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 AWXA200501080Seat Track · corrodedDURING C4 CHECK, DISCOVERED GALVANIC CORROSION ON LT INBOARD SEAT TRACK FROM FR 41 TO FR 47, Y765. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK FROM FR 41 TO FR 47, Y765 IAW AIRBUS 320 SRM 51-42-SDR AWXA200501079Seat Track · corrodedDURING C4 CHECK DISCOVERED EXFOLIATION CORROSION ON LT INBOARD SEAT TRACK AT FR 36 AND Y765. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15 FIG 101. MAINTENANCE REMOVED SEAT TRACK FROM FR 36 TO FR 41 AND Y765 IAW AIRBUS 320 SRM 51-42-11.SDR AWXA200501064Floorbeam · corrodedDURING C4 CHECK DISCOVERED, GALVANIC CORROSION LOCATED ON FLOORBEAM AT FR 68, Y-1292. MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14. REMOVED FLOORBEAM AT FR68, Y-1292 IAW AIRBUS 320 SRM 51-72-11. INSTALLED NEW FLOORSDR AWXA200501018Control Unit · malfunctionedDURING TAKEOFF, LANDING GEAR WOULD NOT RETRACT, ALSO HAD ECAM FAULT FOR MLG SHOCK ABSORBER. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. EMERGENCY WAS NOT DECLARED, GEAR WAS DOWN AND LOCKED. MAINTENANCE REMOVED AND REPLACED NR 2 LGCIU AND ASDR AWXA200500962Wire Harness · damagedORD - EEL - DURING TEST OF EMERGENCY LIGHT SYSTEM, SEAT MOUNTED LIGHT AT SEAT ROW 9R WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT CABLE HARNESS UNDER ROW 9R. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200501012Seat Track · corrodedSAL - MAJOR REPAIR - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE RT INBOARD SIDE AT FR 20+10" Y-765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 20+10" Y-765 ASDR AWXA200501011Fitting · corrodedSAL - MAJOR REPAIR - CORROSION FOUND ON C3 CHECK LOCATED AROUND FITTING AT THE LOWER SILL OF THE FORWARD CARGO DOOR CUTOUT. NO ALLOWABLE DAMAGE LIMITS FOUND IN THE AIRBUS 320 SRM. MAINTENANCE REMOVED AND REPLACED THE FITTING LOCATED ON THE LOWER SILL OF FORWSDR AWXA200501010Seat Track · corrodedSAL - MAJOR REPAIR - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE RT INBOARD SIDE AT FR 36" Y-765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 36" Y-765 AND INSDR AWXA200501005Seat Track · corrodedSAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE RT OUTBOARD SIDE AT FR 39 +3" Y-1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 39 +3" Y-1292 AND INSTALLESDR AWXA200501004Seat Track · corrodedSAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE LT INBOARD SIDE AT FR 39 +10" Y765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 39 +10" Y765 AND INSTALLED NSDR AWXA200501003Seat Track · corrodedSAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE LT OUTBOARD SIDE AT FS 42 +16" Y1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FS 42 +16" Y1292 AND INSTALLESDR AWXA200501002Seat Track · corrodedSAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED ON THE LT OUTBOARD SIDE AT FS 36 +16" Y1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 36 +16" Y1292 AND INSTALLESDR AWXA200501001Seat Track · corrodedSAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED AT LT INBOARD SIDE AT FR 44+7, Y765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 44+7, Y765 AND INSTALLED NEW SEAT SDR AWXA200501000Seat Track · corrodedSAL - DURING C3 CHECK DISCOVERED CORROSION ON SEAT TRACK LOCATED AT RT INBOARD SIDE AT FR 42+17, -Y765. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 42+17, -Y765 AND INSTALLED NEW SESDR AWXA200500999Seat Track · corrodedSAL - DURING C3 CHECK, DISCOVERED CORROSION ON SEAT TRACK LOCATED AT RT OUTBOARD SIDE AT FR 42+17, -Y1292. MAINTENANCE REMOVED CORROSION AND FOUND REWORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-31-15. REMOVED SEAT TRACK AT FR 42+17, -Y1292 AND INSTALLED NESDR AWXA200500963Compressor · stalledCLE - AIR TURNBACK - FLT 281 - DURING TAKEOFF CREW REPORTED COMPRESSOR STALL ON THE NR 2 ENGINE. AIRCRAFT RETURNED TO CLE LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IS REMOVING AND REPLACING THE NR 2 ENGINE AT THIS TIME.SDR AWXA200500957Slide · loosePHX - EES - DURING 4-DAY CHECK WHILE REMOVING GIRT BAR FROM THE L1 DOOR, THE SLIDE DROPPED OUT OF THE BOTTOM. MAINTENANCE REMOVE AND REPLACED THE L1 DOOR SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1C25304. VENDOR FOUND NO FAULTS WITH SLIDE. UNIT WAS OVERHAULSDR AWXA200500954Blades · failedDURING CLIMBOUT, 500 AGL, LOUD BANG ACCOMPANIED WITH ACFT YAWING LT 5-10 FT. ENG RECOVERED IMMEDIATELY. ACFT CONTINUED & LANDED WITHOUT FURTHER EVENT. NO EMERGENCY ACTION TAKEN/DECLARED. MX BORESCOPED BOTH ENGINES TO ENSURE INTEGRITY. NO DEFECTS NOTED ON SDR AWXA200500951Pin · wornAT ROTATION, CREW NOTICED SEVERE VIBRATION FROM MLG AREA. A/C CONTINUED ONTO MSP, CREW FLEW BY TOWER, UNABLE TO DETERMINE IF TIRE DAMAGE HAD OCCURRED. EMERGENCY LANDING DECLARED. MX INSPECTED TIRES, BRAKES & GEAR, NO DEFECTS NOTED. PERFORMED BSCU BITE TESSDR AWXA200500896Wire · brokenLAS - EEL - DURING 8 DAY CHECK DISCOVERED ROW 17 SEAT MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT ROW 17. OPERATIONAL CHECKS WERE GOOD IAW TASK CARD F1C33301.SDR AWXA200500895Wire · brokenLAS - EEL - DURING 8 DAY CHECK, DISCOVERED ROW 12 SEAT MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT ROW 12. OPERATIONAL CHECKS WERE GOOD IAW TASK CARD F1C33301.SDR AWXA200500891Wire Harness · shortedORD - EEL - DURING 4 DAY CHECK, DISCOVERED EMERGENCY EXIT LIGHTING AT LT FORWARD EXIT ROW INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND WIRING HARNESS IAW AIRBUS MM 33-51-19-04. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200500877Battery · dischargedLAS - EEL - DURING 8 DAY CHECK, DISCOVERED AFT LEFT EMERGENCY LIGHT BATTERY PACK INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY BATTERY PACK IAW AMM 33-51-38. OPERATIONAL CHECKS GOOD.SDR AWXA200500853Sensor · failedRNO - EMERGENCY LANDING - FLT 522 - DURING FINAL, RECEIVED GEAR DOWN LOCKED INDICATION BUT HAD GEAR WARNING. DID A FLY BY OF TOWER FOR VISUAL. LANDED IN RNO WITHOUT NOSEWHEEL STEERING AND WAS TOWED TO THE GATE. MAINTENANCE FOUND 15GAA AND 17GAA CONNECTORS OSDR AWXA200500843Manifold · leakingDURING CLIMB HAD GREEN HYDRAULIC FAILURE. AIRCRAFT RETURNED TO PHX, CREW DECLARED AND PREPARED CABIN FOR EMERGENCY. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE GROUND LEAKAGE MEASUREMENT MODULE LEAKING. REMOVE AND REPLACED THE GROUND LESDR AWXA200500949Stringer · corrodedMCN - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION IN SEVERAL LOCATION ON STRINGER 42R, FROM FR 54 + 16" TO FR 58 + 6". MAINTENANCE REMOVED CORROSION ON STRINGER 42R, FROM FR 54 + 16" TO FR 58 + 6", IAW AIRBUS 320 SRM 51-74-00. NO ALLOWABLE DAMAGE LIMSDR AWXA200500934Flap · deterioratedDURING C4 CHECK DISCOVERED COMPOSITE DETERIORATED AT TRAILING EDGE OF THE INBOARD FLAP ON THE LT WING. MAINTENANCE GROUND DOWN AND CLEANED THE SURFACE OF THE INBOARD FLAP, TRAILING EDGE, L/H WING IAW AIRBUS A320 SRM 57-52-00. APPLIED GLASS FABRIC AND LAMINATSDR AWXA200500905Stringer · corrodedSAL - DURING C4 CHECK DISCOVERED CORROSION AT STRINGER 31R, FS 65, INTERNAL STRUCTURE UNDER FLOOR COMPARTMENT. MAINTENANCE REMOVED CORROSION AND NO ALLOWABLE DAMAGE WAS FOUND IN SRM. MAINTENANCE REMOVED STRINGER 31R FROM FS 64 TO FS 67 IAW AIRBUS SRM 51-42-1SDR AWXA200500938Web · corrodedDURING C4 CHECK DISCOVERED CORROSION ON FLANGE OF WEB LOCATED IN THE AFT CARGO COMPARTMENT BETWEEN FS 56 AND FS 57, Y700. NO ALLOWABLE DAMAGE LIMITS FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED WEB IN THE AFT CARGO COMPARTMENT BETWEEN FS 56 AND FS 57, Y700 ISDR AWXA200500935Web · corrodedDURING C4 CHECK DISCOVERED CORROSION ON WEB LOCATED IN THE AFT CARGO COMPARTMENT BETWEEN FS 58 AND FS 59, Y700. WEB WAS REMOVED FROM AFT CARGO COMPARTMENT, BETWEEN FS 58 AND FS 59, Y700 IAW AIRBUS 320 SRM 51-72-11. INSTALLED REPAIR PARTS IAW AIRBUS 320 SRM 5SDR AWXA200500906Seat Track · corrodedSAL - DURING C4 CHECK DISCOVERED CORROSION ON SEVERAL SECTION OF SEAT TRACK LOCATED BETWEEN FS 36 AND FS 47, BUTT LINE Y765 AND Y-1292. MAINTENANCE REMOVED ALL CORROSION FROM SEAT TRACKS BETWEEN FS 36 AND FS 47, BL Y765 AND Y-1292 IAW AIRBUS 320 SRM 51-74-00.SDR AWXA200500889Seat Track · corrodedDURING C4 CHECK, DISCOVERED CORROSION ON THE RT OUTBOARD SEAT TRACK FS 41+10, -Y1292. MAINTENANCE REMOVED CORROSION IAW A320 SRM 51-75-00 AND FOUND REWORK TO BE OUT OF LIMITS IAW A320 SRM 53-31-15. RT OUTBOARD SEAT TRACK, AT FR 41+10, -Y1292, WAS REMOVED IAWSDR AWXA200500882Fitting · corrodedDURING C4 CHECK DISCOVERED CORROSION ON LOWER SILL OF L1 DOOR, FROM FS 16 TO FS 20, Y 1584. NO ALLOWABLE LIMITS FOUND. MAINTENANCE REMOVED AND REPLACED THE FITTINGS ON L1 DOOR, LOWER SILL, FROM FS 16 TO FS 20, Y 1584, IAW AIRBUS 320 SRM 51-72-11.SDR AWXA200500880Fitting · corrodedDURING C4 CHECK, DISCOVERED CORROSION AROUND HOLES ON R1 DOOR LOWER SILL FROM FS 16 TO FS 20. NO ALLOWABLE LIMITS EXIST. MAINTENANCE REMOVED AND REPLACED THE FITTINGS ON R1 DOOR LOWER SILL IAW AIRBUS 320 SRM 51-72-11.SDR AWXA200500950Shear Web · crackedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CRACK IN SHEAR WEB BETWEEN FR 68 AND FR 68+13", AND BETWEEN -Y1190 AND -Y1432. MAINTENANCE REMOVED CRACKED SHEAR WEB BETWEEN FR 68 AND FR 68+13", AND BETWEEN -Y1190 AND -Y1432 IAW AIRBUS 320 SRM 51-42-11. INSTSDR AWXA200500937Cover · corrodedDURING C4 CHECK DISCOVERED CORROSION ALONG LOWER SILL COVER SHEET, UPPER SURFACE, FROM FS 52A TO FS 56 IN THE AFT CARGO COMPARTMENT. MAINTENANCE MECHANICALLY REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-49. REMOVED COVER SHEET ANDSDR AWXA200500936Web · corrodedDURING C4 CHECK DISCOVERED CORROSION ON WEB NEXT TO FORWARD FRAME OF THE R1 DOOR, FS 16 TO FS 14, -Y1379.5. MAINTENANCE REMOVED CORROSION IAW AIRBUS 320 SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS AVAILABLE. MAINTENANCE FABRICATED DOUBLER IAW AMERICA WEST ENGISDR AWXA200500904Sill · corrodedSAL - DURING C4 CHECK DISCOVERED SILL SHAPE LOCATED AT FS 68-8" ON CABIN FLOOR STRUCTURE. MAINTENANCE REMOVED SILL SHAPE LOCATED AT FR 68-8" ON CABIN FLOOR STRUCTURE IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW FASTENERS AND SILL SHAPE AT FS 68-8", CABIN FLOORSDR AWXA200500902Floorbeam · corrodedSAL - DURING C4 CHECK DISCOVERED CORROSION ON FLOORBEAM LOCATED AT +Y1180 AND BETWEEN FR 66+4" AND FR 68-5". MAINTENANCE REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-14 FIG 102. MAINTENANCE REMOVED FLOORBEAM AT +Y1180 AND BETWEEN SDR AWXA200500893Floor Support · corrodedDURING C4 CHECK, DISCOVERED CORROSION ON LONGITUDINAL BEAM BETWEEN FS 68 TO FS 69, BL +Y1170. REMOVED CORROSION IAW A320 SRM 51-74-00 AND WAS FOUND TO BE OUT OF LIMITS. REMOVED BEAM BETWEEN FS 68 TO FS 69 IAW AIRBUS 320 SRM 51-42-11. NEW BEAM WAS PREPARED FSDR AWXA200500892Structure · corrodedDURING C4 CHECK, DISCOVERED CORROSION ON EXTRUSION AT R2 DOOR CUTOUT, BETWEEN FS 66 +5, AND FS 68 -5, BL -Y1465. MAINTENANCE REMOVED CORRODED EXTRUSION AT R2 DOOR CUTOUT BETWEEN FS 66 +5 AND FS 68 -5 IAW AIRBUS 320 SRM 51-42-11. INSTALLED NEW EXTRUSION AT R2SDR AWXA200500890Floor Support · corrodedDURING C4 CHECK, DISCOVERED CORROSION ON LONGITUDINAL BEAM BETWEEN FS 65-5 TO FS 69+4, -Y1170. REMOVED CORROSION IAW A320 SRM 51-74-00 AND WAS FOUND TO BE OUT OF LIMITS. REMOVED BEAM BETWEEN FS 65-5 TO FS 69+4 IAW AIRBUS 320 SRM 51-42-11. NEW BEAM WAS PREPASDR AWXA200500888Seat Track · corrodedDURING C4 CHECK, DISCOVERED CORROSION ON SEAT RAIL BETWEEN FS 64 AND FS 66+5, -Y1292. MAINTENANCE REMOVED CORROSION FROM SEAT RAIL AND FOUND RE-WORK TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-00-15. REMOVED CORRODED SEAT RAIL FROM FS 64 TO FS 66+5 IAW AIRBUS SDR AWXA200500887Dummy Rail · corrodedDURING C4 CHECK DISCOVERED GALVANIC CORROSION ON DUMMY RAIL FROM FS 66+5 TO FS 68-5, FROM -Y1170 TO -Y1292. REMOVED CORROSION FROM DUMMY RAIL, FROM FS 66+5 TO FS 68-5, FROM -Y1170 TO -Y1292 IAW AIRBUS 320 SRM 51-74-00. REWORK FOUND TO BE OUT OF LIMITS IAW AISDR AWXA200500886Floor Support · corrodedDURING C4 CHECK, DISCOVERED CORROSION AT LONGITUDINAL FLOOR SUPPORT, LOCATED AT -Y81, FR 14. NO ALLOWABLE LIMITS FOUND. MAINTENANCE REMOVED FLOOR SUPPORT AT -Y81, FR 14 IAW AIRBUS SRM 51-42-11. INSTALLED NEW FLOOR AT -Y81, FS 14 BEAM IAW AIRBUS SRM 51-42-11SDR AWXA200500885Threshold · corrodedDURING C4 CHECK DISCOVERED CORROSION ALONG LOWER SILL THRESHOLD SHEET IN THE AFT CARGO COMPARTMENT FROM FS 52+9.5 TO FS 56. MAINTENANCE REMOVED LOWER SILL THRESHOLD SHEET IN THE AFT CARGO COMPARTMENT IAW AIRBUS SRM 51-42-11 PAGE 2. FABRICATED NEW THRESHOLD SSDR AWXA200500884Web · corrodedDURING C4 CHECK DISCOVERED EXFOLIATION CORROSION ON WEB, LOCATED AT -Y1180, FROM FS 69 TO FS 70. MAINTENANCE REMOVED CORRODED WEB FROM FS 69 TO FS 70, -Y1180 IAW AIRBUS SRM 51-72-11 PAGE 1 AND 2. INSTALLED NEW WEB IAW AIRBUS SRM 51-72-11 PAGES 1 AND 2.SDR AWXA200500883Support · corrodedDURING C4 CHECK, DISCOVERED CORROSION ON SUPPORT, LOCATED AT FR 70 - 4, -Y 1180, UNDER STRINGER 23R. MAINTENANCE REMOVED CORRODED SUPPORT AT FR 70 - 4, -Y1180, UNDER STRINGER 23R. PREPARED NEW SUPPORT FOR INSTALLATION IAW AIRBUS MM 51-25-00. INSTALLED REPAISDR AWXA200500881Web · corrodedDURING C4 CHECK, DISCOVERED CORROSION ON WEB NEXT TO R1 DOOR, FRAME 20, -Y1584. NO ALLOWABLE DAMAGE LIMITS FOUND IN AIRBUS SRM 53-11-14. MAINTENANCE REMOVED CORRODED NEXT TO R1 DOOR, FS 20 IAW AIRBUS SRM 51-72-11. PREPARED NEW WEB FOR INSTALLATION IAW AIRBUSDR AWXA200500879Floorbeam · corrodedDURING C4 CHECK, DISCOVERED CORROSION ON FLOORBEAM Y-254, FROM FS 16 TO FS 19. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM AT Y -254, FROM FS 16 TO FS 19 IAW AIRBUS SRM 53-11-14 FIG 202. PREPARED NEW FLOORBEAM FOR INSTALLATION IAW AIRBUS SRM 53-11-14 A
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