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 DALA2018052403547Slide Raft · deformedDEFORMATION OF PASSENGER CREW DOOR SLIDE RAFT, 832. REPLACED SLIDE RAFT.May 23, 2018 · N321US · Airbus A320211 · Escape SlideSDR DALA2018052403550Cylinder · defectivePASSENGER CREW DOOR DAMPER EMERGENCY CYLINDER DOOR 832, DOESN'T WORK PROPERLY.May 22, 2018 · N321US · Airbus A320211 · Passenger/Crew DoorsSDR DALA201805213491Cylinder · failedEMERGENCY CYLINDER AT FORWARD GALLEY AREA. DOESN'T WORK CORRECTLY. REPLACED CYLINDER.May 17, 2018 · N321US · Airbus A320211 · Passenger/Crew DoorsSDR DALA201805213490Cylinder · failedEMERGENCY CYLINDER DOOR DAMPER AT FORWARD GALLEY AREA DOESN'T WORK CORRECTLY. REPLACED DOOR DAMPER CYLINDER.May 17, 2018 · N321US · Airbus A320211 · Passenger/Crew DoorsSDR DALA2017102207775Connector · disconnectedEMERGENCY LIGHT IN THE AFT CABIN OTBD AISLE INOPERATIVE. FOUND THE CONNECTOR NOT CONNECTED. SECURED THE CONNECTOR.Oct 22, 2017 · N321US · Airbus A320211 · Light System WiringSDR DALA2020041502251Frame · corrodedFUSELAGE / NOSE FWD / FRAME 16 AT STR23R / CORROSION, ACCOMPLISHED PERMANENT REPAIR PER ERA 522853-14 SECTION V REV CJan 17, 2017 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA2016062304895Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN PASSENGER CREW DOOR LOCATED BETWEEN BEAM 3 TO BEAM 4 AND XP297 TO XP453 AT FORWARD GALLEY AREA. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN PASSENGER CREW DOOR LOCATED BETWEEN BEAM 3 TO BEAM 4 ANDJun 23, 2016 · N321US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016062304894Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN, LOCATED 6" ABOVE RT SIDE STR AT FRAME 9 AT LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED 6" ABOVE OF LOWER STR RT AND FRAME 9 IAW ER/A 547910-14AD, REV ORIGINAL AND PRI 5479Jun 23, 2016 · N321US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016062304893Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN LOCATED 6" ABOVE RT SIDE STR AT FR 11 AT LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED "6" ABOVE OF LOWER STR RT SIDE AND FRAME 11 IAW ER/A N547910-14 AD REV ORIGINAL AND PRIJun 23, 2016 · N321US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016062304892Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN ON UPPER FUSELAGE FROM FRAME 56 TO FRAME 57 AND STR 1L. PERFORMED TIME LIMITED REPAIR ON EXTERNAL SKIN ON UPPER FUSELAGE FROM FRAME 56 TO FRAME 57 AND STR 2LT TO 2RT IAW ER/A 546749-14, REV ORIGINJun 22, 2016 · N321US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2016062304891Skin · dentedDENT ON EXTERNAL SKIN, ON UPPER FUSELAGE STR 23L BETWEEN FRAME 64 TO FRAME 65. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN, ON UPPER FUSELAGE STR 23L BETWEEN FRAME 64 TO FRAME 65 IAW ER/A 546748-14.Jun 22, 2016 · N321US · Airbus A320211 · Fuselage Main, Plate/SkinSDR DALA2015073104768Connector · unsecureEMERGENCY LIGHTS ARE INOPERATIVE AT 17 ABC-26 ABC. SECURED THE CONNECTOR AT THE BATTERY PACK AND OPS CHECKED NORMAL.Jul 30, 2015 · N321US · Airbus A320212 · Light System WiringSDR DALA2014071404082Control Unit · inoperativeDURING NON ROUTINE CHECK, FOUND RT EPCU INOPERATIVE. WITH UNIT FAULT LIGHT. MAINTENANCE REPLACED EPCU AND FUNCTIONAL CHECK WAS NORMAL.Jul 12, 2014 · N321US · Airbus A320211 · Emergency LightingSDR DALA14036143221Door Frame · crackedDURING INSPECTION, ONE CRACK WAS FOUND AT LT AFT PASSENGER DOOR CUT-OUT AT FRAME 68 AND AT STRINGER 8L. REPAIRED IAW ERA 526355-14, SECT I. ERA 526355-14 SECTION I.Jun 17, 2014 · N321US · Airbus A320211 · Fuselage Main, StructureSDR DALA2017112808356Frame · corrodedCORROSION WAS FOUND ON FRAME 16, STRINGER 23R, CORROSION WAS REMOVED IAW SRM 53-11-12 AND ERA 522853 SECT. I.Jun 16, 2014 · N321US · Airbus A320211 · Fuselage Main, FrameSDR DALA14035643221Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB BETWEEN FRAMES 56- 57 S38R. REPLACED WEB IAW PRI 524836-14 REV 0 AND ER/A 524836-14, REV ORIGINAL AND SRM A320 51-72-11;.Jun 14, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14035613221Support Angle · crackedDURING INSPECTION, FOUND CRACK ON SUPPORT ANGLE OF THE RT FORWARD PYLON CANTILEVER STRUCTURE INBD SIDE AT LEVEL RIB 5. REPAIRED SUPPORT ANGLE IAW SRM 54-52-12.Jun 13, 2014 · N321US · Airbus A320211 · Nacelle/Pylon Miscellaneous StructureSDR DALA14035603221Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 41R OF FWD CARGO BAY. REPAIRED BETWEEN FRAMES 29+14.5 - FR 30+14 IAW SRM 53-21-13.Jun 13, 2014 · N321US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA14035243221Profile · crackedDURING INSPECTION, FOUND A CRACK ON FWD LOAD TRANSMITTING PROFILE OF THE OVERWING EMERGENCY EXIT DOOR 844. REPLACED PROFILE IAW SRM 51-72-11 AND DWG D52279040 AND D52279010.Jun 12, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14035233221Profile · crackedDURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING PROFILE LOCATED OVERWING EMERGENCY EXIT DOOR 833. REPLACED PROFILE IAW SRM 51-72 -11 AND DWG D52279010.Jun 12, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14035113221Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON FWD FITTING LOCATED INTERNAL AREA OF OVERWING EMERGENCY EXIT DOOR 844 LOWER POSITION. REPLACED FITTING IAW SRM 51-72-11 AND DWG D52279040.Jun 11, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14034703221Profile · crackedDURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING PROFILE OF OVERWING EMERGENCY EXIT DOOR 843. REPLACED TRANSMITTING PROFILE IAW SRM 51-72-11, DWG D52279010 AND DWG D52279040.Jun 10, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14034693221Profile · crackedDURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING PROFILE AT OVERWING EMERGENCY EXIT DOOR 834. REPLACED AFT LOAD TRANSMITTING PROFILE IAW SRM 51-72-11 AND DWG D52279040.Jun 10, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14034683221Profile · crackedDURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING PROFILE, FOR OVERWING EMERGENCY EXIT DOOR 844. REPLACED AFT LOAD TRANSMITTING PROFILE IAW SRM 51-72-11 AND DWG D52279040.Jun 10, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14034643221Profile · crackedDURING INSPECTION, FOUND A CRACK ON FWD LOAD TRANSMITTING PROFILE ON OVERWING EMERGENCY EXIT DOOR 834. REPLACED FWD LOAD TRANSMITTING PROFILE IAW SRM 51-72-11 AND DWG D52279040.Jun 10, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14034633221Profile · crackedDURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING PROFILE LOCATED OVERWING EMERGENCY EXIT DOOR 843. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-72-11 AND DWG D52279010.Jun 10, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14034623221Profile · crackedDURING INSPECTION, FOUND CRACK ON FWD. LOAD TRANSMITTING PROFILE LOCATED OVERWING EMERGENCY EXIT DOOR 833. REPLACED FWD LOAD TRANSMITTING PROFILE IAW SRM 51-72-11 AND DWG D52279010.Jun 10, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14034613221Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT FRAME 20. REPLACED FLOOR SUPPORT BETWEEN FRAMES 16-20 IAW SRM 51-72-11 AND DWG D53110399.Jun 10, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14034403221Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON FWD CARGO BAY SHEAR TIE FRAME 29 BETWEEN S41-42L. REPLACED SHEAR TIE IAW SRM 51-72-11, DWG D532-31712 AND D532-30320.Jun 10, 2014 · N321US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA14034393221Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 66-68. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 80009.Jun 9, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14034383221Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB BETWEEN FRAMES 51- 52 STR 38R. REPLACED WEB IAW SRM A320 51-72-11 AND DWG D534-70320.Jun 9, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14034363221Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON FWD CARGO BAY SHEAR TIE FRAME 32 BETWEEN S41-42L. REPLACED SHEAR TIE IAW SRM 51-72-11, DWG D532 31712 AND D532 30320.Jun 9, 2014 · N321US · Airbus A320211 · Fuselage Internal Mounting StructureSDR DALA14034353221Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 16 - 20, -Y254. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG 531-12819.Jun 9, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14034343221Support Angle · crackedDURING INSPECTION, FOUND CRACK ON SUPPORT ANGLE OF THE LT UPPER PYLON INBD SIDE AT LEVEL RIB 5 CANTILEVER STRUCTURE. PERFORMED PERMANENT REPAIR ON SUPPORT ANGLE OF THE LT UPPER PYLON INBD SIDE AT LEVEL RIB 5 CANTILEVER STRUCTURE IAW SRM 54-52-12 PARA 5N, FIJun 9, 2014 · N321US · Airbus A320211 · Nacelle/Pylon Miscellaneous StructureSDR DALA14034213221Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL IN AFT PAX CABIN BETWEEN FRAMES 66-68 STRINGER 23 LT. REPLACED LOWER FLOOR SUPPORT IAW SRM AND DWG D53480505.Jun 7, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14034153221Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON AFT LOWER CORNER FRAME 20 OF RT FWD PAX DOOR CUTOUT. REPLACED LOWER CORNER FITTING IAW SRM 51-72-11 AND DWG D531 12109.Jun 6, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14033753221Fitting · corrodedCORROSION ON AFT LOWER CORNER FITTING ON L2 DOOR AT FRAME 68. REPLACED CORNER FITTING IAW SRM 51-72-11 AND DWG D53480505.Jun 4, 2014 · N321US · Airbus A320211 · Passenger/Crew DoorsSDR DALA14033733221Seat Track · damagedDAMAGE ON SEAT TRACK BETWEEN FRAMES 41-47, Y1292. FOUND OUT LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D533 70500.Jun 4, 2014 · N321US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA14033723221Structure · corrodedCORROSION ON SECTION OF INTERNAL STRUCTURE STRINGER 29L, FRAME 67. REPLACE SECTION IAW SRM 51-72-11 AND DWG D53480009.Jun 4, 2014 · N321US · Airbus A320211 · Fuselage Main, StructureSDR DALA14033713221Floor Support · corrodedCORROSION ON FLOOR SUPPORT Y1162 BETWEEN FRAMES 68-69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Jun 4, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14033703221Seat Track · corrodedSEAT TRACK DAMAGED BETWEEN FRAMES 41-47, Y765 AND FOUND OUT LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.Jun 4, 2014 · N321US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR DALA14033693221Floor Support · corrodedCORROSION ON FLOOR SUPPORT Y1225 BETWEEN FRAMES 66-68. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Jun 4, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14033683221Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1162 BETWEEN FRAMES 68-69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Jun 4, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14033673221Fitting · corrodedCORROSION ON LOWER AFT CORNER AT FRAME 20. REPLACED FITTING IAW SRM 51-72-11 AND DWG D53112109.Jun 4, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14033663221Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y464.8, FRAMES 64-67+9. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Jun 4, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14033653221Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1225 BETWEEN FRAMES 66-68. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Jun 4, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14033643221Floor Support · corrodedCORROSION ON FLOOR SUPPORT Y1292 BETWEEN FRAMES 64 - 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Jun 4, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14033623221Fitting · crackedAFTER REMOVAL OF LOWER SILL IAW 260-57, FOUND CRACK ON CORNER FITTING LOCATED AT FR 66 RT SIDE AFT PAX CABIN. REPLACED CORNER FITTING LOCATED AT FR 66 RT SIDE AFT PAX CABIN AS IAW SRM 51-72-11 AND DWG D53480009.Jun 4, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14033313221Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y765, FRAMES 66-70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.Jun 3, 2014 · N321US · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14033303221Shear Tie · corrodedCORROSION ON FWD CARGO COMPARTMENT SHEAR TIE FRAME 33 BETWEEN S40-41R. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231582.Jun 3, 2014 · N321US · Airbus A320211 · Fuselage Internal Mounting Structure
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