Airbus A320-233

Service difficulty reports · 254

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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 aircraft_model_key = 'A320233'
  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 23431924Sill · corrodedAT (C) CHECK, FOUND L2 DOOR SILL HAS RIVET HEADS THAT HAVE EXFOLIATED CORROSION BETWEEN FR 66 AND FR 68. REMOVED AND REPLACED L2 DOOR SILL, LOWER FORWARD CORNER FITTING, DRAINS AND ANGLE AT FRAME 67, LT LOWER UNDER SILL. (SDR NR 23431924)Sep 17, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00139Fitting · corrodedAT C-CHECK, FOUND CORROSION ON FITTING AT FRAME 59 AND STRINGER 41R IN AFT CARGO BAY. FITTING AT FRAME 59, RIGHT STRINGER 41 OF FLOOR STRUCTURE REMOVED AND REPLACED. (M)Sep 16, 2003 · N951LF · Airbus A320233 · Fuselage Main, Attach FittingsSDR 2004F00134Floor Support · corrodedAT C-CHECK, FOUND FLOORBOARD SUPPORT CORRODED AT RIGHT STRINGER 38 BETWEEN FRAME 58 AND 59 ON AFT LOWER CARGO BAY FLOOR. REMOVED AND REPLACED FLOOR SUPPORT FRAME BETWEEN FRAME 58 AND 59. (M)Sep 16, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00133Floor Support · damagedAT C-CHECK, FOUND 5 DAMAGED AREAS ON FLOORBOARD SUPPORT AT FRAME 59 BETWEEN STRINGER 42R AND 43L IN AFT CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 59 ON RIGHT SIDE. (M)Sep 16, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00132Seat Track · corrodedAT C-CHECK, FOUND SEAT TRACK CORRODED BETWEEN FRAMES 20 AND 21 AT RBL 32. REMOVED AND REPLACED SEAT TRACK FROM RBL 32, FRAME 12 TO 24. (M)Sep 16, 2003 · N951LF · Airbus A320233 · Fuselage, Seat/Cargo Attach FittingsSDR 2004F00124Floorbeam · corrodedAT C-CHECK, FOUND CORROSION ON FLOORBEAM AT FRAME 20 AT RBL 12. REMOVED AND REPLACED FLOORBEAM AND SPLICE AT FRAME 20, RBL 12. (M)Sep 16, 2003 · N951LF · Airbus A320233 · Fuselage Main, Floor BeamSDR 2004F00113Structure · corrodedAT C-CHECK, OFUND CORROSION ON AFT CABIN FLOOR STRUCTURE AT FRAME 67 PLUS 13 INCHES TO FRAME 67 AT LBL 45. REMOVED AND REPLACED AFT CABIN FLOOR STRUCTURE AT FRAME 67 PLUS 13 INCHES TO FRAME 67 AT LBL 45. (M)Sep 15, 2003 · N951LF · Airbus A320233 · Fuselage Main, StructureSDR 2004F00112Structure · corrodedAT C-CHECK, FOUND CORROSION ON FLOOR STRUCTURE AT FRAME 69 PLUS 3 INCHES TO 69 PLUS 10 INCHES AND LBL 50 IN CABIN. REMOVED AND REPLACED AFT CABIN FLOOR STRUCTURE AT FRAME 69 PLUS 3 INCHES TO FRAME 69 PLUS 10 INCHES, LBL 50. (M)Sep 15, 2003 · N951LF · Airbus A320233 · Fuselage Main, StructureSDR 2004F00060Plate · wornAT C-CHECK, FOUND R2 DOOR CAM PLATE FOR DOOR HANDLE BACK MECHANISM ROLLER HAD WEAR MARKS. REMOVED AND REPLACED FITTING ON R2 DOOR, DOOR HANDLE BACK MECHANISM. (M)Sep 15, 2003 · N951LF · Airbus A320233 · Service DoorsSDR 2004F00059Fitting · gougedAT C-CHECK, FOUND GOUGES ON THE LATCHES OF THE LOWER FITTING OF THE RT FORWARD EMERGENCY EXIT DOOR. REMOVED AND REPLACED LOWER LATCH FITTINGS ON RT FORWARD EMERGENCY EXIT DOOR. (M)Sep 15, 2003 · N951LF · Airbus A320233 · Emergency ExitsSDR RYN2004F00009Attach Fitting · corrodedAT (C) CHECK FOUND AFT CABIN NR 2 RT DOORWAY, FORWARD GIRT BAR ATTACH FITTING PLATE, WITH CORROSION. REMOVED AND REPLACED FORWARD GIRT BAR ATTACH FITTING PLATE ON AFT CABIN NR 2 RT DOORWAY.Sep 15, 2003 · N951LF · Airbus A320233 · Escape SlideSDR RYN2004F00008Attach Fitting · corrodedAT (C) CHECK FOUND AFT CABIN NR 2 RT DOORWAY AFT GIRT BAR ATTACH FITTING PLATE WITH CORROSION. REMOVED AND REPLACED AFT GIRT BAR ATTACH FITTING PLATE ON AFT CABIN NR 2 RT DOORWAY.Sep 15, 2003 · N951LF · Airbus A320233 · Passenger/Crew DoorsSDR RYN2004F00006Latch · damagedAT (C) CHECK, FOUND GOUGE ON FORWARD LT EMERGENCY EXIT DOOR LOWER AFT FITTING LATCH. REMOVED AND REPLACED FORWARD LT EMERGENCY EXIT DOOR, LOWER AFT LATCH FITTING.Sep 15, 2003 · N951LF · Airbus A320233 · Emergency ExitsSDR 2004F00227Floor Support · bentAT C-CHECK, FOUND FLOOR PANEL SUPPORT FOR FLOOR PANEL 232WF IS BENT. FORMED FLOOR PANEL SUPPORT AT FLOOR PANEL NR 232WF BACK TO ORIGINAL CONTOUR. (M)Sep 13, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00136Pan · corrodedAT C-CHECK, FOUND CORROSION ON LEFT AFT LAVATORY FLOOR PAN ASSEMBLY ATTACH POINTS FOR BLOW-OUT DOOR FRAME, 8 PLACES. AFTER EVALUATION, FOUND NO CORROSION ON LEFT AFT LAVATORY FLOOR PAN ASSEMBLY, ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. (M)Sep 12, 2003 · N951LF · Airbus A320233 · Fuselage Floor PanelSDR 2004F00116Floor Panel · corrodedAT C-CHECK FOUND EXFOLIATED CORROSION AT AFT CARGO COMPARTMENT FLOOR PANEL 151DF. FABRICATED AND INSTALLED FLOOR PANEL NR 151DF, AFT CARGO COMPARTMENT. (M)Sep 12, 2003 · N951LF · Airbus A320233 · Fuselage Floor PanelSDR 2004F00111Floor Panel · corrodedAT C-CHECK, FOUND CORROSON ON FLOOR PANEL NR 152BF IN AFT CARGO COMPARTMENT. FABRICATED, PRIMED AND INSTALLED AFT CARGO FLOOR PANEL NR 152BF. (M)Sep 12, 2003 · N951LF · Airbus A320233 · Fuselage Floor PanelSDR 2004F00118Floor Panel · corrodedAT C-CHECK, FOUND DAMAGE ON UPPER SKIN AND CORROSION ON FLOOR PANEL NR 151BF IN AFT CARGO BAY. FABRICATED AND INSTALLED NEW AFT CARGO COMPARTMENT, FLOOR PANEL NR 151BF. (M)Sep 12, 2003 · N951LF · Airbus A320233 · Fuselage Floor PanelSDR RYN2004F00007Floor Panel · corrodedAT (C) CHECK FOUND AFT LAV FLOOR PANEL WITH CORROSION AT NUMEROUS LOCATIONS AT ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. REPAIRED AFT LAV FLOOR PANEL, CORROSION AT ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. REMOVED AND REPLACED INSERTS.Sep 12, 2003 · N951LF · Airbus A320233 · Fuselage Floor PanelSDR 2004F00114Floor Panel · corrodedAT C-CHECK, FOUND CORROSION ON FLOOR PANEL NR 152EF IN AFT CARGO BAY. FABRICATED, TREATED, PRIMED AND INSTALLED AFT CARGO COMPARTMENT FLOOR PANEL NR 152EF. (M)Sep 11, 2003 · N951LF · Airbus A320233 · Fuselage Floor PanelSDR 2004F00141Floor Support · corrodedAT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 63 ABOVE STRINGER 38L IN AFT CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 63 ABOVE STRINGER 38L. (M)Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00131Floor Support · corrodedAT C-CHECK, FOUND FLOORBOARD SUPPORT CORRODED AT FRAME 58 BETWEEN STRINGER 38R AND 40R IN AFT LOWER CARGO COMPARTMENT. REMOVED FLOORBOARD SUPPORT, FABRICATED AND INSTALLED NEW FLOORBOARD SUPPORT AT FRAME 58 BETWEEN STRINGER 38R AND 40R. (M)Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00130Floor Support · corrodedAT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 59 ABOVE STRINGER 40L IN AFT LOWER CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT CHANNEL AT FRAME 59 ABOVE STRINGER 40L. (M)Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00129Floor Support · corrodedAT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FASTENER HOLE BETWEEN FRAME 60 AND 61 ABOVE STRINGER 43L IN AFT LOWER CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT BETWEEN FRAME 60 AND 61 ABOVE STRINGER 43L. (M)Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00128Floor Support · corrodedAT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN FRAME 58 AND 59 ABOVE STRINGER 38R IN AFT LOWER CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT BETWEEN FRAME 58 AND 59 ABOVE STRINGER 38R. (M)Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00127Floor Support · corrodedAT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN FRAME 62 AND 63 ABOVE STRINGER 37L IN AFT CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT BETWEEN FRAME 62 AND 63 ABOVE STRINGER 37L. (M)Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00126Floor Support · corrodedAT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 63 ABOVE STRINGER 39R IN AFT LOWER CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 63 ABOVE STRINGER 39R. (M)Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00125Floor Support · corrodedAT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN FRAME 49 AND FRAME 50 ABOVE STRINGER 43L IN AFT CARGO BAY. INSTALLED NEW FLOORBAORD SUPPORT BETWEEN FRAME 49 AND 50 ABOVE STRINGER 43L IN AFT CARGO BAY. (M)Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00122Floor Support · crackedAT C-CHECK, FOUND CRACK ON FLOORBOARD SUPPORT AT FRAME 56 AND STRINGER 42R IN AFT LOWER CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 56 AND STRINGER 42R. (M)Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00119Floor Support · corrodedAT C-CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN FRAME 48 AND FRAME 50 ABOVE STRINGER 38L IN AFT LOWER CARGO BAY. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 48L TO 52L, STRINGER 38L IN AFT LOWER CARGO BAY. (M)Sep 10, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00140Frame · corrodedAT C-CHECK, FOUND CORROSION ON LEFT SIDE OF FRAME BETWEEN FRAME 24 AND 35 AT STRINGER 34L TO CENTER BUTT LINE. FABRICATED AND INSTALLED FLOOR SUPPORTS FRAME BETWEEN FRAME 24 TO FRAME 34 AT STRINGER 34L. (M)Sep 9, 2003 · N951LF · Airbus A320233 · Fuselage Main, FrameSDR 2004F00117Floor Panel · corrodedAT C-CHECK, FOUND CORROSION AND BARE METAL ON SEVERAL NUT PLATES AND CLIP NUTS AND THEIR UPPER AND LOWER MOUNTING SURFACE IN FORWARD CARGO COMPARTMENT BETWEEN RIGHT FRAME 28 TO FRAME 34, RIGHT STRINGER R-S 34 TO CENTER B/L. FABRICATE, ALODINED, PRIMED, APPLIESep 9, 2003 · N951LF · Airbus A320233 · Fuselage Floor PanelSDR RYN2004F00010Threshold · corrodedAT (C) CHECK FOUND R2 DOOR THRESHOLD HAS 5 CORRODED RIVETS. REMOVED AND REPLACED CORRODED RIVETS AT R2 DOOR THRESHOLD.Sep 7, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2003F00560Proximity Sensor · malfunctionedDURING CRUISE STAGE LIGHT, MESSAGES 'ENG 2 REVERSER FAULT' AND 'ANTI ICE F/O PITOT INOPERATIVE' WERE DISPLAYED ON ECAM. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING AT SAT STATION, TECHS PERFORMED INSPECTION OF THE REVERSER SYSTEM. POSep 6, 2003 · N461TA · Airbus A320233 · Landing Gear Position and WarningSDR 2003F00535Transceiver · damagedSJO - FLT 691 - DURING CRUISE, THE WX R/T FAILED, THE AIRCRAFT RETURNED TO SJO STATION FOR MAINTENANCE. AFTER LANDING AT SJO, TECHNICIANS FOUND WEATHER RADAR TRANSCEIVER DAMAGED. IT WAS REMOVED AND REPLACED TRANSCEIVER, P/N 622-5132-622, AND PERFORMED INSTALAug 16, 2003 · N482TA · Airbus A320233 · Weather Radar SystemSDR 2003F00517Regulator · stuckSAL - FLT 581 - DURING CRUISE, ENGINE NR 1 BLEED VALVE REMAINS CLOSED AND THE ENGINE NR 2 PRECOOLER REACHED THE LIMITS IN A SINGLE BLEED OPERATION. THE AIRCRAFT WAS DEVIATED TO SAL STATION FOR MAINTENANCE. AFTER LANDING AT SAL, TECHS REPLACED THE PRESSURE REAug 9, 2003 · N462TA · Airbus A320233 · Pneumatic Distribution SystemSDR 2003F00534Engine · making metalSAL - FLT 531 - FLIGHT CREW REPORTED ENGINE NR 2 N1 VIBRATION WHILE ARRIVING AT SAL STATION. TECHNICIANS PERFORMED INSPECTION OF ENGINE NR 2, AND FOUND SOME METALLIC DEBRIS AT THE EXHAUST AREA AND THE FAN BLADES COULD NOT BE TURNED BY HAND. ENGINE NR 2 ENGINAug 3, 2003 · N455TA · Airbus A320233 · Engine (Turbine/Turboprop)SDR 2003F00533Seal · damagedSFO - FLT 562 - DURING GROUND CHECK, MAINTENANCE TECHS FOUND THE NOSE LANDING GEAR STRUT WITH FLUID LEAKAGE. TECHS PERFORMED REPLACEMENT OF THE NOSE LANDING GEAR STRUT SEALS AS PER AMM 32-21-13. OPS TEST OF THE NOSE LANDING GEAR RETRACTION AND EXTENSION WAS Aug 2, 2003 · Airbus A320233 · Nose/Tail Landing Gear Strut/AxleSDR 2003F00468Antenna · inoperativeAFTER TAKEOFF AT SAL STATION, FLT TA580, PILOT REPORTED THE RADAR WEAK ON AND NON-REAL WX DISPLAYED. THE AIRCRAFT RETURNED TO SAL STATION, WHERE MX TECHNICAN INSPECTED THE OPERATION OF THE RADAR. REPLACEMENT OF THE RADAR ANTENNA AND TEST WERE PERFORMED WITH Jul 13, 2003 · N451TA · Airbus A320233 · Weather Radar SystemSDR 2003F00408Cover · brokenDURING TAXIING PROCESS OF FLIGHT, THE 'THS' CONFIGURATION WENT ALL DOWN AND THE AIRCRAFT COULDN'T DEPART FROM LAX STATION. THE AIRCRAFT REMAINED ON GROUND FOR MAINTENANCE. TECHNICIANS CHECKED THE 'THS' MECHANISM PER AMM 27-44-00 AND FOUND ONE OF THE PLASTIC Jun 28, 2003 · N981LR · Airbus A320233 · Hydraulic Power SystemSDR RJEF598H1Indicator · inoperativeMSY - 221 - AIRCRAFT AT GATE, THE STANDBY HORIZONTAL INDICATOR WENT INOPERATIVE AND THE AIRCRAFT STOOD ON GROUND FOR MAINTENANCE. TECHNICIANS REPLACED AND TEST THE STANDBY HORIZONTAL PER AMM 34-22-24. RESULTS WERE SATISFACTORY AND THE AIRCRAFT RETURNED TO NOJun 27, 2003 · N465TA · Airbus A320233 · Attitude Gyro and Indicating SystemSDR 2003F00407Blade · bentDURING CLIMB, TWO COMPRESSOR STALLS AND LOSS OF POWER ON ENGINE NR 1 WERE EXPERIENCED. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT WAS RETURNED TO SAL STATION. ON GROUND TECHNICIANS PERFORMED HPC BOROSCOPE INSPECTION PER AMM 72-00-00. THE 6TH WAS FOUJun 27, 2003 · N464TA · Airbus A320233 · Turbine Engine Compressor SectionSDR 2003F00481Skin · crackedAT C-CHECK, FOUND LEFT MLG WHEEL WELL DOOR INTERIOR SKIN CRACKED AT STATION 17255. REPAIRED DOOR IAW SRM 52-81-14, PAGE 258-264, FIGURE 205. (M)May 23, 2003 · N951LF · Airbus A320233 · Landing Gear DoorsSDR 2003F00476Fairing · delaminatedAT C-CHECK, FOUND BELLY FAIRING 197CB DELAMINATED. REPAIRED FAIRING IAW SRM S3-45-12 PAGE 220, FIGURE 205. (M)May 16, 2003 · N951LF · Airbus A320233 · Aerodynamic FairingsSDR 2003F00475Skin · delaminatedAT C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER SKIN DELAMINATED. REPAIRED NR 1 THRUST REVERSER IAW SRM V2500, 54-30-00, REPAIR NR 22. (M)May 16, 2003 · N951LF · Airbus A320233 · Engine Thrust ReverserSDR 2003F00490Precooler · delaminatedAT C-CHECK, FOUND NR 1 ENGINE INTAKE PRECOOLER, ON BOTH SIDES OF THRUST REVERSER C-DUCT DELAMINATED. REPAIRED PRECOOLER IAW SRM 54-02-00. (M)May 16, 2003 · N951LF · Airbus A320233 · Pneumatic Distribution SystemSDR 2003F00482Fairing · delaminatedAT C-CHECK, FOUND BELLY FAIRING 197EB DELAMINATED. REPAIRED FAIRING IAW SRM S3-4S-12, PAGE 220 FIGURE 205. (M)May 16, 2003 · N951LF · Airbus A320233 · Aerodynamic FairingsSDR 2003F00480Fairing · delaminatedAT C-CHECK, FOUND RIGHT BELLY FAIRING 197GB, DELAMINATED. REPAIRED BELLY FAIRING 197GB IAW SRM S3-4S-12, PAGE 220 FIG 205. (M)May 16, 2003 · N951LF · Airbus A320233 · Aerodynamic FairingsSDR 2003F00474Fairing · delaminatedAT C-CHECK, FOUND BELLY FAIRING 192AB DELAMINATED. REPAIRED FAIRING IAW SRM 51-77-12 PAR 3B, FIGURE 3. (M)May 16, 2003 · N951LF · Airbus A320233 · Aerodynamic FairingsSDR 2003F00489Coupling · delaminatedAT C-CHECK, FOUND NR 1 ENGINE LEFT THRUST REVERSER COUPLING OUTER SKIN C-DUCT DELAMINATED AND MISSING MATERIAL. REPAIRED 'C' DUCT IAW SRM V2500, REPAIR NR 4, REV 31. (M)May 16, 2003 · N951LF · Airbus A320233 · Engine Thrust Reverser
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