Airbus A320-232

Service difficulty reports · 32,653

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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 = 'A320232'
  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 YENA2018110530740Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN AT FRAME 42, +Y1292. REPAIRED THE SKIN IAW EC A18-886-01, AND EA 57-0294--18.Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2018110530739Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON STRINGER 37L, FRAMES 60 AND 64 IN THE AFT CARGO BAY. PERFORMED A PERMANENT REPAIR ON THE STRINGER IAW EC A18-880-01, AND EA 53-0296-18,Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2018110530738Web · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SUPPORT WEB LEVEL STR 23R AND BETWEEN FR 69 AND FR 70 AT AFT GALLEY AREA; REF AEROMAN WO 934679, NR 2018-343796, REPLACED SUPPORT WEB LEVEL STR 23R AND BETWEEN FR 69 AND FR 70 AT AFT GALLEY AREA I.A.W.SRM Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018110530737Web · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SUPPORT WEB LEVEL STR 23L AND BETWEEN FR 69 TO FR 70 AT AFT GALLEY AREA; REF AEROMAN WO 934679, NR 2018-343797, REPLACED SUPPORT WEB LEVEL STR 23L AND BETWEEN FR 70 AT AFT GALLEY AREA I.A.W. SRM A320 51-72Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018110530736Structure · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL BETWEEN FR 66 TO FR 67 AT LEVEL STR 23L AT AFT GALLEY AREA; REF AEROMAN WO 934679, NRC 2018-343822 ,REPLACED LOWER SILL BTW FR 66 TO FR 68 AT LEVEL STR 23L AT AFT GALLEY AREA I.A.W. SRM A320 51-7Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811053735Dummy Rail · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE DUMMY RAIL, Y503.2, BETWEEN FRAMES 12 TO 16. REPLACED THE DUMMY RAIL IAW SRM 51-72-11, AND DRAWING D53112825.Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA201811053734Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, +Y1292, BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT.Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811053733Structure · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER CORNER, STRINGER 23L AND FRAME 68. REPLACED THE CORNER IAW SRM 51-72-11, AND DRAWING D53480505.Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201811053732Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS FOUND ON THE CENTER WING BOX TOP SKIN UPPER SURFACE BETWEEN FRAMES 41 - 42, +Y1292. REPAIRED.Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR GTIA2018110532942Bottle · low pressureL2 DOOR ASSIST BOTTLE PRESSURE WAS LOW. SERIVED THE DOOR ASSIST BOTTLE IAW AMM 52-10-00.Nov 3, 2018 · N625NK · Airbus A320232 · Emergency EquipmentSDR AALA2018110659051Pressure Switch · failedCABIN PRESSURE LIGHT FLASHED WHEN DOOR DISARMED. CABIN DEPRESSURIZED WITH COCKPIT WINDOW. REPLACED PRESSURE SWITCH. ACCOMPLISHED OPERATIONS CHECK OF THE SYSTEM PER AMM 52-73-12-A, AND LOW RANGE LEAK CHECK IAW AMM 34-21-00.Nov 2, 2018 · N665AW · Airbus A320232 · Cabin Pressure Control SystemSDR AALA2018110659050Pressure Switch · failedL2 DOOR CABIN PRESSURE LIGHT ILLUMINATED WHEN DOOR DISARMED, CABIN DEPRESSURIZED WITH COCKPIT WINDOW OPEN. REPLACED PRESSURE SWITCH. OPS CHECKED IAW AMM 52-73-12, AND LOW RANGE LEAK CHECKED IAW AMM 34-21-00.Nov 2, 2018 · N665AW · Airbus A320232 · DoorsSDR CALA2018110502270Skin · dentedAFT FUSELAGE EXTERNAL SURFACE FR 63 STR 41L HAS A DENT - A3NB-05 -3-6003 - GENERATED BY N078570 AT HAECO LCQ PER N/R 9297297 REPAIRED AFT FUSELAGE SKIN AT FR63, STR 41L PER SRM 53-00-11-800 -004.REMOVED DOUBLER AND CLEAT AT FR63 STR41L-STR42L. FABBED & I NSTALNov 2, 2018 · N422UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2018110502279Frame · cracked(SUPPORT TASK) (A-38 NO DOT) L/H FWD EMERGENCY EXIT 833 R/H VER TICAL FRAME CRACKED AAR NONROUTINE 9813987 REMOVED AND REPLACED L/H FWD EMERGENCY EXIT 833 R/H VERTICAL FRA ME IAW A320 SRM 51-42-11-001 PARA 2.E. AAR NONROUTINE 9813987 ADD EMP:V919097Nov 2, 2018 · N457UA · Airbus A320232 · Emergency ExitsSDR CALA2018110502278Frame · cracked(SUPPORT TASK) (A-38) NO DOT) R/H FWD EMERGENCY EXIT 843 R/H VER ICAL FRAME CRACKED AAR NONROUTINE 9813988 REMOVED AND REPLACED CRACKED FRAME AT R/H FWD EMERGENCY EXIT, IA W A320 SRM 51-42-11. AAR NONROUTINE 9813988 ADD EMP:V925284Nov 2, 2018 · N457UA · Airbus A320232 · Emergency ExitsSDR CALA2018110502277Frame · crackedA3NB-05-3-6159 A34-26 RH FWD EMERGENCY EXIT 843 LH VERTICAL F RAME CRACKED. AAR NONROUTINE 9813613 REMOVED AND REPLACED CRACKED FRAME AT L/H VERTICAL OF DOOR, R/H FWD EMERGENCY EXIT IAW A320 SRM 51-42-11 AAR NONROUTINE 98136 13 ADD EMP:V925284Nov 2, 2018 · N457UA · Airbus A320232 · Emergency ExitsSDR CALA2018110502276Frame · crackedA3NB-05-3-6159 A34-24 LH AFT EMERGENCY EXIT 834 AFT VERTICAL FRAMES CRACKED 2PL AAR NONROUTINE 9813595 REMOVED AND REPLACED LH AFT EMERGENCY EXIT AFT VERTICAL FRAME IA W A320 SRM 51-42-11, 51-72-11, 51-24-00-001, 51-23-11-001, 51-23 -12-001 AAR NONROUNov 2, 2018 · N457UA · Airbus A320232 · Emergency ExitsSDR CALA2018110502275Frame · cracked(SUPPORT TASK) A-38 NO-DOT) L/H AFT EMERGENCY EXIT 834 FWD VERTI CAL FRAME CRACKED AAR NONROUTINE 9813986 REMOVED AND REPLACED LH AFT EMERGENCY EXIT FWD VERTICAL FRAME IA W A320 SRM 51-42-11, 51-72-11, 51-23-12-001, 51-24-00-001. AAR NONROUTINE 9813986 ADD Nov 2, 2018 · N457UA · Airbus A320232 · Emergency ExitsSDR CALA2018110502274Door Sill · corroded(A2NB-53-3-6186 L22-007) R2 SILL CORRORED ON I/B EDGE JUST FWD OF FR68 AAR NONROUTINE 9019745 BLENDED CORROSION ON R2 DOOR SILL I/B EDGE FWD OF FRAME 68. FOUN D TO BE OUT OF LIMITS IAW A320 SRM 53-41-14-283-002 REPAIRED R2 DOOR SILL IAW A320 SRM 53-41-14-Nov 2, 2018 · N420UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018110502273Door Sill · corrodedR2 DOOR SILL HAS CORROSION JUST FWD OF FR 68 (A3NB-53-3-6299) PE R HAECO LCQ NON ROUTINE 9296602 GENERATED BY V061742 REMOVED & REPLACED R2 DOOR SILL P/N D5348004320701 PO NO. 105411 6.1 IAW A320 SRM 51-72-11-911-001 AT HAECO LCQ ON HANGAR NR 9296 602 BY MECH Nov 2, 2018 · N424UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018110302269Stringer · corrodedLT FR56 TO FR57 STR43 EVIDENCE OF CORROSION. REMOVED AND REPLACED CORRODED SECTION OF STRINGER 43 BETWEEN FR56 & FR57. SPLICED IN SECTION WITH 2 COUPLINGS PER SRM-53-00-13-3 00-001 PG 8. ALODINED, PRIMED & TOP COATED.Nov 2, 2018 · N422UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2018110302268Plate · damagedWHILE PERFORMING REPAIR ON +Y1292 AT FR24 DAMAGE WAS FOUND ON CROSSBEAM AFT VERTICAL FACE AROUND 5 HI LOKS. REMOVED & REPLACED FR24 UPPER FISHPLATE, P/N D5323252020000 AND LOWERFISH PLATE, P/N D5323074920000 IAW SRM 51-42-11-001, AND SRM 51-72-11.Nov 2, 2018 · N457UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA2018110202934Warning Message · false activationDURING APPROACH, RECEIVED A F/CTL SLATS FAULT, NO ASSYMETRY FELT, CYCLED FLAP HANDLE, AFTER SECOND ATTEMPT, RETURNED TO NORMAL. PERFORMED DETAILED VISUAL INSPECTION OF THE SLATS TRANSMISSION SYS IAW AMM 27-84-00-200-001, INSPECTED THE TORQUE LIMITER AND CNov 2, 2018 · N635NK · Airbus A320232 · Leading Edge Slat Control SystemSDR YENA2018110830766Exhaust Vent · corrodedFT # 344, STI-FLL. FOUND LAV EXHAUST VENT CORRODED DURING WALK AROUND; REF HAECO NR 440531-32003, REMOVED CORROSION AND INSTALLED REPAIR IAW A320 SRM 53-41-11-300-004. AT FR 69 TO 70 STR 31 RH. REPAIR IS A CAT A PERMANENT NO SRI REQUIRED.Oct 31, 2018 · N586JB · Airbus A320232 · Fuselage Main, StructureSDR YENA201811021725Light · inoperativeSEAT 7ABC, EMERGENCY LIGHT WAS INOPERATIVE. R & R EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-18. OPS CHECKED OK.Oct 31, 2018 · N625JB · Airbus A320232 · Emergency LightingSDR YENA20181102724Unknown · odorCOCKPIT/CABIN HAD AN ODOR WHILE DESCENDING FROM 370 - 330. F/A CALLED ABOUT ODOR ROW 21-25. BURNING ELEC. METALIC ODOR IN COCKPIT. ACCOMPLISHED ODOR RECOGNITION AND ISOLATION PROCEDURE FCOM VOL-1 PACK 1 OFF 3-5 MIN. ODOR DISSIPATED, KEPT CONFIGURATION THROUGOct 31, 2018 · N507JT · Airbus A320232 · Air Distribution SystemSDR AALA201811019016Panel · looseTHE AIRCRAFT WAS NOT GROUNDED. LOWER EMERGENCY EXIT LIGHT PANEL BY 1L IS LOOSE. EXIT SIGN IS UPSIDE DOWN. SECURED PANEL AND REMOUNTED LIGHT. OK FOR SERVICE.Oct 31, 2018 · N680AW · Airbus A320232 · Emergency LightingSDR CALA2018110202244Fitting · corrodedUPON REMOVING AFT CARGO THRESHOLD FOUND AFT LWR CORNER FITTING H AS CORROSION. R&R AFT CARGO COMPARTMENT AFT CORNER FITTING AT FR56 ON RIGHT HAND SIDE IAW SRM 51-42-11-001.Oct 30, 2018 · N422UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018110202243Cleat · corrodedFWD CARGO FR 31 BETWEEN STR 41R-42R CLEAT HAS CORROSION FCD 530 0-01440. R&R CLEAT AT FRAME 31 BTWN STR 41R-42R IAW SRM 51-42-11-001.Oct 30, 2018 · N422UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018110202242Hinge Fitting · damagedVERT STAB RUDDER HINGE FITTING 2, 4 AND 5 IS DAMAGED. R&R HINGE FITTINGS NR 2, NR 4 AND NR 5 ON VERTICAL STAB IAW SRM 55-36-41-000-001-A & AMM 55-36-41-400-001-A.Oct 30, 2018 · N422UA · Airbus A320232 · Rudder StructureSDR CALA2018110202241Intercostal · damagedFWD CARGO PIT RT SIDE INTERCOSTAL AT FR29-30, STR 38R HAS OUT OF ROUND AND DOUBLE DRILLED HOLES. R&R INTERCOSTAL AT FR29-FR30, STR38R IAW SRM 51-72-11-911-001 AND SRM 51-42-11-001 PARA 2E AND 2F.Oct 30, 2018 · N422UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018110202239Cleat · corrodedFWD CARGO FR28 BETWEEN 41R-42R CLEAT IS CORRODED. REMOVED, FABRICATED AND INSTALLED CLEAT IN FWD CARGO FR28 BTWN STR 41R-42R IAW DRAWING D53230537, SRM 51-26-00-001 AND 51-7 0-12-001. TREATED/PRIMED IAW SRM 51-21-A-001. TOPCOATED IAW SRM 51-75-12-0013C.Oct 30, 2018 · N422UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018110202238Stringer Splice · corrodedFWD CARGO FR 26-34 STR 41L HAS CORROSION AROUND FASTENER HOLES. REMOVED CORROSION BY BLENDING IAW SRM 53-21-13-283-001. MATERIAL LOSS OF .003 FOUND TO BE WITHIN LIMITS IAW SRM 53-21-13-283-001. REMOVED AND REPLACED STRINGER SPLICE AT FR30-FR31 STR 41L IAW SRM Oct 30, 2018 · N422UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2018110202237Fitting · corrodedUPON REMOVING AFT CARGO THRESHOLD FOUND FWD LWR CORNER FITTING H AS CORROSION. R&R AFT CARGO FWD LWR CORNER FITTING IAW SRM 51-42-11.Oct 30, 2018 · N422UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018110230723Battery · no testEPSU BATTERY 11WL FAILED EMERGENCY LIGHT SYSTEM TEST. R & R THE BATTERY 11WL IAW AMM 33-51-38, EMERGENCY LIGHT SYSTEM CHECKED GOOD.Oct 30, 2018 · N529JB · Airbus A320232 · Emergency LightingSDR AALA201811019017Switch · defectiveTHE AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT REPORTS ALL EMERGENCY LIGHTS ON. OCCURRED WITH COCKPIT SWITCH IN ARM. WITH SWITCH OFF, ALL EMERGENCY LIGHTS EXTINGUISHED. REPLACED EMERGENCY LIGHT SWITCH PER TSM 33-51-00-810-881. OPERATIONS CHECK GOOD.Oct 30, 2018 · N665AW · Airbus A320232 · Emergency LightingSDR YENA201810290950Skin · corrodedDURING C6 CHECK AT SAL, THE RT APU DOOR (PN: D5248570001000 SN: 13500) WAS FOUND WITH CORROSION WITH SKIN PENETRATION AT THE OUTER SKIN. DUE TO THE DAMAGE LOCATION (ZONE 2) AND MAGNITUDE OF THE CORROSION, NO REPAIR IS AVAILABLE ON THE SRM, HENCE THE REASON FOROct 29, 2018 · N709JB · Airbus A320232 · Auxiliary Power Unit (APU) DoorsSDR YENA201810290946Box Beam · crackedDURING HEAVY MAINTENANCE, C6 CHECK AT LHT (BQN), LHT REPORTED THAT AFTER ACCOMPLISHMENT OF ROTOTEST INSPECTION REQUIRED PER REF /4/ SB & REF /6/ AD- CRACKS WERE FOUND ON THE UPPER FLANGE OF THE LT SIDE (CENTER & AFT HOLE) AND RT SIDE (AFT HOLES) SIDE BOX BEAMSOct 29, 2018 · N709JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018110529731Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE SKIN AT THE ANTENNA CUTOUT, FRAMES 60 - 61, STRINGERS 1L - 1R. REPAIRED IAW SRM 53-41-11-283-001, REPAIR CATEGORY B, AND SRM 53-41-11-283-001, DIAGRAM 1, SHEET 2.Oct 29, 2018 · N709JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2018110529730Flange · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON OUTER FLANGE FOUND AT FRAMES 60 - 61, STRINGER 37. REWORKED THE OUTER FLANGE IAW EO A32F-53-5231-00.Oct 29, 2018 · N709JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018110529729Flange · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE OUTER FLANGE, FRAMES 56 - 57, STRINGER 38L. REWORKED THE OUTER FLANGE IAW EO A32F-53-5231-00.Oct 29, 2018 · N709JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018110529728Flange · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE OUTER FLANGE, FRAMES 59 - 60, STRINGER 38L. REWORKED THE OUTER FLANGE IAW EO A32F-53-5231-00.Oct 29, 2018 · N709JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018110529727Flange · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON OUTER FLANGE, FRAMES 55 - 56, STRINGER 38. REWORKED OUTER FLANGE IAW EO A32F-53-5231-00.Oct 29, 2018 · N709JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2018110529726Flange · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE OUTER FLANGE, FRAMES 54 - 55 STRINGER 38. REWORKED THE OUTER FLANGE IAW EO A32F-53-5231-00.Oct 29, 2018 · N709JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018110202233Fitting · corrodedL1 DOORSILL CORRODED AROUND AFT GIRT BAR FITTING AFT OUTBOARD HOLE. CORROSION REMOVED, NDT'D, AND REPAIR WASHER INSTALLED PER SRM 53-11-14-283-005 FIG 10108 SHEETS 1-5.Oct 29, 2018 · N420UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018110202232Door Sill · corrodedAFT CARGO PIT DOOR THRESHOLD HAS CORROSION AROUND THE FWD NR 2 TIEDOWN FITTING AND ALONG THE OUTER EDGE FR 53-56. REMOVED AND REPLACED AFT CARGO DOOR SILL IAW SRM 51-42-11-0 01. INSP COMPLIED WITH.Oct 29, 2018 · N457UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA2018103109023Actuator · defectiveNR 2 ENGINE COMPRESSER VANE 60-80 KTS REJECT TAKE OFF. THE AIRCRAFT WAS GROUNDED. REPLACED ENGINE 2 VSV ACTUATOR PER JOB CARD 26T40075005. POWER ASSURANCE TEST PER JOB CARD 26L00071014. AIRCRAFT OK FOR SERVICE.Oct 29, 2018 · N647AW · Airbus A320232 · Turbine Engine Compressor SectionSDR GTIA2018102902928A/C Pack · odorWET SOCK ODOR IN AFT CABIN REPORTED ON CLIMB OUT ISOLATED PACK 2. ODOR DISSIPATED. PERFORMED TSM 05-50-00-810-831. INSPECTED APU, ENG NR 1 & NR 2 NO OIL LEAKS NOTICED AT THIS TIME. SMELL ISOLATED TO PACK NR 2. PACK NR 1 OK, NO ODOR AT THIS TIME.Oct 29, 2018 · N644NK · Airbus A320232 · Cabin Cooling SystemSDR CALA2018102902229Stringer · corrodedLT FR56 TO FR57 STR43 EVIDENCE OF CORROSION A3NB-53-4-6179 GENERATED ON NR 9296814 REMOVED AND REPLACED CORRODED SECTION OF STRINGER 43 BETWEEN FR5 6 & FR57. SPLICED IN SECTION WITH 2 COUPLINGS PER SRM-53-00-13-3 00-001 PG 8. ALODINED, PRIMED & TOP COATED. SRIOct 29, 2018 · N422UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2018102902227Door Sill · corroded(CUSTOMER REQUEST) AFT CARGO PIT DOOR THRESHOLD HAS CORROSION AROUND THE FWD NR 2 TIEDOWN FITTING AND ALONG THE OUTER EDGE FR 53-56. N/R 9813949. REMOVED AND REPLACED AFT CARGO DOOR SILL IAW SRM 51-42-11-0 01. INSP. COMPLIED WITH.Oct 29, 2018 · N457UA · Airbus A320232 · Fuselage Miscellaneous Structure
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