Airbus A320-232
Service difficulty reports · 32,653
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 = '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.
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
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 YENA2021093000627Stringer · corrodedDURING HEAVY MIANTENANCE, (REF. AEROMAN N/R 2021-393852) CORROSION STRINGER 39R BTW FR31 TO FR32 IN FWD CARGO COMPARTMENT; (PER AEROMAN N/R 2021-393852) R & R STRINGER 39R LOC. BTW FR30 TO FR35 IN FWD CARGO COMPARTMENT I.A.W A320 SRM 51-72-11 DRAWING D53231962SDR AALA202109246782Power Supply · failedAIRCRAFT WAS NOT GROUNDED: AFT LEFT HAND SEAT EMERGENCY LIGHT OUT. REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38-401.SDR CALA2021092401673Skin · crackedAFTER ULTRASOUND INSPECTION AS PER EA 5300-02254 REV B STEP 2.2 REF. (NTM 51-10-15-270-801-A-01) AT DOUBLER REPAIR FOUND INDICATION OF CRACK. EVALUATE ACCORDINGLY, AS NOTED ON LTPR NR# 5001090137-0010. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF LATEST RSDR CALA2021092401672Battery Pack · noneBRAKE 2 OVERHEATED ONCLIMB DEN THEN ONPARKING SLC WAS 420..BRAKE 1 350 UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. REF MT 32-001 FOR POSSIBLE DRAGGING BRAKES , PLEASE JACK ACFT UP AND ATTEMPT TO ROTATE IF YOU FESDR CALA2021092401671Connector · brokenCONNECTOR BACKSHELLS FOUND BROKEN 202 WL-A. REPLACED CONNECTOR BACKSHELLS 202 WL-A IAW ESPM 20-53-45-02 REV 41 AND AWM 33-51-02 PAGE 203 SHEET 1 AND 2 REV 114. PERFORMED OPC CONTINUITY CHECK IAW ESPM 20-52-21. REV 41 AND IAW AWM 33-51-02 SHEET 1 AND 2 REV 114.SDR CALA2021092401670Connector · brokenCONNECTOR BACKSHELL 205WL-A NEEDS REPLACEMENT. REPLACEMENT OF CONNECTOR BACKSHELL 205 WL-A WAS PERFORMED IAW ESPM 20-53-45-02 REV 41. AND AWM 33-51-02 PAGE 203 SHEET 1 AND 2 REV 114. PERFORMED CONTINUITY CHECK IAW ESPM 20-52-21 REV 41 AND IAW AWM 33-51-02 SHEESDR CALA2021092401669Connector · brokenREPLACEMENT OF THE CONNECTOR BACKSHELL 203WL-A IS NEEDED. REPLACEMENT OF CONNECTOR BACKSHELL 203WL-A WAS PERFORMED IAW ESPN 20-53-45-02 REV 41 AND AWM 33-51-02 PAGE 203 SHEET 1 AND 2 REV 114. PERFORMED CONTINUTY CHECK IAW ESPM 20-52-21 REV 41. AND AWM 33-51-02SDR CALA2021092401668Skin · corrodedCORROSION ON FASTENERS AND ADJACENT STRUCTURES 7113VC AND 7102VC HOLE AND SURROUNDING STRUCTURES BTW FRAME 66-70 STRG 3L-3R IAW SRM 53-41-11-283-865 REV.137 INSTALLED 2EA DOUBLERS ON AREA 7102VC AND 7113VC IAW A320 SRM 51-42-11, SRM 51-43-00 REV 137 AND EO A32SDR CALA2021092401667Stringer · corrodedCORROSION ON STRG 37R AND STRG 38R BTW FR56-58. REPLACED STRG 37R AND STRG 38R BTW FR56-58 IAW 320 SRM 51-72- 11; SRM 51-42-11 REV 137. THIS REPAIR BY REPLACEMENT IS CLASSIFIED AS MAYOR CAT "A" REPAIR WITH NO ADDITIONAL REQUIREMENTS.SDR CALA2021092401665Beam · corrodedCORROSION ON CABIN FLOOR BEAM Y-765 AT FR20 (A3NB-53-3-6038)SDR CALA2021092401662Epsu · no testFOR SCEPTRE TRACKING PURPOSE ONLY REMOVE AND REPLACE (A3NB-33-3- 6013) OPC EMERGENCY LIGHTING BATTERY CAPACITY WAS PERFORMED AND FAIL. THE TWO MESSAGES WERE EPSU UNIT FWD L AND EPSU BAT CAP AFT L. TROUBLE SHOOTING REQUIRED. FOR SCEPTRE TRACKING PURPOSE ONLY RESDR CALA2021092401664Beam · corrodedCORROSION ON AFT CABIN FLOOR BEAM Y1162.5 AT FR68. (A3NB-53-3-62 22)SDR CALA2021092401663Epsu · no testEPSU UNIT FAIL OPC/ REMOVAL OF THE EPSU 10WL IAW AMM 33-51-38- 000-001-A REV 113. INSTALLATION OF ESPU 10WL IAW AMM 33-51-38-400-001-A. REV 113 PERFORMED OF A BITE TEST IAW AMM 33-51-00-710-001 A REV 113.SDR CALA2021092401666Seat Track · corrodedCORROSION ON CABIN FLOOR BEAM Y-1292 AT FR20. (A3NB-53-3-6038)SDR YENA2021093000626Slide · out of positionDURING HEAVY MAINTENANCE, ESCAPE SLIDE DOOR 841 TOUCHES THE FUSELAGE PER AMM 25-62-44-400-803-A POCEDURE 4.B.12 (C) ; (REF AEROMAN NR 2021-382146) R & R SLIDE RAFT 841 PER AMM 25-62-44-000-803-A & 25-62-44-400-803-A OPS CHECKS OK. SUPPLEMENTAL INFORMATION TO FSDR YENA2021093000625Support · corrodedDURING HEAVY MAINTENANCE, CORROSION ON LOWER SILL, LH FR 69, AFT GALLEY AREA (CPCP RELATED TASK MPD 534195-01); REMOVED CORROSION ON REWORK AREAS P1, P2, & P3 IAW A320 SRM 51-73-00 & ISRM 51-74-00 AND FOUND P2 & P3 TO BE WITHIN LIMITS PER SRM 53-41-14-283-002,SDR YENA2021093000624Shear Plate · corrodedDURING HEAVY MAINTENANCE, CORROSION SHEAR PLATE STR 23RH BTW FR69 & FR 70, AFT GALLEY AREA ( CPCP RELATED REFER TO MPD 534195-01); R & R SHEAR PLATE STGR 23 R, BTW FR69 & FR 70, AFT GALLEY AREA (CPCP RELATED MPD TASK 534195-01). NOTE: REPAIR WAS ACCOMPLISHED SDR YENA2021093000623Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM SYTRUCTURE L/H WEB BTW FR69 AT AFT GALLEY AREA (CPCP RELATED REFER TO MPD TASK 534195-01); R & R FLOOR STRUCTURE LH WEB BTW FR69 AND FR70 AT AFT GALLEY AREA IAW SRM A320- 51-72-11 AND DWG D534-74180. WORK WAS ACCOSDR YENA2021093000622Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION ON FLOOR BEAM +Y765, FR 68, AT AFT GALLEY AREA (REF CPCP MPD TASK 534195-01); R & R FLOOR BEAM Y765 AT AFT GALLEY AREA IAW A320 SRM 51-42-11 AND A320 SRM 51-72-11, DWG D534-72795 AND DWG D534-78913. REPAIR WAS ACCOMPLISHED ASDR YENA2021093000621Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR STRUCTURE LH WEB BTW FR69 & FR 70 AT AFT GALLEY AREA (CPCP RELATED REFER TO MPD TASK 534195-01); R & R FLOOR STRUCTURE LH WEB BTW FR 69 AND FR 70 AT AFT GALLEY AREA IAW SRM A320 51-72-11 AND DWG D534-74180. REF AEROMANSDR CALA2021092401661Fitting · corrodedCORROSION-R2 DOOR STILL BEAM GRT BAR FIT ZONE 261 SEQ 2282 A3NB-53-3-6222 AS NOTED ON LTPR NR# 5001085231-0130. REPAIR IS A CAT-A MAJOR AND PERMANENT REPAIR. NO FURTHER ACTION REQUIRED IAW EC/RA 5311-02643 WITH LHT-PR EO A320-53-10796-00-FINAL. NO RE-ISPECTIONSDR CALA2021092401660Beam · corrodedCORROSION ON AFT CABIN FLOOR BEAM UPPER INBD SPLICE ANGLE (LOWER SURFACE) AT Y-1162.5 FR68 (A3NB-53-3-6222) (SDR) AFT CABIN FLOOR BEAM UPPER INBD SPLICE ANGLE WAS AVALUATED IAW S RM 53-00-15 AND FOUND OUT OF LIMITS, L=0.620" W=0.400" D=0.110", RECEIVED, LOCATESDR CALA2021092401658Beam · corrodedCORROSION ON CABIN FLOOR DUMMY RAIL AT APPRX Y-150 BETWEEN FR20 AND FR23. (A3NB-53-3-6038) REPLACED RAIL BETWEEN FR20 TO FR23 Y-150 IAW A320 SRM 51-72-11- 911-001 AND SRM 51-42-11. P/N: D5311141420200 BTCH: 0003838983. SFR# 1026487. MAINTENANCE ACCOMPLISHED BSDR AALA202109239161Lens · missingAIRCRAFT WAS GROUNDED: FLOOR EMERGENCY EXIT LIGHT MISSING RED COVER AT ROW 11 LEFT SIDE. REPLACED MISSING EMERGENCY EXIT LIGHT LENS COVER PER AMM 33-51-13.SDR CALA2021092201651Frame · corrodedBULK CARGO COMPARTMENT FR 61-62 STR33R HAS LIGHT SURFACE CORROSION (REMOVE CORROSION AND CHECK LIMITS) DAMAGE LOCATED AT STR 33R FR 60 - 62 BLENDED IAW SRM 51-74-00. BLENDED AREA MEASURES L=15" W= 1.5" D=.047", ORIGINAL THICKNESS .063", REMAINING MATERIAL .016SDR CALA2021092201648Stringer · corrodedA3BN-05-3-6013 DURING INSPECTION OF THE FWD CARGO COMPARTMENT, FOUND CORRODED FLOOR RIVETS FROM STRINGER 38 L/H TO STRINGER 38 R/H FROM FRAME 24 TO FRAME 34, FURTHER EVALUATION REQUIRED. REMOVED AND REPLACED CLEATS ON FRAME 32 FROM STRINGER 41-42R PER AIRBUS SDR AALA202109215987Cover · out of positionAIRCRAFT WAS NOT GROUNDED: LEFT OVERWING EXIT NOT SHOWING ARMED ON ELECTRONIC CENTRALIZED AIRCRAFT MONITOR. RESET LEFT OVERWING SLIDE COVER OPERATIONS CHECK GOOD.SDR CALA2021092001618Stringer · corroded(A3NB-52-4-6058) CORROSION ON STRINGER 33R BETWEEN FR 56-57. REMOVED AND REPLACED STINGER AT 33R BETWEEN FR 56 AND 58 IAW SRM 51-42-11. ACCOMPLISHED BY EMP#922369 AT BFM VT AEROSPACE MOBILE NR#0013329SDR CALA2021092001617Oxygen Mask · no testON O2MASK DROP TEST, UNIT AT 20 RIGHT DID NOT DEPLOY. FOUND DISCONNECTED WIRE RUNNING TO UNIT. SECURED WIRE. UNIT TESTED PROPERLY THRICE.SDR CALA2021092001616Support · corrodedPER NR 9296437/30437. CABIN FLOOR STRUCTURE HAS CORROSION ON R2 DOOR SILL IN SEVERAL PLACES. GENERATED BY V892443 REMOVED AND REPLACED AFT CABINR2 DOOR SILL BEAM FR66-68 STR23R I AW A320 SRM 51-72-11-911-001. MECH V061619 INSP BY V892443SDR GTIA2021092035994None · noneL2 DOOR EMER ASSIST BOTTLE REQ SERVICE-SERVICED L2 DOOR EMERG ASSIST BOTTLE IAW AMM 52-10-00SDR CALA2021092001610Door Frame · corrodedPER NR 9292495/26495 R1 DOOR LWR FRAME CORRODED AT AFT GIRT BAR ATTACH POINT.SDR CALA2021092001608Fitting · corrodedCABIN FLOOR STRUCTURE HAS CORROSION ON R2 DOOR SILL FWD CORNER F ITTING. REMOVED AND REPLACED R2 DOOR FWD CARNER FITTING AT FR66 ST23R IA W A320 SRM 51-42-11-001 REMOVED AND REPLACED R2 DOOR FWD CORNER FITTING AT FR66 ST 23R I AW A320 SRM 51-42-11-001SDR CALA2021092001606Shear Plate · corrodedAFT CABIN R/H SIDE FLOOR STRUCTURE LATERAL SHEAR PLATE CRACKED A PPRX 5" AFT FR69. INSTALLED NEW SHEAR PLATE AFT FR69 AND ANGLE IAW SRM 51-75-11 AN D SRM 51-42-11. SFR# 1026424. MAINTENANCE ACCOMPLISHED BY V93387 0 ON WC 0014622 AT ST ENGINEERING BFMSDR AALA202109203745Lens · brokenAIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT BROKEN NEAR LAVATORY DOOR AFT LEFT. REPLACED LIGHT LENS.SDR CALA2021092001604Fitting · corrodedCABIN FLOOR STRUCTURE HAS CORROSION ON R2 DOOR SILL AFT CORNER F ITTING. PER HAECO LCQ NR 9296438/30438 GENERATED BY V892443 REMOVED & REPLACED R2 DOOR AFT CORNER FITTING AT FR68 ST 23R IAW A320 SRM 51-42-11-001 REMOVED AND REPLACED R2 DOOR CORNER FITTING AT FSDR YENA2021092200613Unknown · odorFLT 2135, JFK-PHX. ON DESCENT INTO PHX FA'S REPORTED A STRONG GLUE ODOR THAT SPREAD ACROSS THE CABIN; COMPLIED WITH INFO NOTICE 2017-T015 SEC ""A"" ISOLATED FAULT TO TRANSIENT ENVIRONMENTAL ODOR PER TSM 05-50-00-810-085-B. NO ODOR WITHIN 25 FLT CYCLES. A/C OK SDR GTIA2021092035992Warning Message · false activationAIR PACK 1 OVHT CAME ON IN FLIGHT DURING DESCENT ACCOMPANIED BY FAINT ACRID SMELL ( PACKS A320 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - FAULT CAUTIONS ASSOCIATED WITH OPERATIVE SIDE NOT DISPLAYED )-PERFORMED RESET SDR AALA202109200226Proximity Switch · faultyAIRCRAFT WAS GROUNDED: AT GATE, RIGHT AFT EMERGENCY EXIT SLIDE WILL NOT ARM. REPLACED DOOR SLIDE PROXY SWITCH PER AMM 52-13-00.SDR CALA2021091701600Skin · dentedA3NB-53-3-6349 DURING INSPECTION OF UPPER HALF FUSE FOUND DENT BTW FR69-FR70, STGR 20L-21L. EVALUATE IAW THE APPLICABLE SRM REVISION. ZONE 200 SEQ 1008. EVALUATE DENT BTW FR69-FR70, STGR 20L-21L IAW A320 SRM 53-41-11- 283-059 REV. 137. MEASURED DENT ON FUSE SKSDR CALA2021091701603Hydraulic System · leakingECAM CAUTION MESSAGE - G RSVR LO AIR PR MESSAGE INOP - HYD ON DES INTO ORD 15K CREW DEBRIEF: ON DESCENT THROUGH 15,000, CREW NOTICED ECAM FOR GREEN SYSTEM LOW PRESSURE. THEY LOOKED AT THE HYD PAGE AND QUANTITY WAS NEAR ZERO (ARROW POINTING IN LOWER YELLOW BOXSDR CALA2021091701599Floor Support · corrodedCORROSION ON CABIN FLOOR SUPPORT AT APPRX Y-1673 AT FR20 REMOVED CORROSION ON CABIN FLOOR SUPPORT AT Y-1673 FR20 IAW SRM 51-74-00 FOUND OUT LIMITS IAW SRM 53-11-14-07 ORIGINAL THICKNESS 0.080" REMAINING THICKNESS 0.030" D=0.050". REMOVED AND REPLACE D FLOOR SSDR CALA2021091701598Eiu · failedEIU FAULT DISPLAYED ON UPPER ECAM SCREEN. - ENG 1 OCCURED ON GNDRESET AND ECAM CLRDOCCURED AGAIN INFLT- FADEC 1B FAULT. BITE TEST OF FADEC HAD EIU/HC/EEC1. REPLACED #1 EIU. AND FADEC BITE TEST CK GOOD. RAN ENGINE,NO FAULTS NOTED. REF MM 73-25-00-810-887A. PASDR CALA2021091701596Shear Plate · crackedAFT CABIN R/H SIDE FLOOR STRUCTURE LATERAL SHEAR PLATE CRACKED A PPRX 5" AFT FR69.SDR GTIA2021091635989Bottle · low pressurePER WEEKLY FOUND L1 AND R2 DOOR EMER ASSIST BOTTLE REQ SERVICE -SERVICE L1 AND R2 DOOR EMER ASSIST BOTTLE IAW AMM 52-10-00SDR CALA2021091501580Fuel Cap · missingPDA 2 REF LP 7032358, FUEL CAP REPORTED MISSING BY FUELER. ITEM ENTERED INTO HISTORY E-SFR ENTRY MADE. SDR #1026386 SUBMITTED. MISSING FUEL CAP, AS REPORTED BY FUELER.PLACED ON CDL, CDL CARD 280010, PAGE 28-2 / COMPLIED WITH CDL.R&R FUEL CAP AND RETAINER. OPS SDR YENA2021091700602Oil System · contaminatedFLT 6196, SJU-JFK. LEVEL 1 ODOR "MAGIC MARKER" TYPE SMELL WHEN FLYING THROUGH MOISTURE/ PRECIP WITH VERY MILD EYE IRRITATION ; REF DEFECT NO. 3170012/1, PERFORMED ENG HIGH POWER BLEED AIR TEST REF TSM 71-00-00-710-085-A. NO SMOKE / OIL SMELL DETECTED IN FLIGHTSDR YENA2021091700601Unknown · odorFLT 788, SXM-JFK. INFLIGHT REPORTED SAME "ELECTRICAL SMELL" IN-CABIN DURING DESCENT BELOW 10,000' CORRECTION: INFLIGHT SAID SMELL WAS SIMILAR TO A DIRTY SOCK; AS PER TSM 05-50-00, ACCOMPLISHED LEVEL A DECONTAMINATION IAW AMM 21-00-00. NO SMELL DEFECTS NOTED ATSDR YENA2021091700600Unknown · odorFLT 787, JFK-SXM. ELECTRICAL SMELL IN CABIN DURING DESCENT BELOW FL 100; PERFORM TSM 24-00-00-810-823A AND 05-50-00-810-831-A. NO DEFECTS OR ABNORMAL SMELL DETECTED. ALL CHECKS GOOD.SDR YENA2021091700599Line · leakingFLT 1460, FLL-BDL. GREEN HYD RSVR LOW LEVEL AFTER LANDING EXTENSION FOUND LEAK NEAR MAIN GEAR ON RIGHT SIDE POST RIGHT; R/R R/H GEAR DOOR ACTUATOR FWD BRAIDED HYD LINER IAW AMM 32-31-35 LEAK + OPS CHECKS GOOD. (AN EMERGENCY WAS DECLARED)
Back to Airbus A320-232