Airbus A320-231
Service difficulty reports · 3,758
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'A320231' 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.
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 = 'A320231' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAA2011011990268Floor Panel · delaminatedSAL - S5 - MAJOR REPAIR - DELAMINATION ON SURFACE OF FLOOR PANEL 261NF BETWEEN FR64 TO FR66, -Y765 TO Y765. REPLACED FLOOR PANEL 261NF BETWEEN FR64 TO FR66, -Y765 TO Y765 IAW A320 SRM 53-02-00 & MCGILL IRM 9701 REV G.SDR USAA2011011890255Angle · crackedSAL - S5 - MAJOR REPAIR - CRACK ON LEFT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 843 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON LEFT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 843 BETWEEN FR38 TO FR39 & BETWESDR USAA2011011890254Angle · crackedSAL - S5 - MAJOR REPAIR - CRACK ON LEFT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 833 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON LEFT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 833 BETWEEN FR38 TO FR39 & BETWESDR USAA2011011890253Angle · crackedSAL - S5 - MAJOR REPAIR - CRACK ON RIGHT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 843 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON RIGHT LOAD TRANSMITTING PROFILE AT EMERGENCY EXIT HATCH 843 BETWEEN FR38 TSDR USAA2011011890252Angle · crackedSAL - S5 - MAJOR REPAIR - CRACK ON RIGHT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 833 BETWEEN FR38 TO FR39 & BETWEEN BEAM 1 TO BEAM 3. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON RIGHT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 833 BETWEEN FR38 TO FR39 & BETSDR USAA2011011890251Beam · crackedSAL - S5 - MAJOR REPAIR - CRACK ON LEFT SEGMENT BEAM AT EMERGENCY EXIT HATCH 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON LEFT SEGMENT BEAM AT EMERGENCY EXIT HATCH 834 BETWEEN FR40 TO FR41 & BETWEENSDR USAA2011011890250Angle · crackedSAL - S5 - MAJOR REPAIR - CRACK ON LEFT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 834 BETWEEN FR40 TO FR41 & BETWEEN BEAM 1 TO BEAM 3. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON LEFT SEGMENT ANGLE AT EMERGENCY EXIT HATCH 834 BETWEEN FR40 TO FR41 & BETWESDR USAA2011011890249Profile · crackedSAL - S5 - MAJOR REPAIR - CRACK ON LEFT LOAD TRANSMITTING PROFILE AT EMERGENCY EXIT HATCH 844. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON LEFT LOAD TRANSMITTING PROFILE AT EMERGENCY EXIT HATCH 844.SDR USAA2011011890248Profile · crackedSAL - S5 - MAJOR REPAIR - CRACK ON RIGHT LOAD TRANSMITTING PROFILE AT EMERGENCY EXIT HATCH 844. PERFORMED ENGINEERING ORDER MODIFICATION 5210Y228 ON RIGHT LOAD TRANSMITTING PROFILE AT EMERGENCY EXIT HATCH 844.SDR USAA2011011090153Structure · corrodedS5 - MAJOR REPAIR - LEVEL 2 CORROSION ON RIGHT AFT EMERGENCY EXIT HATCH LOWER LEFT CURVED EDGE BETWEEN FR40 TO FR41 BEAM 4. REPLACED RIGHT AFT EMERGENCY EXIT HATCH LOWER LEFT CURVED EDGE BETWEEN FR40 TO FR41 BEAM IAW SRM 51-72-11 & DRAWING D52279028204.SDR USAA2011011090152Structure · corrodedS5 CHECK - MAJOR REPAIR - LEVEL 2 CORROSION ON LEFT AFT EMERGENCY EXIT HATCH LOWER RIGHT CURVED EDGE BETWEEN FR40 TO FR41 BEAM 4. REPLACED LEFT AFT EMERGENCY EXIT HATCH LOWER RIGHT CURVED EDGE BETWEEN FR40 TO FR41 BEAM 4 IAW 51-72-11 & DRAWING D2279010.SDR USAA2011011090147Floor Panel · delaminatedSAL - S5 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 232DF BETWEEN FR20 TO FR24, S23R & BETWEEN -Y765 TO -Y254. REPLACED FLOOR PANEL 232DF BETWEEN FR20 TO FR24, S23R & BETWEEN -Y765 TO -Y254 IAW A320 SRM 53-02-00.SDR USAA2011010390015Dummy Rail · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, -Y81. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, -Y81 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112619.SDR USAA2011010390014Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, Y254. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, Y254 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53110876.SDR USAA2010122393234Floor Panel · delaminatedSAL - MAJOR REPAIR - S5 CHECK - CABIN FLOOR PANEL 241EF HAS DELAMINATION. REPLACED CABIN FLOOR PANEL 241EF.SDR USAA2010122393232Floor Panel · delaminatedSAL - MAJOR REPAIR - S5 CHECK - CABIN FLOOR PANEL 242GF HAS DELAMINATION. REPLACED CABIN FLOOR PANEL 242GF.SDR USAA2010122393231Floor Panel · delaminatedSAL - MAJOR REPAIR - S5 CHECK - CABIN FLOOR PANEL 242FF HAS DELAMINATION. REPLACED CABIN FLOOR PANEL 242FF.SDR USAA2010122393230Floor Panel · delaminatedSAL - MAJOR REPAIR - S5 CHECK - CABIN FLOOR PANEL 251RF HAS DELAMINATION. REPLACED CABIN FLOOR PANEL 251RF.SDR USAA2011011990267Sill · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON LOWER DOOR SILL OF R-2 DOOR CUTOUT AT FR68, S23R. REPAIRED LOWER DOOR SILL OF R-2 DOOR CUTOUT AT FR68, S23R IAW EA 133246.SDR USAA2011010490041Seat Track · corrodedS5 CHECK- MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR20, -Y765. REPLACED SEAT TRACK AT FR20, -Y765 IAW A320 SRM 51-72-11.SDR USAA2011011090146Slide Raft · defectiveSAL - S5 - MAJOR REPAIR - OVER INFLATE SLIDE RAFT PACK ASSEMBLY AT PASSENGER / CREW DOOR 842. REPLACED SLIDE RAFT PACK ASSEMBLY AT PASSENGER / CREW DOOR 84 IAW A320 AMM 25-62-44.SDR USAA2011010790119Slide Raft · defectiveSAL - S5 - EES - OVER INFLATED SLIDE RAFT PACK ASSEMBLY AT PASSENGER CREW DOOR 831. REPLACED SLIDE RAFT PACK ASSEMBLY AT PASSENGER CREW DOOR 831 IAW JOB CARD 26C83152008.SDR USAA2010120992935Cylinder · low pressureFLT 94 - PHX - EES - R-2 DOOR ASSIST BOTTLE LOW PRESSURE. MAINTENANCE SERVICED R-2 DOOR ASSIST BOTTLE TO PROPER PRESSURE.SDR USAA2010121793142Slide Raft · faultySAL - EES - S5 CHECK - PASSENGER CREW DOOR 842 SLIDE RAFT WAS OVER INFLATED. REPLACED SLIDE RAFT AT PASSENGER CREW DOOR 842 IAW TASK CARD 26C84252006.SDR USAA2010121793141Slide Raft · faultySAL - EES - S5 CHECK - PASSENGER CREW DOOR 832 SLIDE RAFT WAS OVER INFLATED. REPLACED SLIDE RAFT AT PASSENGER CREW DOOR 832 IAW TASK CARD 26C83252008.SDR USAA2010121793140Slide Raft · faultySAL - EES - S5 CHECK - PASSENGER CREW DOOR 841 SLIDE RAFT WAS OVER INFLATED. REPLACED SLIDE RAFT AT PASSENGER CREW DOOR 841 IAW TASK CARD 26C84152006.SDR USAA2010120792901Fitting · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR30 BETWEEN S39L TO S40L. REPLACED CLEAT AT FR30 BETWEEN S39L TO S40L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231212.SDR USAA2010120692869Accumulator · low pressureFLT 342 - LAS - EES - R2 DOOR ASSIST ACCUMULATOR REQUIRES SERVICING. MAINTENANCE SERVICED R2 DOOR ASSIST ACCUMULATOR IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614-050.SDR USAA2010120692868Slide Raft · faultyFLT 342 - LAS - EES - DURING EMERGENCY LIGHT TEST, L FWD EXT LOAD FAULTED. MAINTENANCE REMOVED AND REPLACED L1 SLIDE RAFT.SDR USAA2010121793119Stiffener · crackedSAL - S5 - MAJOR REPAIR - CRACKS FRONT SPAR OF LEADING EDGE OF LEFT HORIZONTAL STABILIZER INTERNAL AREA OF ACCESS PANEL 331AB. REPAIRED STIFFENER BETWEEN RIB 4 TO RIB 5 OF LEADING EDGE OF LEFT HORIZONTAL STABILIZER INTERNAL AREA IAW EA 133177 & A320 SRM 51-77SDR USAA2010120892925Shear Pin · corrodedSAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN RIB 4 AND RIB 5 ON INNER PIN, LOCATED AT LEFT UPPER FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN RIB 4 AND RIB 5 LOCATED AT LEFT UPPER FROM LINK PIN ASSY OF AFT ENGINE MSDR USAA2010120892924Shear Pin · corrodedSAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN RIB 4 AND RIB 5 ON INNER PIN, LOCATED AT LEFT MIDDLE FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN RIB 4 AND RIB 5 LOCATED AT LEFT MIDDLE FROM LINK PIN ASSY OF AFT ENGINESDR USAA2010120892923Shear Pin · corrodedSAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN RIB 4 AND RIB 5 ON INNER PIN, LOCATED AT RIGHT MIDDLE FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN RIB 4 AND RIB 5 LOCATED AT RIGHT MIDDLE FROM LINK PIN ASSY OF AFT ENGISDR USAA2010120392796Connector · looseFLT 34 - PHX - EEL - SEAT ROW 9 LT EMERGENCY LIGHT ON SEAT INTERMITTENT. MAINTENANCE FOUND LOOSE CONNECTION. RECONNECTED EMERGENCY LIGHT ON SEAT 9 LT.SDR USAA2010121793108Hinge Pin · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON INNER HINGE PIN FOR RIGHT AFT NR 1 ENGINE MOUNT AT PYLON STA 684. REPLACED RIGHT AFT NR 1 ENGINE MOUNT AT PYLON STA 684 IAW A320 AMM 71-22-11.SDR USAA2010121793107Hinge Pin · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON INNER HINGE PIN FOR LEFT AFT NR 1 ENGINE MOUNT AT PYLON STA 684. REPLACED LEFT AFT NR 1 ENGINE MOUNT AT PYLON STA 684 IAW A320 AMM 71-22-11.SDR USAA2010120892927Shear Pin · corrodedSAL - MAJOR REPAIR - S5 - CORROSION WAS FOUND BETWEEN WS 3758 TO WS 4067, BETWEEN RIB 7 AND RIB 8 ON INNER PIN, LOCATED AT RIGHT LOWER FROM LINK PIN ASSY OF AFT ENGINE MOUNT (ENGINE NR 1). REPLACED INNER PIN BETWEEN WING STATION 3758 TO 4067, BETWEEN RIB 7 ANSDR USAA2010120292763Lens · missingFLT 89 - PHX - EEL - LT AFT OVERWING EMERGENCY EXIT SIGN MISSING. MAINTENANCE INSTALLED MISSING EMERGENCY LIGHT LENS COVER ON LT AFT OVERWING DOOR.SDR USAA2010112992673Oil Cooler · leakingFLT 89 PDX-PHX - ODOR - WET, DIRTY SOCK SMELL REPORTED DURING TAXI AND CLIMB - DISSIPATED DURING CRUISE. STRONG ODOR RETURNED DURING DESCENT AND TAXI. MAINTENANCE FOUND EVIDENCE OF OIL LEAK AT APU OIL COOLER - REMOVED AND REPLACED OIL COOLER I/A/W AIRBUS MAISDR USAA2010120192710Eec · faultyFLT 4 ORD-PHX - RTO - DURING TOGA POWER T/O, NR 2 ENGINE EPR SURGED TWICE - DECREASED TO 1.25 FROM 1.4. REJECTED TAKEOFF AT APPROXIMATELY 100 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE FUEL METERING UNIT (FMU) AND ELECTRONIC ENGINE CONTROL (EEC).SDR USAA2010120192709Fmu · faultyFLT 4 ORD-PHX - RTO - DURING TOGA POWER T/O, NR 2 ENGINE EPR SURGED TWICE - DECREASED TO 1.25 FROM 1.4. REJECTED TAKEOFF AT APPROXIMATELY 100 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE FUEL METERING UNIT (FMU) AND ELECTRONIC ENGINE CONTROL (EEC).SDR USAA2010120192716Sill · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION FOUND AROUND NUT PLATE OF LOWER SILL RT SIDE LOCATED FR67+9 INCH. REPAIRED LOWER SILL RT SIDE LOCATED FR67+9 INCH IAW A320 SRM 53-41-14.SDR USAA2010120192715Floorbeam · corrodedSAL - MAJOR REPAIR - S5 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM AT FR 65 + 5 INCH, + Y1215. REPLACED FLOORBEAM AT FR 65 + 5 INCH, + Y1215 IAW A320 SRM 51-72-11.SDR USAA2010112992671Power Supply · inoperativeFLT 211 - LAS - EEL - EMERGENCY LIGHT TEST FAILED RIGHT SIDE 115V AC. POWER SUPPLY UNIT WILL NOT PASS TEST. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT RIGHT SIDE IAW AIRBUS MAINTENANCE MANUAL 33-51-38.SDR USAA2010120192714Seat Track · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON SEAT TRACK LOCATED AT FR 34 + 9 INCHES -Y1292. REPAIRED SEAT TRACK LOCATED AT FR 34 + 9 INCHES -Y1292 IAW A320 SRM 53-21-15.SDR USAA2010121793132Access Panel · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON RIGHT WING FUEL PANEL 640RB BETWEEN RIB 21 AND RIB 22, WS 11664 - WS 11198. REPLACED RIGHT WING FUEL PANEL 640RB BETWEEN RIB 21 AND RIB 22, WS 11664 - WS 11198 IAW A320 SRM 57-27-11.SDR USAA2010121793131Access Panel · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON RIGHT WING FUEL PANEL 640MB BETWEEN RIB 17 AND RIB 18, WS 9704 - WS 9235. REPLACED RIGHT WING FUEL PANEL 640MB BETWEEN RIB 17 AND RIB 18, WS 9704 - WS 9235 IAW TASK CARD 26C60057091.SDR USAA2010120192712Seat Track · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON SEAT TRACK LOCATED AT FR 29+6 INCHES -Y1292. REPAIRED SEAT TRACK LOCATED AT FR 29+6 INCHES -Y1292 IAW A320 SRM 53-00-15 FIG 201.SDR USAA2010120192711Shear Plate · crackedSAL - MAJOR REPAIR - S5 CHECK - CRACK ON SHEAR PLATE AT FR 68 - FR 69, S23R. REPLACED SHEAR PLATE AT FR 68 - FR 69, S23R IAW A320 SRM 51-72-11.SDR USAA2010121793171Fitting · corrodedSAL - MAJOR REPAIR - S5 CHECK - LEVEL 2 CORROSION ON THE NR 2 PYLON LOWER SPIGOT FITTING. REPLACED THE NR 2 PYLON LOWER SPIGOT FITTING IAW EA 133205.
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