N178US

Service difficulty reports · 347

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 = 'N178US' 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 USAA2013062800016Floor Support · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR24, -Y254. REPLACED FLOOR SUPPORT BETWEEN FR12 TO FR24, -Y254 IAW SRM 51-74-00, 51-11-14 & 51-42-11.Jun 20, 2013 · N178US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013062800014Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR64 TO FR66, -Y765. REPLACED SEAT TRACK BETWEEN FR64 TO FR66, -Y765 IAW SRM 53-00-14, FIG 102 & 51-42-11.Jun 20, 2013 · N178US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013062800013Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y1292 IAW SRM 53-11-15 FIG 102 & 51-42-11.Jun 20, 2013 · N178US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013062800011Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y765 IAW SRM 51-42-11, 51-74-00, 53-11-15, 51-44-11.Jun 20, 2013 · N178US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013062800010Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y254. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y254 IAW SRM 53-11-14, FIG 104 & 51-42-11.Jun 20, 2013 · N178US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013062800009Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT TRACK BETWEEN FR20 TO FR21, -Y198. REPLACED FLOOR SUPPORT TRACK BETWEEN FR20 TO FR21, -Y198 IAW SRM 51-42-11, 53-11-14 & 51-75-12.Jun 20, 2013 · N178US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013062800008Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, Y160. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, Y160 IAW A321 SRM 53-00-14 FIG 102 & 51-42-11.Jun 20, 2013 · N178US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA2013062800019Floor Support · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR68 TO FR70, -Y254. REPLACED FLOOR SUPPORT BETWEEN FR68 TO FR70, -Y254 IAW SRM 53-41-14, 53-00-14, 51-42-11 & 51-44-11.Jun 19, 2013 · N178US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013070900023Web · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT WEB AT FR16, -Y1379. REPLACED SUPPORT WEB AT FR16, -Y1379 IAW SRM 51-42-11.Jun 15, 2013 · N178US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013070900012Floor Support · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BEAM BETWEEN FR65 TO FR67, -Y318. REPLACED FLOOR SUPPORT BEAM BETWEEN FR65 TO FR67, -Y318 IAW SRM 53-00-14, 51-42-11 & 51-75-12.Jun 15, 2013 · N178US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013070900024Angle · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT ANGLE AT FR20, -Y1732. REPLACED FLOOR SUPPORT ANGLE AT FR20, -Y1732 IAW SRM 51-42-11.Jun 14, 2013 · N178US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013070900022Stiffener · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON STIFFENER AT FR12, -Y254. REPLACED STIFFENER AT FR12, -Y254 IAW A321 SRM 51-42-11 & SRM 51-75-12.Jun 14, 2013 · N178US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013062800012Seat Track · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW SRM 51-42-11 & 53-11-14.Jun 14, 2013 · N178US · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2013070900011Floor Support · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BEAM BETWEEN FR20 TO FR24, -Y1584. REPLACED FLOOR SUPPORT BEAM BETWEEN FR20 TO FR24, -Y1584 IAW SRM 53-00-14, 51-42-11, & 51-44-11.Jun 13, 2013 · N178US · Airbus A321211 · Fuselage Miscellaneous StructureSDR USAA2013011000022Relay · defectiveWHEN STARTING APU, EMERGENCY LIGHT CABIN (H-7) CIRCUIT BREAKER POPPED - ON POWER TRANSFER, H-10 CIRCUIT BREAKER ALSO POPPED. REMOVED AND REPLACED CONTROL RELAY 21XG IAW ELECTRICAL STANDARD PRACTICES MANUAL & EWM 24-41-03.Jan 9, 2013 · N178US · Airbus A321211 · External Power SystemSDR USAA2012112700031Power Supply · inoperativeEXIT 3R EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT IAW AIRBUS MAINTENANCE MANUAL 33-51-38-000-002A.Nov 26, 2012 · N178US · Airbus A321211 · Emergency LightingSDR USAA2012100800010Power Supply · inoperativeEMERGENCY EXIT LIGHT AT DOOR 3R DOES NOT ILLUMINATE WITH SWITCH ON. REMOVED AND REPLACED POWER SUPPLY FOR 3R DOOR LIGHT IAW AIRBUS MAINTENANCE MANUAL 33-51-38-000-002A.Oct 7, 2012 · N178US · Airbus A321211 · Emergency LightingSDR USAA2012090500057Dampener · low pressureEMERGENCY EXIT DOOR DAMPER LOW PRESSURE AT 3L DOOR. SERVICED EMERGENCY DOOR DAMPER AT 3L DOOR IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002-A.Sep 2, 2012 · N178US · Airbus A321211 · Emergency ExitsSDR USAA2012090500056Damper · low pressureEMERGENCY EXIT DOOR DAMPER LOW PRESSURE AT 2R DOOR. SERVICED EMERGENCY DOOR DAMPER AT 2R DOOR IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002-A.Sep 2, 2012 · N178US · Airbus A321211 · Emergency ExitsSDR USAA2012090500055Damper · low pressureEMERGENCY EXIT DOOR DAMPER LOW PRESSURE AT 2L DOOR. SERVICED EMERGENCY DOOR DAMPER AT 2L DOOR IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002-A.Sep 2, 2012 · N178US · Airbus A321211 · Emergency ExitsSDR USAA2012050700012Line · brokenNR 1 ENGINE FIRE EXTINGUISHER LINE IS BROKEN JUST AFT OF FORWARD MOUNT. INSTALLED SERVICEABLE FIRE EXTINGHISHER LINE IAW MM 26-21-49-400.May 4, 2012 · N178US · Airbus A321211 · Extinguishing SystemSDR USAA2012010900028Ecs · contaminatedA STRONG MUSTY ODOR WAS REPORTED THROUGHOUT CABIN AND COCKPIT AFTER ENGINE START. AIRCRAFT RETURNED TO GATE AND FLIGHT CREW DONNED OXYGEN MASKS. MAINTENANCE PERFORMED DECONTAMINATION OF ENVIRONMENTAL CONTROL SYSTEM. NO ODORS NOTED.Jan 8, 2012 · N178US · Airbus A321211 · Air Distribution SystemSDR USAA2011121300007Extinguisher · low pressureFORWARD LAV TRASH CAN FIRE EXTINGUISHER BOTTLE GAUGE SHOWS EMPTY. REMOVED AND REPLACED FORWARD LAV TRASH CAN FIRE EXTINGUISHER IAW AIRBUS MAINTENANCE MANUAL 26-25-41-400-001 AND 26-25-41-000-001.Dec 12, 2011 · N178US · Airbus A321211 · Fire Bottle, FixedSDR USAA2011071900005Lens · missingLIGHT COVER FOR EMERGENCY EXIT LIGHT 3L DOOR MISSING. INSTALLED MISSING EMERGENCY EXIT LIGHT LENS AT DOOR 3L.Jul 18, 2011 · N178US · Airbus A321211 · Emergency LightingSDR USAA2011040191308Power Supply · inoperativeMX-CLT - EEL - EMERGENCY POWER SUPPLY UNIT MID RIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT IAW AIRBUS MAINTENANCE MANUAL 33-51-38.Mar 31, 2011 · N178US · Airbus A321211 · Emergency LightingSDR USAA2011032891255Connector · looseFLT 1790 - LAS - EEL - CREW REPORTED EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROW 9 RIGHT SIDE AFT POSITION. MAINTENANCE FOUND LOOSE CONNECTOR AT ROW 10 A/C RIGHT SIDE WALL. RECONNECTED AND TESTED IAW AIRBUS MAINTENANCE MANUAL 33-51-00.Mar 26, 2011 · N178US · Airbus A321211 · Light System WiringSDR USAA2011020890581Skin · saturatedPIT - GEAR CHANGE - MAJOR REPAIR - WATER INCLUSION ON RIGHT ELEVATOR UPPER SURFACE AT 124 INCHES FROM INBOARD EDGE & 17 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE AT 124 INCHES FROM INBOARD EDGE & 17 INCHES FROM TRAILING EDGE IAW A321 SRFeb 5, 2011 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR USAA2011020890595Rib · corrodedPIT - GEAR CHANGE - MAJOR REPAIR - CORROSION IN RIGHT WING RIB AFT PINTLE PIN RIB 5 BORE AT WSTA 2580/RIB 5. REPAIRED RIGHT WING RIB AFT PINTLE PIN RIB 5 BORE AT WSTA 2580/ RIB 5 IAW EA 117170.Feb 5, 2011 · N178US · Airbus A321211 · Wing, Rib/BulkheadSDR USAA2011020890585Skin · saturatedPIT - GEAR CHANGE - MAJOR REPAIR - WATER INCLUSION ON RIGHT ELEVATOR UPPER SURFACE 57 INCHES FROM INBOARD END & 13 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE 57 INCHES FROM INBOARD END & 13 INCHES FROM TRAILING EDGE IAW A321 SRM 55-21-11Feb 5, 2011 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR USAA2011020890582Skin · saturatedPIT - GEAR CHANGE - MAJOR REPAIR - WATER INCLUSION ON RIGHT ELEVATOR UPPER SURFACE 40 INCHES FROM INBOARD END & 13 INCHES FROM TRAILING EDGE. REPAIRED RIGHT ELEVATOR UPPER SURFACE 40 INCHES FROM INBOARD END & 13 INCHES FROM TRAILING EDGE IAW A321 SRM 55-21-11.Feb 5, 2011 · N178US · Airbus A321211 · Elevator, Plate/SkinSDR USAA2011010490037Lens · missingFLT 1776 - BOS - EEL - R-4 DOOR EMERGENCY LIGHT LENS COVER MISSING. MAINTENANCE REPLACED MISSING EMERGENCY LIGHT LENS COVER ON R-4 DOOR.Jan 1, 2011 · N178US · Airbus A321211 · Emergency LightingSDR USAA2010091491986Oil System · overservicedFLT 1433 CLT - LAX - RTF - DURING CLIMB, RIGHT ENGINE OIL TEMP BEGAN FLASHING AT 130. STOPPED CLIMB AT 25000FT AND TEMP INCREASED TO 145 FOR 9 MINUTES. TEMP BEGAN TO DECREASE AT DESCENT POWER AND STABILIZED AT 120. CREW DECLARED AN EMERGENCY AND RETURNED TOSep 13, 2010 · N178US · Airbus A321211 · Engine Oil Storage (Airframe Furnished)SDR USAA2010081791689Actuator · low pressureFLT 1538 - BOS - EES - EMERGENCY EXIT DOOR "AFT (R)" REQUIRES SERVICING. MAINTENANCE ACCOMPLISHED CHARGING PROCEDURE OF EMERGENCY EXIT DOOR "AFT (R)" IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.Aug 16, 2010 · N178US · Airbus A321211 · Emergency ExitsSDR USAA2010081791688Actuator · low pressureFLT 1538 - BOS - EES - EMERGENCY EXIT DOOR "MID (L)" REQUIRES SERVICING. MAINTENANCE ACCOMPLISHED CHARGING PROCEDURE OF EMERGENCY EXIT DOOR "MID (L)" IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-001.Aug 16, 2010 · N178US · Airbus A321211 · Emergency ExitsSDR USAA2010080991619Epsu · inoperativeFLT 1538 - CLT-BOS - EMERGENCY LIGHTS - L2 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT AT L2 DOOR MID OVERHEAD PER AMM 33-51-38.Aug 6, 2010 · N178US · Airbus A321211 · Emergency LightingSDR USAA2010080491591Light · inoperativeFLT 964 - SFO - PHL - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHT ON DOOR 2L BURNT OUT. FOUND EMERGENCY EXIT LIGHT ON L2 DOOR WORKING BUT L1 DOOR EMERGENCY LIGHT BURNT OUT AND REPLACED AS REQUIRED PER AMM TASK 33-51-16-04-000/400.Aug 3, 2010 · N178US · Airbus A321211 · Emergency LightingSDR USAA2010031590575Cover · missingFLT 701 - LAX - EEL - AFT LEFT ENTRY DOOR EMERGENCY EXIT LIGHT COVER MISSING. MAINTENANCE INSTALLED COVER AS REQUIRED.Mar 14, 2010 · N178US · Airbus A321211 · Emergency LightingSDR USAA2010010790042Lens · missingFLT 1529 - DEN - EEL - SEAT MOUNTED EMERGENCY LIGHT LENS IS MISSING AT SEAT 12ABC. MAINTENANCE INSTALLED NEW LENS IAW AIRBUS MAINTENANCE MANUAL 33-51-19.Jan 6, 2010 · N178US · Airbus A321211 · Emergency LightingSDR USAA2009011590077Sensor · faultyLOG PAGE 8366438 - FLT NR 1511 PHX-LAX - EMERGENCY LANDING - CREW RECEIVED A HOT BRAKE ECAM MSG IMMEDIATELY AFTER TAKEOFF. NR 3 BRAKE TEMP CONTINUED TO INCREASE TO 995C THEN CHANGED TO AMBER XX'S. ACFT CONTINUED WITH GEAR EXTENDED IAW QRH AND CAPTAIN DECLAREJan 13, 2009 · N178US · Airbus A321211 · Landing Gear Brake SystemSDR USAA2009011490070Power Supply · dischargedEMERGENCY LIGHTS FAILED CIDS TEST - SHOWED "EPSU UNIT EXIT L". MX R&R EMERGENCY POWER SUPPLY UNIT 11WL PER MM 33-51-38. OPS CHECK GOOD.Jan 13, 2009 · N178US · Airbus A321211 · Emergency LightingSDR USAA070414Floorbeam · corrodedEXFOLIATION AT FR 16 ON TOP OF FLOORBEAM Y254. FLOORBEAM REMOVED & REPLACED PER SRM 51-72-11; CORR TASK JA-220-53500; LEVEL 1, DEFECT SIZE: 1 X 2 INCHES.May 25, 2007 · N178US · Airbus A321211 · Fuselage Main, Floor BeamSDR USAA070415Shear Plate · corrodedLEFT SHEAR TIE PLATE FRAMES 69 - 70 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL. CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 5 X 17 INCHES.May 25, 2007 · N178US · Airbus A321211 · Fuselage Main, StructureSDR USAA200705U12Beam · corrodedA 1.125 X 2 INCH CORROSION FOUND AT RIGHT AFT SILL BEAM. REPAIRED PER SRM 53-41-14. CORROSION TASK JA-260-53500, CORR LEVEL 1.May 24, 2007 · N178US · Airbus A321211 · Fuselage Main, StructureSDR USA2007F00000Structure · corrodedCORRODED RIVET TAILS WERE FOUND IN FUSELAGE CARGO COMPARTMENT BETWEEN FRAME 35.1 TO 35.7, STRINGER 39L TO 39R. APPROXIMATELY 1,000 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FLAKING OFF THE RIMay 18, 2007 · N178US · Airbus A321211 · Fuselage Main, StructureSDR SA06054Epsu · faultyTHE EMERGENCY LIGHT SYSTEM FAILED OPERATIONAL TEST WITH FAILURE MESSAGE (EPSU UNIT EXIT R). MAINTENANCE REPLACED THE MID-CABIN, RT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.Jul 22, 2006 · N178US · Airbus A321211 · Emergency LightingSDR SA04091Epsu · faultyRECEIVED LEFT FWD MID EXT SLIDE LIGHTS FAULT. MAINTENANCE REPLACED THE LEFT MID CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.Sep 28, 2004 · N178US · Airbus A321211 · Emergency LightingSDR USAASA01042Odor · detectedPHL - FLT 8 - EN ROUTE LAX-PHL, THE CABIN CREW REPORTED AN ODOR DURING FLIGHT. THE ODOR DISSIPATED AND THE FLIGHT LANDED WITHOUT INCIDENT IN PHL. MAINTENANCE INSPECTED THE GALLEYS AND RAN THE AIR CONDITIONING PACKS. NO ODORS WERE DETECTED. OK FOR SERVICE. Aug 13, 2001 · N178US · Airbus A321211 · Air Distribution System
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