N322US, cancelled Mar 2, 2023

Service difficulty reports · 101

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 = 'N322US' AND deregistration_id = 'N322US-2023-03-02'
  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 DALA2019121007214Light · damagedEMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATION 1C, REPLACED LIGHT FIXTURE AT SEAT 1CDec 10, 2019 · N322US · Airbus A320211 · Emergency LightingSDR DALA2018081095007Control Valve · failedEMERGENCY DECLARED FOR A NOSE WHEEL STEERING FAULT. REPLACED THE NOSE WHEEL STEERING SERVO CONTROL VALVE AND CONNECTOR 6GC IAW AMM. OPS AND LEAK CHECKED GOOD.Aug 9, 2018 · N322US · Airbus A320211 · Steering UnitSDR DALA2018071904574Skin · damagedPERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOWER FUSELAGE FRAME 72 TO FRAME 73, STR 24L TO 25L PER PRI 570056-14. COMPLIED WITH PRI/ERA 5700556-14 REV O.Jul 17, 2018 · N322US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2018071604504Damper · unserviceableCREW DOOR DAMPER 842, AFT GALLEY AREA, DOESN'T PASS CHECK. REMOVED AND REPLACED DOOR DAMPER AND EMERGENCY CYLINDER. CHECKS GOOD.Jul 14, 2018 · N322US · Airbus A320211 · Passenger/Crew DoorsSDR DALA2018071604502Rod End · corrodedCORROSION ON TRAILING EDGE ROD END OF YAW DAMPER. REMOVED, REPLACED AND FUNCTIONAL CHECK.Jul 14, 2018 · N322US · Airbus A320211 · Autopilot SystemSDR DALA2018071604501Slide · deformedSLIDE DEFORMATION PASSENGER CREW DOOR 832, AFT GALLEY AREA. REMOVED AND REPLACED SLIDE. CHECKS GOOD.Jul 14, 2018 · N322US · Airbus A320211 · Escape SlideSDR DALA2018060903916Wire · cutFOUND L2 SLIDE WIRES CUT. REMOVED AND REPLACED L2 DOOR SLIDE ASSEMBLY.Jun 8, 2018 · N322US · Airbus A320211 · Escape SlideSDR DALA2017091106815Power Supply · inoperativeEMERGENCY LIGHT FAILED, INT LOADS AFTL, EXT LOADS AFTL & BATTERY AFTL ILLUMINATED. REPLACED THE EPSU 13WL AND SLIDE.Sep 9, 2017 · N322US · Airbus A320211 · Emergency LightingSDR DALA2017052404232Battery Pack · inoperativeDURING A SERVICE CHECK, FOUND THE AFT LT BATTERY PACK FOR EMERGENCY LIGHTS INOPERATIVE, REPLACED THE BATTERY PACK.May 24, 2017 · N322US · Airbus A320211 · Emergency LightingSDR DALA2019070704066Skin · not reportedFUSELAGE SKIN AT GOGO WI-FI FWD ATG4 ANTENNA, FR 25 TO FR 26, S-43L TO S-42R; SECTION II PERMANENT REPAIR II PER ER/A 539169-14AD REV.B.Mar 7, 2017 · N322US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2017020301036Vent · corrodedLAVATORY VENT HAS CORROSION AND CRACK ON SKIN BETWEEN FR69 AND FR70, S31R AND S32R. SEE NR FOR ADDITIONAL INFORMATION 001-0001:2000-2001/001 00008 SEALED AND PAINTED AND CLOSED RT AFT BULKHEAD PANEL. REPAIRED IAW SRM 53-41-11.Feb 3, 2017 · N322US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016072805619Fitting · damagedDAMAGE ON RIGHT CRUCIFORM, REPAIRED IAW ER/A 548323-14AD REV A FOR WING CENTER CRUCIFORM FITTING.Jul 27, 2016 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2016072105469Frame · damagedDAMAGE ON FRAME 24, STRINGER 6R ON THE AFT SIDE OF THE FRAME. CUTOUT DAMAGE AND REPAIRED IAW ERA 548700-14.Jul 20, 2016 · N322US · Airbus A320211 · Fuselage Main, FrameSDR DALA2016072105468Frame · crackedCRACK INDICATIONS AT FRAME 16. COMPLIED WITH FINAL ERA 548219-14AD REV ORIGINAL.Jul 20, 2016 · N322US · Airbus A320211 · Fuselage Main, FrameSDR DALA2016072105467Box Beam · not reportedCENTER FUSELAGE RT SIDE BOX BEAM AT FRAME 43 AND Y1650. COMPLY WITH ERA 548164-14AD.Jul 20, 2016 · N322US · Airbus A320211 · Fuselage Main, StructureSDR DALA2016072105466Box Beam · not reportedCENTER FUSELAGE LT SIDE BOX BEAM AT FRAME 43 AND Y1650. COMPLY WITH ERA 548129-14AD.Jul 20, 2016 · N322US · Airbus A320211 · Fuselage Main, FrameSDR DALA2016111808959Stringer · corrodedCORROSION WAS FOUND ON STRINGER 43L BETWEEN FRAMES 33 AND 34. CORROSION WAS CUTOUT AND REPAIRED IAW SRM.Jul 18, 2016 · N322US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016111808958Stringer · corrodedCORROSION WAS FOUND ON STRINGER 43L BETWEEN FRAMES 33 AND 34. CORROSION WAS CUTOUT AND REPAIRED IAW SRM.Jul 18, 2016 · N322US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2016071205309Skin · damagedSKIN MISDRILLED THRU STRINGER FRAME 64 STRINGER 10L. REPAIRED THE SKIN IAW SRM 53-00-11 FIG. 239, PARA 4.W. AND REPAIRED STRINGER IAW SRM 53-00-13 FIG 203 PAR 4.AJul 10, 2016 · N322US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2015091005572Skin · damagedEVIDENCE OF DAMAGE TO LOWER FWD SKIN BETWEEN FRAMES 25-26 AND STRINGERS 44-43R PRI/ERA ISSUED 539169-14 REV 0 REV 1 REV 2 REV 3. C/W PRI/ERA 539169-14 REV 0,1,2 AND 3.Sep 9, 2015 · N322US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2015011200226Wire · brokenDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 6C INOPERATIVE. FOUND BOTH WIRES PULLED OUT OF LIGHT ASSY IN SEAT. REPAIRED BROKEN WIRES AND FUNCTIONAL CHECKED NORMAL.Jan 1, 2015 · N322US · Airbus A320211 · Light System WiringSDR DALA2014092105120Light · missingDURING INSPECTION, FOUND EMERGENCY EXIT ROW LIGHT AT 20 RT MISSING AT SEAT. MAINTENANCE REPLACED SEAT EMEGENCY LIGHT ASSY AND REPAIRED WIRING. FUNCTIONAL CHECKED NORMAL.Sep 20, 2014 · N322US · Airbus A320211 · Emergency LightingSDR DALA2014082004662Stringer Splice · corrodedCORROSION ON STRINGER SPLICE 42R IN FWD CARGO BAY BETWEEN FRAMES 28 - 31. REPLACED STRINGER SPLICE IAW SRM 51-42-11, 51-72-11, DWG D53231248200, ERA 528125-14, ORIGINAL REVISION AND PRI 528125-14 REV 0.Aug 19, 2014 · N322US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014081704625Door Sill · corrodedCORROSION ON LOWER L1 DOOR SILL BETWEEN FRAMES 16 - 20. REPLACED LOWER L1 DOOR SILL IAW SRM 51-72-11 AND DWG D53110339.Aug 16, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081604597Stringer · corrodedCORROSION ON STRINGER 33L BETWEEN FRAMES 65 - 66. REPAIRED STRINGER IAW SRM 53-00-13 PARAGRAPH 4A, FIG 201, SHEET 2, 3, 4 AND 5, PAGES 202-218.Aug 16, 2014 · N322US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014082004663Window Frame · crackedDURING M2-CHECK, A CRACK WAS FOUND ON THE FRAME SECTION AT LT SLIDING WINDOW IAW ALI 53-11-35-PB6. REPAIRED IAW ER/A 527498-14AD, REV ORIGINAL.Aug 15, 2014 · N322US · Airbus A320211 · Fuselage Main, StructureSDR DALA2014081504598Plate · corrodedAFTER REMOVING LOWER CORNER FITTING PERFORMED VISUAL INSPECTION AND FOUND CORROSION ON REINFORCEMENT PLATE FRAME 20 STRINGER 23L. REPLACED LOWER REINFORCEMENT PLATE AND FASTENER IAW SRM 51-72-11 AND ENGINEERING REPAIR AUTHORIZATION, 527501-14, REV ORIGINAL ANAug 15, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081804586Frame · corrodedCORROSION ON FWD FACE LATERAL FRAME 20 STRINGER 23R. PERFORMED TIME LIMITED REPAIR ON FWD FACE LATERAL FRAME 20 LOCATED FWD PASSENGER ENTRY DOOR LEVEL STR 23 RT INTERNAL STRUCTURE IAW ER/A 527494-14, REVISION ORIGINAL AND PRELIMINARY REPAIR INSTRUCTIONS 52749Aug 14, 2014 · N322US · Airbus A320211 · Fuselage Main, FrameSDR DALA2014081504585Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN FRAME 16 AND 20 Y-254. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND ENGINEERING REPAIR , AUTHORIZATION N 527502-14, REV: ORIGINAL.Aug 14, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081504583Floor Support · corrodedCORROSION ON LOWER SILL IN AFT PAX CABIN LOCATED BETWEEN FRAMES 66 AND 68 AT STRINGER 23R. REPLACED LOWER SILL IN AFT PAX CABIN LOCATED BETWEEN FR 66-FR 68 AT LEVEL STR 23R IAW SRM 51-72-11 AND DWG D53480019; JOB COMPLETE.Aug 14, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081404578Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER CORNER ON FWD LEFT PASSENGER DOOR AT FRAME 16, STINGER 23. REPLACED LOWER CORNER IAW SRM 51-72-11 AND DWG D53112109;Aug 13, 2014 · N322US · Airbus A320211 · Fuselage Main, StructureSDR DALA2014081404577Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING, FWD OF LEFT PASSENGER ENTRY DOOR, BETWEEN FRAMES 16 - 20. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53112109.Aug 13, 2014 · N322US · Airbus A320211 · Fuselage Main, StructureSDR DALA2014081404576Structure · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER CORNER LOCATED FWD OF LEFT PASSENGER ENTRY DOOR AT FRAME 20, STRINGER 23L. REPLACED LOWER CORNER STRUCTURE IAW SRM 51-72-11 AND DWG 53112109.Aug 13, 2014 · N322US · Airbus A320211 · Fuselage Main, StructureSDR DALA2014081304566Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Aug 12, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081304565Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Aug 12, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081304563Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y-1292, BETWEEN FRAMES 64 - 66+5". REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.Aug 12, 2014 · N322US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014081204420Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y512 BETWEEN FRAMES 64 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081204419Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 42L IN FWD CARGO BAY BETWEEN FRAMES 33 - 34. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53231212.Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014081104394Angle · crackedDURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE INTERNAL AREA EMERGENCY DOOR 843. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522 79010.Aug 11, 2014 · N322US · Airbus A320211 · Emergency ExitsSDR DALA2014081104393Angle · crackedDURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING ANGLE INTERNAL AREA EMERGENCY DOOR 843. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522-79010.Aug 11, 2014 · N322US · Airbus A320211 · Emergency ExitsSDR DALA2014081104392Angle · crackedDURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING ANGLE LOCATED INTERNAL AREA EMERGENCY DOOR 844. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522-79010.Aug 11, 2014 · N322US · Airbus A320211 · Emergency ExitsSDR DALA2014081104391Angle · crackedDURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE LOCATED INTERNAL AREA EMERGENCY EXIT DOOR 833. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522-79010.Aug 11, 2014 · N322US · Airbus A320211 · Emergency ExitsSDR DALA2014081104390Angle · crackedDURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE LOCATION INTERNAL AREA EMERGENCY DOOR 834. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D52279010.Aug 11, 2014 · N322US · Airbus A320211 · Emergency ExitsSDR DALA2014081104389Angle · crackedDURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE LOCATION INTERNAL AREA EMERGENCY DOOR 844. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522 79010.Aug 11, 2014 · N322US · Airbus A320211 · Emergency ExitsSDR DALA2014081104388Structure · crackedDURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING PROFILE LOCATED INTERNAL AREA EMERGENCY DOOR 833. REPLACED SEGMENT ANGLE LOCATED ON INTERNAL AREA EMERGENCY DOOR AFT POSITION IAW SRM 51-72-11 AND DWG D522 79010.Aug 11, 2014 · N322US · Airbus A320211 · Emergency ExitsSDR DALA2014081104386Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1162 BETWEEN FRAMES 67+15 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081104385Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 43L IN FWD CARGO BAY BETWEEN FRAMES 32 - 34. REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG D53231626.Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014081104384Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-464.5 LOCATED BETWEEN FRAMES 64 - 67+10. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72305.Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014081004383Cleat · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT AT FRAME 33 AND BETWEEN STR 40L TO STR 41L MEASURES APPROXIMATELY L=0.110", W=0.105", D=0.002" SSI 532180. REPLACED CLEAT AND FASTENERS LOCATED IN FWD CARGO COMPARTMENT AT FR 33 AND BETWEEN Aug 10, 2014 · N322US · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2014081004382Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-765 BETWEEN FRAMES 66 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DG D53472000.Aug 9, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous Structure
Back to N322US, cancelled Mar 2, 2023