-14 FIG 102 & 51-44-11.Aug 7, 2011 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011082300021Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR65 TO FR66, Y765. REPLACED LONGITUDINAL BEAM BETWEEN FR65 TO FR66, Y765 IAW A320 SRM 53-00-14 FIG 102 & 51-44-11.Aug 7, 2011 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011082300020Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR20 TO FR23, -Y254. REPLACED LONGITUDINAL BEAM BETWEEN FR20 TO FR23, -Y254 IAW A320 SRM 53-11-14 FIG 104 & SRM 51-42-11.Aug 7, 2011 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011082300019Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR64 TO FR65, -Y464. REPLACED LONGITUDINAL BEAM BETWEEN FR64 TO FR65, -Y464 IAW A320 SRM 53-41-14 FIG 102 & SRM 51-42-11.Aug 7, 2011 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011082300018Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR68 TO FR70, -Y464. REPLACED LONGITUDINAL BEAM BETWEEN FR68 TO FR70, -Y464 IAW A320 SRM 53-41-14 FIG 102 & SRM 51-42-11.Aug 7, 2011 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011082300016Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR16 TO FR20, -Y254. REPLACED LONGITUDINAL BEAM BETWEEN FR16 TO FR20, -Y254 IAW A320 SRM 53-11-14 FIG 104 & SRM 51-42-11.Aug 7, 2011 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011082400008Floorbeam · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, -Y160. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, -Y160 IAW A320 SRM 51-74-00, 53-11-14 FIG 104, 51-42-11.Aug 5, 2011 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2011082400029Sill · corroded2S CHECK - LEVEL 2 EXFOLIATION CORROSION ON DOOR SILL AT FR66, Y1732. REPLACED DOOR SILL AT FR66, Y1732 IAW A320 SRM 53-41-14 FIG 10 & SRM 51-74-00.Aug 2, 2011 · N110UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2011070800012Lens · missingFORWARD ENTRY DOOR L1 EMERGENCY LIGHT MISSING LENS. REPLACED MISSING LENS BY DOOR L1.Jul 5, 2011 · N110UW · Airbus A320214 · Emergency LightingSDR USAA2011061400003Lens · missingFLL - EEL - EMERGENCY EXIT LENS ROW 11L MISSING. INSTALLED EMERGENCY EXIT LENS ROW 11L.Jun 13, 2011 · N110UW · Airbus A320214 · Emergency LightingSDR USAA2011053100012Wire · looseLAX - EEL - EMERGENCY POWER SUPPLY UNIT (EPSU) FIN#13WL FAILED TEST AFTER BATTERY REPLACEMENT. EXTERIOR LIGHT FAULT INDICATION. PERFORMED TROUBLESHOOTING PROCEDURE. FOUND LOOSE WIRE CONNECTOR ON R AFT DOOR SLIDE LIGHT. SECURED CONNECTOR. SYSTEM TEST GOOD.May 28, 2011 · N110UW · Airbus A320214 · Light System WiringSDR USAA2011040191305Unknown · odorFLT 882-CUN-CLT - ELECTRICAL SMELL - CREW REPORTED AVIONICS SMOKE ECAM MESSAGE AT GATE ALONG WITH STRONG ELECTRICAL SMELL IN COCKPIT. POWERED DOWN AIRCRAFT AND EVACUATED. MAINTENANCE REMOVED AND REPLACED THE AVIONIC VENT FILTER AND CABIN RECIRCULATION FILTERMar 27, 2011 · N110UW · Airbus A320214 · Air Distribution SystemSDR USAA2010110592519Fitting · corrodedPIT - GDAF VISIT - MAJOR REPAIR - CORROSION IN BORE OF RIGHT MAIN LANDING GEAR DOOR LOWER ACTUATOR LUG FITTING. REPAIRED BORE OF RIGHT MAIN LANDING GEAR DOOR LOWER ACTUATOR LUG FITTING IAW EA NR 116481.Nov 4, 2010 · N110UW · Airbus A320214 · Landing Gear DoorsSDR USAA2010110392469Lens · missingCK - LAX - EEL - FIRST CLASS EMERGENCY LENS IS MISSING. MAINTENANCE INSTALLED NEW LENS COVER.Nov 2, 2010 · N110UW · Airbus A320214 · Emergency LightingSDR USAA2010110292464Brake Sys · malfunctionedFLT 1539 - CLT-SEA - EMERGENCY LANDING - ON APPROACH TO SEA, SLAT/FLAP FAULT, UNABLE TO RECYCLE, STUCK AT SLAT 2 & FLAP 0. RESET FLAPS PER AMM TASK 27-50-00-869-006 RESET WING TIP BRAKE SYSTEM. OPERATIONAL CHECK WAS GOOD.Oct 30, 2010 · N110UW · Airbus A320214 · Trailing Edge Flap Control SystemSDR USAA2010100192172Cylinder · low pressureFLT 894 - ATL - EES - L-2 DOOR ASSIST BOTTLE LOW. MAINTENANCE SERVICED L-2 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.Sep 30, 2010 · N110UW · Airbus A320214 · Passenger/Crew DoorsSDR USAA2010060291055Monitor · malfunctionedFLT 1219 CLT-DFW - REJECTED TAKEOFF - AIRCRAFT ABORTED TAKEOFF AT 135 KNOTS DUE TO LEFT ENGINE BIRD INGESTION WHICH CAUSED ENGINE TO SURGE. AIRCRAFT HAD TROUBLE STOPPING EVEN WITH MAX AUTOBRAKE. MAINTENANCE PERFORMED ENGINE BORESCOPE FOLLOWED BY POWER ASSURAJun 1, 2010 · N110UW · Airbus A320214 · Landing Gear Brake SystemSDR USAA2010033190684Actuator · malfunctionedFLT 1911 PHL-NAS - DIVERSION - ON DESCENT INTO NAS, CREW WAS UNABLE TO DEPLOY THE FLAPS - COULD ONLY EXTEND THE SLATS. AIRCRAFT DIVERTED TO FLL AND REGAINED FLAPS ON APPROACH. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND INBOARD FLAP TORQUE LIMITER INDMar 30, 2010 · N110UW · Airbus A320214 · Trailing Edge Flap Control SystemSDR USAA2010030890515Lens · missingFLT 1788 - ORD - EEL - LENS MISSING ON NR 2 RIGHT DOOR EMERGENCY EXIT LIGHT. MAINTENANCE REPLACED LENS ON NR 2 RIGHT DOOR EMERGENCY EXIT LIGHT.Mar 7, 2010 · N110UW · Airbus A320214 · Emergency LightingSDR USAA2009051391164Cylinder · low pressureFLT 1072 - PIT - EMERGENCY EQUIPMENT - LEFT AFT CREW DOOR EMERGENCY CYLINDER ACCUMULATOR PRESSURE LOW. MAINTENANCE SERVICED AFT CREW DOOR EMERGENCY CYLINDER ACCUMULATOR.May 12, 2009 · N110UW · Airbus A320214 · Passenger/Crew DoorsSDR USAA2008122292283Power Supply · inoperativeFLT 1162 PIT-BOS - EEL - RIGHT OVERWING EMERGENCY POWER SUPPLY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RIGHT OVERWING EMERGENCY POWER SUPPLY PACK. OPERATIONAL CHECK GOOD.Dec 19, 2008 · N110UW · Airbus A320214 · Emergency LightingSDR USAA920081387Strut · corrodedPIT- C11- MAJOR REPAIR - LT STRUT UPPER LEG HAS CORROSION AT BASE BLENDED CORROSION ON LT STRUT UPPER LEG FOUND TO BE OUT OF LIMITS. REPLACED LEFT GEAR ASSEMBLY IAW US AIRWAYS ROUTINE TASK CARD 26-3200-9-004. (A)Jul 8, 2008 · N110UW · Airbus A320214 · Main Landing Gear Strut/Axle/TruckSDR USAA920080908Controller · failedFLT 1697 - CLT-RSW - DIV - CREW REPORTED BOTH PACKS FAULTED SIMULTANEOUSLY AT FL 360 AND WOULD NOT RESET CAUSING AN EMERGENCY DESCENT. PACKS RESET THEMSELVES AUTOMATICALLY ON DESCENT, THEN FAULTED AGAIN CAUSING CABIN ALTITUDE WARNING. REACHED APPROX 10,200 FApr 21, 2008 · N110UW · Airbus A320214 · Cabin Pressure ControllerSDR USAA920071105Hydraulic System · lowFLT 1162 - SAN - PHX - EMERGENCY LANDING - CREW REPORTED ACARS 80 MILES OUT OF PHX LOSS OF GREEN HYDRAULIC SYSTEM RENDERING NOSE WHEEL STEERING INOP. CREW DECLARED AN EMERGENCY. AIRCRAFT WAS TOWED TO GATE. OPENNov 8, 2007 · N110UW · Airbus A320214 · Hydraulic System, MainSDR SA07053Slide · leakingTPA - THE L2 DOOR SLIDE PRESSURE WAS FOUND OUT OF GREEN BAND. MAINTENANCE REPLACED THE L2 DOOR ESCAPE SLIDE ASSEMBLY. INSPECTED OK FOR SERVICE.Aug 27, 2007 · N110UW · Airbus A320214 · Escape SlideSDR SA06042Lanyard · misinstalledPIT - THE R2 DOOR SURVIVAL KIT LANYARD WAS FOUND IMPROPERLY INSTALLED. MAINTENANCE INSTALLED THE LANYARD CORRECTLY. OK FOR SERVICE.Jun 15, 2006 · N110UW · Airbus A320214 · Emergency EquipmentSDR USAA051014Floorbeam · corrodedPIT - S2 - FLOORBEAM, 2 INCH X 6 INCH CORROSION, LEVEL 2; TASK JA-220-53500, 9 INCHES RT OF CENTER FROM FRAME C16 TO C21. REPLACED IAW SRM. (K)Aug 17, 2005 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA051013Clip · corrodedPIT - S2 - CLIP, 2 INCH X 1 INCH CORROSION; LEVEL 1; TASK JA-220-53500, FRAME C-20 AND AFT CORNER OF FWD SERVICE DOORWAY. REPAIRED WITH MANUFACTURED PART IAW SRM. (K)Aug 17, 2005 · N110UW · Airbus A320214 · Fuselage Main, Attach FittingsSDR USAA050977Floorbeam · corrodedPIT, S2, BEAM, .018, .028, .026, CORROSION; LEVEL 1 ASK JA-260-53500, FLOOR SUPPORT BEAM, FR66-68, Y1182 TO Y1292. DEVECTIVE PART REPLACED WITH IDENTICAL PART NUMBER. (K)Aug 5, 2005 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA050985Floorbeam · corrodedPIT - S2 - FLOORBEAM, 2 INCH X 36 INCH, CORROSION; LEVEL 1; TASK JA-260-53500, FLOOR SUPPORT BEAM FROM FR 68-66, IB AFT ENTRY DOOR. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (K)Aug 5, 2005 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA050982Floorbeam · corrodedPIT - S2 - FLOORBEAM, 2 INCH X 96 INCH, CORROSION; LEVEL 1; TASK JA-260-53500, FLOOR SUPPORT FR 64-70 IB AFT ENTRY DOOR. DEFECTIVE PART REPLACED WITH IDENTENTICAL PART IAW SRM. (K)Aug 5, 2005 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA050983Floorbeam · corrodedPIT - S2 - FLOORBEAM, 2 INCH X 2 INCH, 2 INCH X 2 INCH, 1.5 INCH X .5 INCH, CORROSION; LEVEL 1; TASK JA-220-53500, BETWEEN C18 AND C24 - Y1292. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM. (K)Aug 5, 2005 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA050981Floorbeam · corrodedA .7500 INCH DIA AREA OR LEVEL 1 CORROSION ON FLOORBEAM AT Y765 FR C-16. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM. (K)Aug 5, 2005 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA050980Floorbeam · corroded1 INCH OF CORROSION. NO LEVEL OR TASK, FRAME 66 Y-765 AT ATTACH FITTING. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM. (K)Aug 5, 2005 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA050979Floorbeam · corrodedPIT - S2 - FLOORBEAM, 1 IN DIA AND .7500 INCH DIA AREA, CORROSION; LEVEL 1; TASK JA-220-53500, FLOORBEAM AT Y765 BETWEEN C16 ADN C20. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM. (K)Aug 5, 2005 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA050978Floorbeam · corrodedPIT - S2 - BEAM, .5 INCHES X .5 INCHES, CORROSION; LEVEL 1; TASK JA-260-53500, FLOOR SUPPORT BEAM FR 66-68, Y1182 TO Y1292. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (K)Aug 5, 2005 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA050976Floor Support · corrodedPIT - S2 - FLOOR SUPPORT, 1 INCH DIA, CORROSION; LEVEL 1; TASK JA-220-53500, FLOOR SUPPORT, 8 INCHES RT OF CENTER AT C-20 AND C-21. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM. (K)Aug 5, 2005 · N110UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA050975Floorbeam · corrodedPIT - S2 - FLOORBEAM, 2 INCH X 3 INCH CORROSION, LEVEL 2; TASK: JA-220-53500 20 INCH LT OF CENTER AT FRAME C-16. REMOVED AND REPLACED IAW SRM. (K)Aug 5, 2005 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA050940Floorbeam · corrodedPIT - S2 - FLOORBEAM, 1 INCH DIA AREA CORROSION; LEVEL 1; TASK JA-260-53500, FLOOR SUPPORT BEAM, FR 66 AT RT AFT ENTRY DOOR. INSTALLED DOUBLERS/ REPAIR ANGELS IAW SRM. (K)Aug 3, 2005 · N110UW · Airbus A320214 · Fuselage Main, Floor BeamSDR SA05015Lanyard · looseCLT - PRIOR TO DEPARTURE, THE CABIN CREW COULD NOT GET ESCAPE SLIDE TO ARM AT DOOR 2R. MAINTENANCE SECURED A LOOSE LANYARD ON SLIDE AT 2R DOOR. SLIDE ARMING OPERATIONALLY CHECKS OK.Feb 5, 2005 · N110UW · Airbus A320214 · Escape SlideSDR USAASA04006Power Supply · failedDCA - FOUND INTERNAL FAULT ON LEFT EPSU. MAINTENANCE REPLACED THE EPSU. (M)Jan 17, 2004 · N110UW · Airbus A320214 · Emergency LightingSDR USAASA02093Power Supply · dischargedDCA- THE EMERGENCY LIGHT SYSTEM FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M)Oct 29, 2002 · N110UW · Airbus A320214 · Emergency LightingSDR USAASA02085Latch · brokenDCA - THE FORWARD, LEFT EMERGENCY EXIT SLIDE ACTUATING LATCH WAS FOUND BROKEN. MAINTENANCE REPLACED THE LATCH ASSEMBLY. ALSO REPLACED THE PIN GUIDE FITTING ASSEMBLY. OPS CHECKED OK. (M)Oct 12, 2002 · N110UW · Airbus A320214 · Emergency EquipmentSDR USAASA02068Slide · malfunctionedENROUTE, DURING FLIGHT, THE SERVICE DOOR BECAMED DISARMED. THE RED WARNING LIGHT FLASHES CONTINUOUSLY IN CABIN DOORS AND CABIN INTERCOM DATA SYSTEM. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FORWARD SERVICE DOOR SLIDE ASSEMBLY. OPS CAug 8, 2002 · N110UW · Airbus A320214 · Escape SlideSDR USAA010507Skin · crackedDCA - FOUND FUSELAGE SKIN CRACKED 4 INCHES, JUST AFT OF FRAME NR 79, BETWEEN STRINGER 1R AND 2R. INSTALLED REPAIR DOUBLER PER SRM 53-00-11 PAGE 209/210. (M)May 7, 2001 · N110UW · Airbus A320214 · Fuselage Main, Plate/SkinSDR USAA010458Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED 4 INCHES, FRAME 79 JUST AFT OF BETWEEN S1R AND S2R. INSTALLED DOUBLER PER SRM 53-00-11, PAGE 209/210. (M)Apr 25, 2001 · N110UW · Airbus A320214 · Fuselage Main, Plate/Skin
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