N321US

Service difficulty reports · 204

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 = 'N321US' 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 DALA2021041202117Psu · no testSHIP 3221 DURING TEST AFT F/A LH PSU PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7594654)Apr 10, 2021 · N321US · Airbus A320211 · Emergency EquipmentSDR DALA2021041202116Psu · no testSHIP 3221 DURING TEST SEAT 1CD PSU PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7594653)Apr 10, 2021 · N321US · Airbus A320211 · Emergency EquipmentSDR DALA2021022401069Housing · damagedSHIP 3221 EMERGENCY PATH LIGHT HOUSING DAMAGED AT ROW 21R. CORRECTIVE ACTION: RESECURED EMERGENCY LIGHT TO HOUSING ASSY AT SEAT 21R AS PER A320 CMM 25-23-51. OK FOR SERVICE. (4055027)Feb 24, 2021 · N321US · Airbus A320211 · Emergency LightingSDR DALA2021021600860Psu · no testSHIP 3221 DURING TEST FOUND SEAT 22ABC PSU OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPS CK GOOD. (7546393)Feb 15, 2021 · N321US · Airbus A320211 · Emergency EquipmentSDR DALA2021021600859Psu · no testSHIP 3221 DURING TEST FOUND SEAT 2ABC PSU OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPS CK GOOD. (7546392)Feb 15, 2021 · N321US · Airbus A320211 · Emergency EquipmentSDR DALA2021020200632Switch · malfunctionedSHIP 3221 ALL 4 DOORS SHOW RED PRESSURE LIGHT AT BLOCK END. REPEAT WRITE UP. CORRECTIVE ACTION: R/R CABIN PRESSURE DETECTION SWITCH PER A320 AMM 52-73 OPS CHECK GOOD. (7526744)Jan 13, 2021 · N321US · Airbus A320211 · Door Warning SystemSDR DALA2021010500045Probe · malfunctionedDURING DESCENT, ABOUT FL300, LEFT FUEL QUANTITY WAS ABOUT 1,000 LBS LOW, GOT LEFT FUEL QTY LOW ECAM. THE LEFT TANK WAS LOW AND WAS SLOW TO TRANSFER FROM OUTER TANK TO INNER TANK. REQUESTED PRIORITY HANDLING BY ATC. CORRECTIVE ACTION: NEEDS PROBE MFG P/N 021Dec 31, 2020 · N321US · Airbus A320211 · Fuel Indicating SystemSDR DALA2022111007262Stop Fitting · crackedSHIP 3221 ERA 585867-14AD REVISED TO REV 'A'. SECTION I ISSUED FOR CRACK FINDINGS AT HOLES 5, 6, A, B, E, AND F AT FR16 DOOR-STOP. CORRECTIVE ACTION: COMPLIED WITH REVISION. (1609685)Sep 6, 2020 · N321US · Airbus A320211 · Fuselage Main, StructureSDR DALA2022111007261Stop Fitting · crackedSHIP 3221 ERA 585867-14AD REVISED TO REV 'A'. SECTION I ISSUED FOR CRACK FINDINGS AT HOLES 5, 6, A, B, E, AND F AT FR16 DOOR-STOP. CORRECTIVE ACTION: COMPLIED WITH ERA 585867-14. (1609684)Sep 6, 2020 · N321US · Airbus A320211 · Fuselage Main, StructureSDR DALA202008112759Linkage · lack of lubeFWD CARGO DOOR SHOWED OPEN DURING CRUISE. FAULTING THE HANDLE PROX SENSOR 28WV. LUBRICATED THE HANDLE FLAP LINKAGE. CHECKED GOOD IAW AMM 52-31.Aug 5, 2020 · N321US · Airbus A320211 · Cargo/Baggage DoorsSDR DALA2020051302394Frame · crackedCRACK INDICATION ON FRAME 16 LH SIDE DOUBLE JOGGLE AREA OPEN FASTENER HOLE A, CRACK DIRECTION IS 3 OCLOCK, AT FWD GALLEY AREA (1 EA), PERFORMED REPAIR INSTRUCTIONS ON FR.16 L/H SIDE AS PER ER/A 585862-14AD REV. ORIGINAL AND PRI 585862-14AD REV.0, REV.1, REV.2May 13, 2020 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020051302395Damper · failedOPERATIONAL TEST PASSENGER CREW DOOR 831 DOOR DAMPER AT FWD GALLEY AREA DID NOT PASS, REPLACED DOOR DAMPER PASS/CREW DOOR 831 AS PER A320 FAM AMM 52-11-14-400-001-A AND CHECKED CORRECT DAMPER OPERATIONMay 12, 2020 · N321US · Airbus A320211 · Passenger/Crew DoorsSDR DALA2020051302393Hinge Fitting · crackedCRACK DOOR ON HINGE ARM FITTING ASSY #4 TRAILING EDGE ON VERTICAL STABILIZER (1 EA), PERFORMED PERMANENT REPAIR ON DOOR HINGE ARM FITTING ASSY #4 TRAILING EDGE ON VERTICAL STABILIZER (1EA) ASPER A320 SRM 55-36-42-300-003May 12, 2020 · N321US · Airbus A320211 · Vertical StabilizerSDR DALA2020050802377Structure · corrodedCORROSION INTERNAL STRUCTURE SECTION CONNECTION AT FRAME67 AND STRINGER 30 RIGHT UNDERFLOOR BAY IN AFT CARGO COMPARTMENT (1 EA), REPLACED INTERNAL STRUCTURE SECTION CONNECTION (1EA) LOC FR67 AND STR 30R UNDERFLOOR BAY IN AFT CARGO COMPARTMENT ASPER SRM 51-42-1May 3, 2020 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020050802376Damper · unserviceable841 DOOR DAMPER AT FWD GALLEY AREA DONT PASS OPERATIONAL TEST, REPLACED CYLINDER DOOR DAMPER IN UNSERVICEABLE CONDITION P/N FE174-004 S/N 129 AT CREW DOOR 841 AS PER FAM AMM 52-11-14- 000-001-AMay 1, 2020 · N321US · Airbus A320211 · Passenger/Crew DoorsSDR DALA2020043002323Frame · corrodedCORROSION ON FR 16 AT LEVEL OF STRINGER 23R/H SIDE, PERFORMED PERMANENT REPAIR ON FR 16 AT LEVEL OF STRINGER 23R/H SIDE AS PER PRI 522853-14 REV O, REV 1,REV 2,REV 3 AND ER/A 522853-14 REV "C"Apr 28, 2020 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020043002319Frame · crackedCRACK INDICATION ON FRAME 36 , CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 1 AT FR 36, PERFORMED REPAIR AT CWB FRONT SPAR VERTICAL STRINGER POSITION 1 AT FR 36 AT HOLE ZONE 1 (INB SIDE) Y1292 IN FWD CARGO COMPARTMENT AS PER PRI 585863-14AD REV 0,1Apr 21, 2020 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020043002318Frame · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT FR 36. REPAIR PRIOR TO FURTHER FLIGHT. WC 5711-01 036-03B, AD 2018-13-08. HOLE ZONE 2 (OUTBD SIDE) Y 765, DIRECTION IS 1 2 AND 9 OCLOCK, DEPTH IS 0.160 INCH. IN FWD CARGApr 15, 2020 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020041502262Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 4 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 4 HOLE 2 (INB SIDE) -Y754 AT FR 36 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINAApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502261Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 5 HOLE ZONE 2 FR 36 (INB SIDE) -Y765 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGIApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502260Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 5 FR 36 -Y765 ZONE 1 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502259Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 3 AT HOLE ZONE 2 (O/B SIDE) Y754 AT FR 36 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV Apr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502258Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER POSITION 2 ZONE 1 (INB SIDE) Y765 AT FR 36 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502257Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 2 ZONE 1 (INB SIDE) Y765 AT FR 36 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502255Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER POSITION 3 AT ZONE 2 (O/B SIDE) Y254 AT FR 36 PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502254Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 3 AT ZONE 1 Y254 (INB SIDE) FR 36 PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502253Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER AT POSITION 3 FR36 AT ZONE 1 Y254 INB ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGINALApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020041502252Structure · crackedCRACK INDICATION ON FRAME 36 CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 AT FR 36, REPAIRED FRONT SPAR VERTICAL STRINGER POSITION 5 AT HOLE ZONE 1 FR 36 (O/B SIDE) -Y765 ASPER PRI ER/A 585863-14 AD REV 0 THRU REV 2 AND ER/A 585863-14AD REV ORIGIApr 15, 2020 · N321US · Airbus A320211 · Wing, Center BoxSDR DALA2020040602190Frame · crackedCRACK INDICATION ON FRAME 36 ON PRESSURE DECK PANEL LOCATED - Y1300 CRACK DIRECTION 3 OCLOCK IN FWD CARGO COMPARTMENT (1 EA), REPLACED WEB LOC. FRAME 36 RH SIDE ON PRESSURE DECK PANEL ASPER A320 SRM 51-42-11 AND DRAWING D53370500, D28270011Apr 4, 2020 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020040602189Frame · crackedCRACK INDICATION ON FRAME 36 PRESSURE DECK PANEL LOCATED -Y 1301 CRACK DIRECTION 3 OCLOCK IN FWD CARGO COMPARTMENT (1 EA), REPLACED WEB LOC. FRAME 36 RH SIDE ON PRESSURE DECK PANEL ASPER A320 SRM 51-42-11 AND DRAWING D53370500, D28270011Apr 4, 2020 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020040602188Floorbeam · corrodedCORROSION FLOOR BEAM -Y765 BTW FR67 TO FR68 AT AFT GALLEY AREA, REPLACED FLOOR BEAM LOC -Y765 BTW FR 66 TO FR 70 AFT GALLEY AREA FLOOR STRUCTURE AS PER A320 SRM 51-72-11 AND SRM 51-42- 11 AND DWG D53472816Apr 3, 2020 · N321US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2020040602187Frame · corrodedCORROSION WEB FRAME 20 AT LEVEL STR 23R FLOOR STRUCTURE AT FWD GALLEY AREA, REPLACED WEB FRAME 20 AT LEVEL STR 23R FLOOR STRUCTURE AT FWD GALLEY AREA ASPER A320 SRM 51-72-11 AND DWG D53112784Apr 2, 2020 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA2020040602186Intercostal · crackedCRACK INDICATION ON FRAME 16 RH SIDE ON DOOR STOP FITTING 7 HOLE 3, CRACK AT 8 O CLOCK ON UPPER FUSELAGE (1 EA), INTERCOSTAL REPLACEMENT IS DOCUMENTED ON NON-ROUTINE CARD 64/200 RII INSPECTION COMPLETEApr 2, 2020 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020040602185Floorbeam · corrodedCORROSION FLOOR BEAM -Y765 AT LEVEL FR20 AT FWD GALLEY AREA, REPLACED FLOOR BEAM -Y765 AT LEVEL FR.12 TO FR24 AT FWD GALLEY AREA ASPER SRM A320 FAM AMM 51-72-11 AND DWG D53112782Apr 2, 2020 · N321US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2020040602184Stop Fitting · crackedCRACK INDICATION ON FRAME 16 RH SIDE ON DOOR STOP FITTING 7 HOLE 1, CRACK AT 7 O CLOCK ON UPPER FUSELAGE (1 EA), REPLACED NEW LOC. FR.16 RH SIDE ON DOOR STOP #7 7 ASPER A320 SRM 51-42-11 AND 51-72-11 AND DWG D53112300Apr 2, 2020 · N321US · Airbus A320211 · Fuselage Main, StructureSDR DALA2020032001957Structure · corrodedCORROSION INTERNAL STRUCTURE SECTION CONNECTION AT FR67 AND STRG 28L UNDERFLOOR BAY IN AFT CARGO COMPARTMENT (1EA), REPLACED NEW SECTION CONECTION LOC. FR67 AND STR 28L UNDER FLOOR BAY IN AFT CARGO COMPARTMENT (1EA) AS PER A320 SRM 51-72-11 AND DRAWING D534805Mar 19, 2020 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020032001956Door Sill · corrodedCORROSION LOWER SILL AT LEVEL FR68 AND STR23L AT AFT GALLEY AREA, REPAIRED LOWER SILL AT LEVEL FR68 AND STR 23L AT AFT GALLEY AREA AS PER SRM A320 53-41-14-300-001Mar 19, 2020 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020032001955Seat Track · corrodedCORROSION FLOOR BEAM -Y765 AT LEVEL FR66 AT AFT GALLEY AREA, REPLACED SEAT TRACK LOCATED -Y765 BTW FR64 TO FR66 AFT GALLEY AREA FLOOR STRUCTURE AS PER A320 SRM 51-72-11, SRM 51-42-11 AND DWG #D53472816Mar 19, 2020 · N321US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020032001954Floorbeam · corrodedCORROSION FLOOR BEAM BTW -Y1292 AND -Y1162.5 BTW FR66 TO FR 68 AT AFT GALLEY AREA, REPLACED FLOOR BEAM -Y1162 LOC BTW -Y1292 AND 1162.5 BTW FR66 TO FR68 AT AFT GALLEY AREA AS PER DWG D53472000Mar 19, 2020 · N321US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2020032001953Floorbeam · corrodedCORROSION FLOOR BEAM -Y1162.5 BTW FR68 AND FR 69 AFT GALLEY AREA, REPLACED FLOOR BEAM -Y1162.5 NEW LOCATED BTW FR68 AND FR69 AFT GALLEY AS PER A320 SRM 51-72-11 AND DWG #D53472001Mar 19, 2020 · N321US · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2020032001952Stringer · corrodedCORROSION STRINGER 26R AT LEVEL OF FR66 IN AFT CARGO COMPARTMENT (1EA), REPLACED NEW STRINGER 26R AT LEVEL OF FR 66 IN AFT CARGO COMPARTMENT (1EA) AS PER A320 SRM 51-72-11, SRM 51-42-11 AND DRAWING D53480020Mar 19, 2020 · N321US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2020032001951Seat Track · corrodedCORROSION SEAT TRACK -Y1292 AT LEVEL OF FR 20 FLOOR AREA AT FWD GALLEY AREA, REPLACED NEW SEAT TRACK -Y1292 AT LEVEL FR20 FLOOR AREA FWD GALLEY AREA AS PER A320 SRM 51-72-11 AND DWG D53918547Mar 19, 2020 · N321US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020032001950Dummy Rail · corrodedCORROSION RAIL DUMMY Y503.2 LOCATED BTW FR 12 TO FR 16 AT FWD GALLEY AREA, REPLACED BEAM Y503.2 LOCATED BTW FR12 TO FR16 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11 AND DWG D53112827Mar 19, 2020 · N321US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2020032001949Door Sill · corrodedCORROSION LOWER SILL AT LEVEL OF FR 68 AND STR 23RH AT AFT GALLEY AREA, REPLACED LOWER SILL AT LEVEL OF FR 66 TO FR 68 AND STR 23R/H AT AFT GALLEY AREA AS PER A320 SRM 51-72-11 AND DWG #D53480505Mar 18, 2020 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020031401838Intercostal · crackedCRACK INDICATION ON FRAME 16 LH SIDE ON DOOR STOP FITTING 7 HOLE 3, CRACK AT 4 O CLOCK ON UPPER FUSELAGE (1 EA), REPLACED INTERCOSTAL FITTING IS TO BE ACCOMPLISHED ON NON-RUTINE CARD 66/200Mar 13, 2020 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2020031401837Intercostal · crackedCRACK INDICATION ON FRAME 16 LH SIDE ON DOOR STOP FITTING 7 HOLE 1, CRACK AT 5 O CLOCK ON UPPER FUSELAGE (1 EA), REPLACED INTERCOSTAL FITTING ON FRAME 16 LH SIDE AT LEVEL DOOR STEP 7 ON UPPER FUSELAGE AS PER A320 SRM 51-72-11 AND DRAWING #D53112300Mar 13, 2020 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2019022801323Panel · missingPDA PART DEPARTING AIRCRAFT. LOG 5291024 DURING SERVICE CHECK FOUND LT BELLY FAIRING SLIDING PANEL MISSING, PLACED LT BELLY FAIRING SLIDING PANEL ON CDL 57-00-02. MCO AND PLACARD INSTALLED.Feb 28, 2019 · N321US · Airbus A320211 · Aerodynamic FairingsSDR DALA2018052503598Slide · deformedDEFORMATION OF PASSENGER CREW DOOR SLIDE. . REPLACED THE SLIDE.May 25, 2018 · N321US · Airbus A320211 · Escape SlideSDR DALA2018052503597Skin · crackedCRACK FOUND ON THE DOOR EXTERNAL SKIN. REPAIRED IAW SRM 52-10-00.May 24, 2018 · N321US · Airbus A320211 · DoorsSDR DALA2018052403548Slide Raft · deformedDEFORMATION OF PASSENGER CREW DOOR SLIDE RAFT, 843. REPLACED SLIDE. OPERATION CHECKS OKAY.May 23, 2018 · N321US · Airbus A320211 · Escape Slide
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