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 YENA2022080900784Light · inoperativeDURING HEAVY MAINTENANCE: BROKEN EMERGENCY LIGHT ON CEILING PANEL 251JC (DID NOT ILLUMINATE); REF; AEROMAN WO# 2022+165/1 WCC# 2022-0385701 REMOVED AND REPLACED EMERGENCY LIGHT ON CEILING PANEL 251JC IAW AMM 33-51-11-000-001-A STEP 1 THRU 4. A(1) AND AMM 33SDR YENA2022080900783Light · inoperativeDURING HEAVY MAINTENANCE: EMERGENCY EXIT LIGHT ASSY ON DOOR FRAME DOOR 832 AND 842 (SMALL EXIT 2 EA) AND UPPER SQUARE (2 EA) REFER TO AMP; 534134-01-1 (DID NOT ILLUMINATE); REF; AEROMAN WO# 2022-165/*1 WCC# 2022-385749 REMOVED AND REPLACED EMERGENCY EXIT LIGHSDR YENA2022080900782Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE OF THE UPPER SKIN OF THE CENTER WING BOX BTW Y1292 TO Y1732 AND BTW FR41 TO FR42 IN PASSENGER CABIN; PERFORMED PERMANENT REPAIR ON UPPER SURFACE OF THE UPPER SKIN OF THE CENTER WING BOX BTW. Y1292 TO Y1732 AND SDR YENA2022080900781Skin Panel · corrodedDURING HEAVY MAINTENANCE: CORROSION OF UPPER SURFACE (P2) OF THE UPPER SKIN OF THE CENTER WING BOX BTW Y1292 TO Y1732 AND BTW FR41 TO FR42 IN PASSENGER CABIN; PERFORMED REPAIR ON UPPER SURFACE (P2) OF THE UPPER SKIN OF THE CENTER WING BOX BTW Y1292 TO Y1732 ANSDR YENA2022080900780Spar · crackedDURING HEAVY MAINTENANCE: WINGS/CENTER WING SKIN/ TOP SKIN BETWEEN FR41-42/ CORROSION AND CRACK/ PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)SDR GTIA2022080836576Megaphone · malfunctionedFWD MEGA PHONE SIREN GOES OFF IN FLIGHT-REMOVED AND REPLACED FWD MEGAPHONE IAW A320-EMER EQUIP REV3.SDR YENA2022080800777Acm · dirtyFLT#788, SXM-JFK. 'DESCENDING THROUGH 7000 TO 5000 FEET STRONG MUSTY DIRTY SOCK SMELL DETECTED BY BOTH PILOTS. NO ODOR IN CABIN, ODOR WS COMING FROM COCKPIT VENTS. TURNED OFF PACK 1 AND THE ODOR WENT AWAY. LAST ODOR EVENT ON 7-14-22; PERFORMED LEVEL A DECONTAMSDR YENA2022080800778Apu · dirtyFLT#222, PBI-BOS. ' DIRTY SOCK ODOR FUME IN COCKPIT SEEMS ASSOCIATED WITH PACK 1 NO REPORTS FROM CABIN. PRIOR HISTORY OF FUMES 7/22/22 DESCENT PHASE AND TAXI IN FURTHER TROUBLESHOOT- PACK 1 ALSO HAS ODOR; REMOVED AND REPLACED APU COOLING FAN IAW AMM 49-52-51. SDR AALA202208098760Lamp · inoperativeAIRCRAFT WAS NOT GROUNDED: MULTIPLES EMERGENCY EXIT LOCATION - SIGN INOPERATIVE. RELAMPED MULTIPLES EMERGENCY EXIT LOCATION - SIGN PER AMM 33-51-17 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR CALA2022080501974Floorbeam · corrodedCORROSION FLOORBEAM -Y1292 LOC. BTW 12 TO FR24 IN PASSENGER CAB IN. SEE AEROMAN NON ROUTINE 2022-393811 REPLACED FLOOR BEAM -Y1292 LOC. BTW FR.12 FR.24 IN PASS CABIN OF CORROSION ARE: L=3.615 IN, W=1.212 IN, D=0.086 IN, TOOL USED IAW A320 SRM 51-72-11-911-001 SDR CALA2022080501973Dummy Rail · corrodedCORROSION RAIL DUMMY -Y81 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393815 REPLACED RAIL DUMMY -Y81 AT FWD GALLEY AREA IAW A320 SRM L=2.820 IN, W=2.017IN, D=0.116 IN, TOOL USED: CALIPER P/N: 51-72-11-911-001 AND DRAWING D53110984, PERFORMED DVI ON AREA SDR CALA2022080501972Floorbeam · corrodedCORROSION FLOORBEAM -Y765 LOC. BTW FR12 TO FR24 IN PASSENGER CABIN. SEE AEROMAN NON ROUTINE 2022-393813 REPLACED FLOORBEAM -Y765 LOC BTW FR.12 TO FR.14 IN PASSENGER MEASURE OF CORROSION ARE L=4.125 IN, W=1.217 IN, D=0.083IN, CABIN IAW A320 SRM 51-72-11-911-001SDR CALA2022080501971Fitting · corrodedCORROSION CENTER FITTING PASSENGER CREW DOOR AT AFT GALLEY AREA LH SIDE. SEE AEROMAN NON ROUTINE 2022-360080. REMOVED AND REPLACED CENTER FITTING PASSENGER AREA IAW NTM 51-90-00. PERFORMED SCEPTRE ENTRY ON LOGPAGE SEP-29-2022 CREW DOOR AT AFT GALLEY AREA LH SISDR YENA2022080500746None · failedFLT#1463, LAX-CUN. (AIRCRAFT PERFORMED AN AIR TURN ABCK TO LAX) 'DURING CLIMB THROUGH 15000 FEET NOTICEABLE CABIN PRESSURE FLUCTUATION OCCURRED WITH SIMULTANEOUS ECAM " CAB PRESS SYS 1 FAULT" CAB PRESS V/S FLUCTUATIONS CONTINUED VARYING BETWEEN -1900 TO + 1000SDR CALA2022080501967Floorbeam · corrodedCORROSION FLOORBEAM +Y1292 LOCATED FR66 IN PASSENGER CABIN SEE AEROMAN NON ROUTINE 2022-343175 REMOVED AND REPLACED FLOOR BEAM + Y1292 LOCATED BTW FR 64 TO FR D=2.29MM (0.090IN). TOOL SPLICES AND NOT FOUND MORE DAMAGE IAW NTM 51-90-00. PERFORMED 66 AFT GALLEYSDR CALA2022080501966Fitting · crackedCRACK INDICATION ON FRAME 58 IN OPEN FASTENER HOLE IN HORIZONTAL FLANGE AT LEVEL OF STGR 37LH, CRACK DIRECTION IS 9 OCLOCK, REPAIR BEFORE FURTHER FLIGHT IN AFT CARGO COMPARTMENT (1 EA) REMOVED AND REPLACED SUPPORT FITTING AND FASTENER LOC. ON FR58 BRACKET LAYSDR CALA2022080501965Frame · crackedCRACK INDICATION ON FRAME 43 FOOT COUPLING LH SIDE IN OPEN FASTENER HOLE AT LEVE OF STGR22, CRACK DIRECTION IS 3 OCLOCK IN PASSENGER CABIN (1 EA) REPAIR BEFORE NEXT FLIGHT REMOVED AND REPLACED FRAME 43 FOOT COUNPLING AND FASTENERS LOC FOOT FITTING AT LEVEL STRSDR CALA2022080501964Beam · corrodedCORROSION LOWER SILL LOCATED FR66 TO FR68 R/H SIDE AT AFT GALLEY AREA REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 R/H SIDE CORRODED AREAS ARE:DEEPEST POINT L=3.980 IN W=2.049 IN D=0.055 IS 9151970.SEE AEROMAN NON ROUTINE 2022-343194 AT AFT GALLEY AREASDR GTIA2022080436573None · noneR1 AND L1 DOOR ASSIT BOTTLES LOW-SVC R1 AND L1 DOOR ASSIST BOTTLES PER A 52-10-00SDR YENA2022080500745None · failedFLT#1463, LAX-SJD. (AIRCRAFT PERFORMED AN AIR TURN ABCK TO LAX) 'DURING CLIMB CABIN PR SYS 1 FAULT LEVELED AT 21000 DUETO STRONG PRESSURE FLUCTUATIONS. THE CABIN OUTFLOW VALVE OPENED AND CLOSED RAPIDLY. 2800-3100 CABIN ALT. VS CLMB AND 1000 / -1000 10 MIN AFTESDR CALA2022080501959Doubler · misrepairedA3NB-51-4-6001 TOILET VENT DOUBLER LOCATED FR69-70 STR 30-33R DOES NOT COMPLY WITH CFR 121.1109 PER AMM 51-00-80-200-801C1 FLOW CHART 1 STEP 3 NO REPAIR DATA FOUND.() REMOVED AND REPLACED TOILET VENT DOUBLER IAW SRM 53-41-11-300-00 4 CAT A MAJOR REPAIR. EMP# VSDR GTIA2022080436571None · noneDURING WEEKLY CHECK FOUND L2 DOOR ASSIST REQ SERVICE-SERVICED L2 DOOR ASSIST IAW AMM 52-10-00SDR CALA2022080301948Floor Support · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED FR66 LEVEL STRG 23L IN PASSENGER CABIN, SEE AEROMAN NON ROUTINE 2022-343169 REMOVED AND REPLACED FLOOR STRUCTURE ANGLE LOCATED FR.66 LEVEL 24-JUN-23, PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND STR. 23L IN PASSENGER CASDR CALA2022080301947Floorbeam · corrodedCORROSION FLOORBEAM +Y1292 LOCATED FR66 IN PASSENGER CABIN SEE AEROMAN NON ROUTINE 2022-343175 REMOVED AND REPLACED FLOORBEAM + Y1292 LOCATED BTW FR 64 TO FR D=2.29MM (0.090IN). TOOL SPLICES AND NOT FOUND MORE DAMAGE IAW NTM 51-90-00. PERFORMED 66 AFT GALLEY SDR CALA2022080301946Floor Support · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED FR66 LEVEL STRG23R IN PASSE ABIN. SEE AEROMAN NON ROUTINE 2022-343195 REMOVED AND REPLACED FLOOR STRUCTURE ANGLE LOCATED FR 66 LEVEL 24-JUN-23. PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND STR 23R IN PASSEGER CABIN IASDR CALA2022080301945Floor Support · corrodedCORROSION FLOOR STRUCTURE -Y1162.5 AND FR68 IN PASSENGER CABIN REMOVED AND REPLACED FLOOR STRUCTURE -Y1162.5 LOC. FR.68 TO DIGITRAL CALIPER P/N: 500-197-30; S/N: A21147760; CAL DUE DATE: PERFORMED SCEPTRE ENTRY ON LOG PAGE NUMBER 9206195 FR.69 AND -Y1162.5 IASDR YENA2022080500751None · noneFLT#1405, MCO-SDQ. (AIRCRAFT DECLARED AN EMERGENCY) 'BRAKES ALTN LET RELEASED; RESET BSCU IAW AMM 32-42-00. CLEARED ECAM MSG ALL IS OPERATING NORMALLY. A/C OK FOR SERVICE MCC SAI NOTIFIED.'SDR YENA2022080500748None · noneFLT#1568, PUJ-JFK. 'ON TAXI OUT, INFLIGHT CALLED UP REPORTING A PUNGENT ODOR. AGREED TO TAKE OFF TO SEE IF IT WOULD DISSIPATE. NO SMELL COMING FROM A/C OUTLETS. CALLED UP AGAIN ON CLIMB & CRUISE. ODOR WAS ONLY NOTICED IN GALLEY AND THE FIRST 4 ROWS. RAN SDR GTIA2022080436563None · fault messageFUME EVENT UPON APPROACH INTO TJSJ ISOL PACK 2 ( 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 INSP OF CABIN ODOR IAW TSM 05-50-00, NO FSDR CALA2022080301955Stringer · corrodedA3NB-53-4-6175 AFT CARGO COMP STR 43L BET FR63-64 HAS CORROSION. () REMOVED, FABRICATED AND PLACED STRINGERS IAW SRM 51-42-11, DWG D 53470418, D5347034. EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEE RING AEROSPACE OF MOBILE AT BFM ON NR# 34951.SDR CALA2022080301953Stringer · corrodedA3NB-53-4-6175 AFT CARGO COMP STR 42L BET FR63-FR64 HAS CORROSIO N() AFT CARGO STR 42L BET FR60-FR64 WAS REMOVED AND MANFACTURED NEW STR IAW AIRBUS DRAWING 17D53470418 AND INSTALLED IAW SRM 51-42-1 1, D53473045. EMP# V936191 WORK ACCOMPLISHED AT ST ENGINEERINGSDR CALA2022080301952Doubler · discoveredA3NB-51-4-6001 DOUBLER LOCATED FR69-70 STR 18L-19L DOES NOT COMP LY WITH 14 CFR 121.1109 PER AMM 51-00-80-200-801C1 FLOW CHART 1 STEP 3 NO REPAIR DATA FOUND.() REMOVED AND REPLACED DOUBLER OF FR69-70 STGR 18-19L IAW SRM 53-4 1-11-300-036 CAT A MAJOR REPAIR. EMSDR YENA2022080500749None · noneFLT#1470, CHS-LGA. 'DIRTY SOCK SMELL BELOW 10000 FT. ISOLATED BY TURNING PACK #1 OFF AS SMELL WAS MOSTLY CONTAINED IN COCKPIT & FWD CABIN SMELL IMPROVED BUT STILL PRESENT; C/W INFO NOTICE 2017-T15 SECTION (A) ISOLATED FAULT TO TYPE 10, 1C TSM 05-50-00-810-831-SDR YENA2022080300743Drive Unit · failedFLT#2603, EWR- TPA. (AIRCRAFT PERFORMED AN AIR TURN BACK TO EWR) WEATHER RADAR FAILURE ON CLIMB OUT; REMOVED AND REPLACED WX RADAR TRANSCEIVER IAW AMM 34-41-33. DUE TO BITE TEST FAILURE. REF LOG PAGE 3476359, ITEM 1 (REMOVED AND REPLACED WX RADAR ANTENNA & DRISDR YENA2022080300742Transceiver · failedFLT#2603, EWR- TPA. (AIRCRAFT PERFORMED AN AIR TURN BACK TO EWR) WEATHER RADAR FAILURE ON CLIMB OUT; REMOVED AND REPLACED WX RADAR TRANSCEIVER IAW AMM 34-41-33. DUE TO BITE TEST FAILURE. REF LOG PAGE 3476359, ITEM 1 (REMOVED AND REPLACED WX RADAR ANTENNA & DRISDR GTIA2022080136562None · noneDURING CRUSE FL 340 STRONG BURNING ODOR AIRCRAFT RIGHT ROW 29 OVERHEAD BIN INSTRUCTION NKMX TO TURN OFF ONE PACK TO TROUBLESHOOT SMELL WENT AWAY WHEN PACK ONE SELECTED OFF ( PACKS A320 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHASDR CALA2022080101931Floorbeam · corrodedCORROSION FLOORBEAM Y-189 LOC.BTW FR20 TO FR24 AT FWD GALLEY AREA.REPLACED FOORBEAM -Y189 LOC BTW FR20 TO FR24 AT FWD GALLEY AREA OF CORROSION ARE L=2.360 IN W=0.878 IN D=0.010.SDR CALA2022080101934Coupling · crackedCRACK INDICATION ON FRAME 43 FOOT COUPLING LH SIDE IN OPEN FASTENER HOLE AT LEVE OF STGR22, CRACK DIRECTION IS 3 OCLOCK IN PASSENGER CABIN. REMOVED AND REPLACED FRAME 43 FOOT COUNPLING AND FASTENERS LOC FOOT FITTING AT LEVEL STR21 LH.SDR CALA2022080101933Frame · crackedCRACK INDICATION ON FRAME 58 IN OPEN FASTENER HOLE IN HORIZONTAL FLANGE AT LEVEL OF STGR 37LH, CRACK DIRECTION IS 9 OCLOCK, REMOVED AND REPLACED SUPPORT FITTING AND FASTENER LOC. ON FR58 BRACKET LAYER.SDR CALA2022080101932Floor Support · corrodedCORROSION FLOOR STRUCTURE Y1162.5 AND FR68 IN PASSENGER CABIN REMOVED AND REPLACED FLOOR STRUCTURE Y1162.5 AND FASTENER LOC D=1.150 MM (0.045 INCH).SDR YENA2022080200740Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION REAR SPAR TRAILING EDGE TOP SKIN, LOWER SURFACE, OVERHANG BT W RIB8 TO RIB9 ON RH WING (REFER TO THE MPD TASK: 572178-01.); PERFORMED REPAIR ON RH WING TOP SKIN BOTTOM SURFACE TRAILING EDGE BTW RIB 8 TO RIB 9 I.A.W EA NO. 57SDR YENA2022080200739Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION REAR SPAR LOC. TOP SKIN, LOWER SURFACE, OVERHANG BTW RIB8 TO RIB9 ON LH WING; PERFORMED REPAIR ON TOP SKIN LOWER SURFACE OVERHANG LOC RIB 8 PLUS 4 INCH ON LH WING I.A.W. EC NO. A22-604-01 AND EA NO. 57-0204-22, PART 1, PART SDR YENA2022080200738Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION LOCATED ON RIB 11 PLUS 3 INCH TOP SKIN LOWER SURFACE OVERHANG TRAILING EDGE LH WING. REFER TO THE MPD TASK 572178-01; REWORKED AFFECTED AREA LOC. ON RIB 11 PLUS 3IN AT TOP SKIN LOWER SURFACE OVERHANG TRAILING EDGE AT LH WINSDR YENA2022080200737Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION REAR SPAR TRAILING EDGE TOP SKIN, LOWER SURFACE, OVERHANG. BT W RIB7 TO RIB8 ON RH WING (REFER TO THE MPD TASK: 572178-01); PERFORMED REPAIR ON RH WING TOP SKIN BOTTOM SURFACE TRAILING EDGE BTW RIB 7 TO RIB 8 IN ACCORDANCE WSDR YENA2022080200736Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION REAR SPAR LOC. ON TOP SKIN, LOWER SURFACE, OVERHANG BTW RIB7 TO RIB8 ON LH WING; PERFORMED REPAIR ON TOP SKIN LOWER SURFACE OVERHANG LOC RIB 7 ON LH WING I.A.W. EC NO. A22-604-01 AND EA NO. 57-0204-22, PART 1, PART 5, AND PASDR YENA2022080200735Skin Panel · corrodedDURING HEAVY MAINTENANCE: CORROSION REAR SPAR LOC. TOP SKIN, LOWER SURFACE, OVERHANG BTW RIB10 T O RIB11 ON LH WING. REFER TO THE MPD TASK 572178-01; PERFORMED REPAIR ON TOP SKIN LOWER SURFACE OVERHANG BTW RIB 10 TO RIB 11 ON LH WING I.A.W. EC NO. A22-605-01 ASDR YENA2022080200734Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION REAR SPAR LOC. TOP SKIN, LOWER SURFACE, OVERHANG BTW RIB14 T O RIB15 ON LH WING REFER TO THE MPD TASK 572179-01; PERFORMED INTERIM REPAIR ON TOP SKIN LOWER SURFACE OVERHANG LOC RIB 14 ON LH WING I.A.W. EC NO. A22-606-01, ANDSDR YENA2022080200733Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION REAR SPAR LOC. TOP SKIN, LOWER SURFACE, OVERHANG BTW RIB13 TO RIB14 ON LH WING REFER TO THE MPD TASK 572179-01; B17030932, DUE DATE NOV-29-2022 ULTRASONIC PHASED ARRAY P/N: OMNI-MX; S/N: OMNI-102103; DUE DATE: JUL-30-2022. CSDR YENA2022080200732Skin Panel · corrodedDURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL #2 / TE OVERHANG LOWER SURFACE BETWEEN RIB 9 AND 11 - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2022080200731Skin Panel · corrodedDURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL #2 / TE OVERHANG LOWER SURFACE BETWEEN RIB 13 AND 15 - TIME-LIMITED REPAIR. (CONSIDERED AS A MAJOR REPAIR)
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