N122US

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 = 'N122US' 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 USAA2012031300011Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, Z-500, Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, Z-500, Y765 IAW A320 SRM 53-41-15 FIG 102 & # EA 201988.Mar 2, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012031300010Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Z-500, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Z-500, Y765 IAW A320 SRM 53-41-15 FIG 102 & # EA 201988.Mar 2, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012031200017Beam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON Z-BEAM BETWEEN FR66.6 TO FR68.6, Z-500 & BETWEEN Y1162.5 TO Y1292. REPLACED Z-BEAM BETWEEN FR66.6 TO FR68.6, Z-500 & BETWEEN Y1162.5 TO Y1292 IAW A320 SRM 53-41, 51-42-11, 51-72-11 & EA # 201988.Mar 2, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012031200016Sill · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON DOOR SILL AT FR66, Z-500, Y1589. REPLACED DOOR SILL AT FR66, Z-500, Y1589 IAW A320 SRM 51-42-11.Mar 2, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012031200012Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67.5, Z-500, Y512.5. REPLACED FLOORBEAM BETWEEN FR64 TO FR67.5, Z-500, Y512.5 IAW A320 SRM 51-42-11, 51-43-11 & EA # 201988.Mar 2, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012031200010Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68-6 INCHES TO FR69+4 INCHES, Z-500, Y1162.5. REPLACED FLOORBEAM BETWEEN FR68-6 INCHES TO FR69+4 INCHES, Z-500, Y1162.5 IAW A320 SRM 51-42-11, 51-72-11 & EA # 201988.Mar 2, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012031200006Shear Plate · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1162.5. REPLACED SHEAR PLATE BETWEEN FR68 TO FR69, -Y1162.5 IAW A320 SRM 53-41-14 FIG 2 ITEM 15A & TYPICAL REPAIR # TR320-2528-10-0011C.Mar 2, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012030900003Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM APPROX 1 INCH FORWARD OF FR16, Z-500, Y503.2. REPLACED FLOORBEAM AT FR16, Z-500, Y503.2 IAW A320 SRM 51-72-11.Mar 2, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012030800002Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR21, Z-500, Y1292. REPLACED FLOORBEAM BETWEEN FR16 TO FR21, Z-500, Y1292 IAW A320 SRM 51-42-11 & 51-21-11.Mar 2, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012030500016Sill · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON SHAPE SILL BETWEEN FR66+4 INCHES TO FR68-4 INCHES. REPLACED SHAPE SILL BETWEEN FR66+4 INCHES TO FR68-4 INCHES IAW A320 SRM 51-72-11.Mar 2, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012031500002Sill · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON DOOR SILL AT FR66, Z-500, -Y1589. REPLACED DOOR SILL AT FR66, Z-500, -Y1589 IAW A320 EA 201968 & A320 SRM 53-41-14.Mar 1, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012031500001Sill · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON R2 DOOR SILL PLATE AT FR68, Z-500, -Y1292. REPAIRED R2 DOOR SILL PLATE AT FR68, Z-500, -Y1292 IAW A320 EA 201968.Mar 1, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012031300006Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1162 IAW A320 SRM 51-72-11.Mar 1, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012031200013Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Z-500, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, Z-500, -Y1292 IAW A320 SRM 51-72-11.Mar 1, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012031200011Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Z-500, -Y1292.5. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Z-500, -Y1292 IAW A320 SRM 51-72-11.Mar 1, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012031200015Seat Track · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR64 TO FR66, -Y765. REPLACED SEAT TRACK BETWEEN FR64 TO FR66, -Y765 IAW A320 SRM 53-00-14 FIG 102, 51-72-11 & EA # 201988.Mar 1, 2012 · N122US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2012031200008Shear Plate · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Z-500, Y1292. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Z-500, Y1292 IAW A320 SRM 51-72-11.Mar 1, 2012 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA2012030900009Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66+6 INCHES, Z-500, Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66+6 INCHES, Z-500, Y1292 IAW A320 SRM 51-42-11 & 51-44-11.Mar 1, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012030900004Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR12 TO FR16, Z-500, -Y81. REPLACED FLOORBEAM BETWEEN FR12 TO FR16, Z-500, -Y81 IAW A320 SRM 51-42-11.Mar 1, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012030900001Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR67, Z-500, -Y464.8. REPLACED FLOORBEAM BETWEEN FR66 TO FR67, Z-500, -Y464.8 IAW A320 SRM 51-72-11.Mar 1, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012030800004Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR20 TO FR21, Z-500, -Y189. REPLACED FLOORBEAM BETWEEN FR20 TO FR21, Z-500, -Y189 IAW A320 SRM 51-72-11 & 51-42-11.Mar 1, 2012 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA2012011200010Ball Lock · obstructedNEW OVERHAULED SLIDE ARRIVED FROM VENDOR WITH ENCLOSURE BALL LOCKS PAINTED OVER RENDERING SLIDE UNSERVICEABLE. MAINTENANCE ACCOMPLISHED E/O #2508Y025 PAINT REMOVAL FROM THE OVERWING SLIDE ENCLOSURE BALL LOCKS MAKING SLIDE SERVICEABLE AGAIN.Jan 11, 2012 · N122US · Airbus A320214 · Escape SlideSDR USAA2011101900005Mechanism · obstructedCREW REPORTED FORWARD SERVICE DOOR ARMING HANDLE BINDS IN THE ARMING PROCESS. MAINTENANCE CLEARED DEBRIS FROM GIRT BAR ATTATCH MECHANISM.Oct 18, 2011 · N122US · Airbus A320214 · Emergency EquipmentSDR USAA2011071500004Uplock · stuckLOUDER THAN USUAL WIND NOISE THAT APPEARED TO BE COMING FROM NOSE GEAR OR RADOME AREA AT ALL ALTITUDES AND AIRSPEEDS OVER 220 KTS. DURING LATTER STAGE OF FLIGHT, NOTICED AMBER X'S AT NOSE GEAR DOOR POSITION INDICATOR. FOUND NLG DOOR UPLOCK STUCK IN CLOSED POJul 14, 2011 · N122US · Airbus A320214 · Landing Gear Door Retract SectionSDR USAA2010051890981Lens · missingLOG PAGE 4662621 - FLT 894-ATL - EEL - EMERGENCY LIGHT LENS MISSING RT FORWARD OVERWING EXIT. MAINTENANCE INSTALLED EMERGENCY LIGHT LENS RT FORWARD OVERWING EXIT.May 17, 2010 · N122US · Airbus A320214 · Emergency LightingSDR USAA2009071591833Lens · missingFLT 958 - ORD - EEL - LENS FOR R2 DOOR LOWER EMERGENCY EXIT LIGHT MISSING. REPLACED MISSING LENS IAW AIRBUS MAINTENANCE MANUAL 33-51-13-04-400-001.Jul 14, 2009 · N122US · Airbus A320214 · Emergency LightingSDR USAA2009061191460O-Ring · leakingFLT 977 CLT-PDX - RETURN TO FIELD - CREW REPORTED LOSS OF YELLOW HYDRAULIC SYSTEM. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED O-RING ON BRAKE AUTOMATIC SELECTOR 2576GM. SERVICED SYSTEM AND OPERATED WITH NO LEAKS NOTEDJun 10, 2009 · N122US · Airbus A320214 · Master Cylinder/Brake ValveSDR USAA2009021690339Cylinder · low pressureLOG PAGE 4260655 FLT NR 1723 CLT-FLL EMERGENCY EQUIPMENT L2 DOOR ASSIST LOW PRESSURE. MX SERVICED THE L2 DOOR ASSIST BOTTLE PER AIRBUS MM 52-10-00-614-001.Feb 13, 2009 · N122US · Airbus A320214 · Passenger/Crew DoorsSDR USAA920080605Diaphragm · defectiveFLT 9225 - MBJ-CLT - R2 DOOR WOULD NOT MOVE WITH NORMAL PRESSURE. MAINTENANCE REPLACED THE DIAPHRAGM IN THE PERCUSSION MECHANISM OF THE RIGHT AFT DOOR DAMPER AND EMERGENCY OPERATION CYLINDER. DOOR OPERATION NORMAL.Mar 10, 2008 · N122US · Airbus A320214 · Passenger/Crew DoorsSDR SA06033None · odorFLIGHT 103, CLT-MSY, RUBBER ODOR FROM ROW 6 AFTER, NEVER DISSIPATED FOR ENTIRE FLIGHT. MAINTENANCE CREW RAN SYSTEM ON APU AND ENGINES, ISOLATED PROBLEM TO RIGHT PACK. RELEASED PER MEL. RAN BOTH PACKS, AND COULDN'T DUPLICATE BURNING ODOR. CABIN DOES HAVE A Apr 30, 2006 · N122US · Airbus A320214 · Air Distribution SystemSDR USAA060637Floorbeam · corrodedFOUND FLOORBEAM CORRODED -Y1292 STA 66 - 68. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-11-15, DWG 53474180, DEFECT SIZE: 2" BY 60" BY .100".Apr 27, 2006 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA060636Seat Track · corrodedFOUND TRACK CORRODED Y254 AT 16 TRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-11-15; CORRODED TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 2" BY 2" BY .100".Apr 27, 2006 · N122US · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USAA060635Shear Tie · corrodedFOUND RT SHEAR TIE PLATE AT STA 69 CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-11-15; TASK NR JA-260-53500, DEFECT SIZE: 1/4" BY 1/4" BY 1/4".Apr 27, 2006 · N122US · Airbus A320214 · Fuselage Internal Mounting StructureSDR USAA060634Floorbeam · corrodedFOUND FLOORBEAM CORRODED Y1292 STA 66 - 68. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-11-15, DWG D53474180; CORROSION TASK JA-260-53500, DEFECT SIZE: 2" BY 60" BY .100".Apr 27, 2006 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA060629Floorbeam · corrodedFOUND CORROSION ON BEAM AT -Y254 C18 AND C16. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-11-15; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 1-1/2" BY 1-1/2" BY .040".Apr 27, 2006 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA060638Floorbeam · corrodedFOUND CORROSION FLOORBEAM AT Y1292 LEFT FRAME 66-68. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-72-11; CORR TASK JA-260-53500; LEVEL 1, DEFECT SIZE: 2 AREAS - 1" DIA AND 1" BY 2".Apr 27, 2006 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA060605Sill · corrodedFOUND CORROSION RT AFT DOOR SILL STA 66. CUT OUT AND INSTALLED ANGLES PER SRM 53-41-14; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1/4" BY 1/4" BY .090".Apr 21, 2006 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA060604Floorbeam · corrodedFOUND FLOORBEAM CORRODED, TOP SIDE. REPLACED FLOORBEAM PER SRM 51-72-11L, CORROSION LEVEL 1; TASK JA-220-53500, DEFECT SIZE: 1" BY 1".Apr 21, 2006 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA060603Sill · corrodedFOUND CORROSION STA 66 LT AFT DOOR SILL. CUT OUT, PUT IN FILLER PER SRM 53-41-00 REP. 06; CORROSION LEVEL 1, TASK JA-260-53500, DEFECT SIZE: 1" BY 4".Apr 21, 2006 · N122US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA060602Floorbeam · corrodedFOUND FLOORBEAM CORRODED 2 AREAS, AT Y 1292 LEFT FRAME 66 - 68. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORROSION LEVEL 2; TASK JA-260-53500, DEFECT SIZE: 1" DIAMETER AND 1" AND 2".Apr 21, 2006 · N122US · Airbus A320214 · Fuselage Main, Floor BeamSDR SA05115Epsu · faultyPHL - THE EMERGENCY LIGHTS FAILED THE SYSTEM TEST. MAINTENANCE REPLACED THE MIDDLE, RIGHT EMERGENCY POWER SUPPLY UNIT (FIN 12WL). OPERATIONALLY CHECKS OK.Nov 15, 2005 · N122US · Airbus A320214 · Emergency LightingSDR SA05081Slide · unsecureTHE L1 DOOR SLIDE BECAME PARTIALLY UNSTOWED DURING THE CLOSING OF THE DOOR. MAINTENANCE REMOVED AND THEN INSTALLED THE SAME GIRT BAR. OPERATIONAL CHECKS NORMAL.Jun 28, 2005 · N122US · Airbus A320214 · Escape SlideSDR SA05068Epsu · faultyPIT - THE EMERGENCY LIGHTS SYSTEM TESTED INOPERATIVE. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.Jun 11, 2005 · N122US · Airbus A320214 · Emergency LightingSDR SA05067Epsu · faultyPIT - THE EMERGENCY LIGHTS SYSTEM TESTED INOPERATIVE. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT AND BATTERIES. OPERATIONALLY CHECKS OK.Jun 11, 2005 · N122US · Airbus A320214 · Emergency LightingSDR USAASA04016Power Supply · faultyPHL - THE MID CABIN, LEFT EMERGENCY POWER SUPPLY UNIT WAS FAULTING DURING TEST. MAINTENANCE REPLACED THE MID CABIN, LEFT EMERGENCY POWER SUPPLY UNIT. (M)Feb 16, 2004 · N122US · Airbus A320214 · Emergency LightingSDR USAASA03059Slide · destroyedTHE RT FORWARD SLIDE FELL APART WHEN COVER WAS REMOVED. MAINTENANCE REPLACED THE ESCAPE SLIDE. OK FOR SERVICE. (M)Jun 2, 2003 · N122US · Airbus A320214 · Escape SlideSDR USAASA03001Door · stuckCLT - FLT 654 - EN ROUTE AUA-PHL, WHILE IN FLIGHT, THE COCKPIT DOOR WOULD NOT OPEN. THE CIRCUIT BREAKER CONTROLLING THE COCKPIT DOOR LOCKS WAS PULLED, HOWEVER, THE DOOR STILL REMAINED STUCK CLOSED. A CREW MEMBER THEN TRIED TO EXIT THE COCKPIT THROUGH THE EMEJan 1, 2003 · N122US · Airbus A320214 · Fixed Inner Doors
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