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 GTIA2023090537458Skin · damagedTOOL MAK ON LH WING LOWER SURFACE FUEL TANK HOLE CUTOUT BTW RIB 17 AND RIB 18 DIMENSION: L=N/A W= N/A D= 0.273 RAF-01-3073925-02 GENERATED-PERFORMED PERMANENT REPAIR ON CUTOUT ON LH WING OF FUEL TANK PANEL IAW A320 SRM 57-21-11-300-002. THIS REPAIR IS CATEGORYSDR GTIA2023090537457Skin · damagedTOOL MARK LOWER SURFACE CUTOUT FUEL TANK BTW RIB 16 AND RIB 17 ON RH WING. RAF-01 3073927-01 GENERATED-PERFORMED PERMANENT REPAIR ON CUTOUT OF RIB 16 AND RIB 17 OF RH WING FUEL TANK PANEL IAW A320 SRM 57-21-11-300-002. THIS REPAIR IS CATEGORY B. REQUIRED INSPESDR GTIA2023090537456Skin · damagedCRACK LEADING EDGE OUTBOARD FLAP LOWER SKIN ON RH WING. RAF-01 GENERATED. SDR GENERATED.-PERFORMED PERMANENT REPAIR ON EDGE OUTBOARD FLAP RH WING IAW A320 SRM 57-53-00-300-029SDR GTIA2023090537455Skin · damagedTOOL MARK LOWER SURFACE HOLE CUTOUT FUEL TANK BTW RIB 13 AND RIB 14 ON RH WING. RAF-01 3073926-02 GENERATED-PERFROMED PERMANENT REPAIR ON CUTOUT OF RIB 13 AND RIB 14 ON RH WING OF FUEL PANEL IAW A320 SRM 57-21-11-300-002. THIS REPAIR IS CATEGORY B. REQUIRED INSDR GTIA2023090537454Skin · damagedTOOL MARK LOWER SURFACE HOLE CUTOUT FUEL TANK BTW RIB 18 AND RIB 19 ON RH WING. RAF-01 3073927-02 GENERATED-PERFORMED PERMANENT REPAIR ON CUTOUT OF RIB 18 AND RIB 19 ON RH WING OF FUEL TANK PANEL IAW A320 SRM 57-21-11-300-002. THIS REPAIR IS CATEGORY B. REQUIRSDR GTIA2023090537453Skin · damagedTOOL MARK LOWER SURFACE HOLE FULE TANK BTW RIB 13 AND RIB 14 ON LH WING RAF-01 3073924-02 GENERATED-PERFORMED PERMANENT REPAIR ON CUTOUT OF FUEL TANK PANEL IAW A320 SRM 57-21-11-300-002. THIS REPAIR IS CATEGORY B. REQUIRED INSPECTION THRESHOLD FROM AIRCRAFT FISDR GTIA2023090537452Skin · damagedTOOL MARK ON LH DALING LODNER SRFACE FUEL TANK HOLE CUTOUT BTW RIB 14 AND RIB 15 DIMENSIONS: L=N/A DN=N/A D=0.67" RAF-01 3073929-02 GENERATED -PERFORMED PERMANENT REPAIR ON CUTOUT OF RIB 14 AND RIB 16 IS ON LH WING OF FUEL TANK PANEL IAW A320 SRM 57-21-11-300-SDR YENA2023090501033Filter · failedFLT#626, FLL-RDU. 'ODOR/ FUME EVENT: LEVEL 2 AFT FLIGHT ATTENDANTS REPORTED SMELLING DIRTY SOCKS " SMELL SHORTLY AFTER THE 10000 CHIME ON DESCENT INTO RDU. CLEAR SKIES, NO CLOUDS, FIRST OFFICER REPORTED ODOR SMELL AROUND 3000FT ODOR DISSIPATED ON LANDING. ( PASDR YENA2023090501032Unknown · unknownFLT#1510, PUJ-FLL. 'APU OFF- STRONG ACRID / BURNING OIL/DIRTY SOCK TOXIC FUMES THROUGHOUT AIRCRAFT WITH STRONGEST SMELL IN COCPIT. DESCENT PHASE BELOW 10,000' FROM PACKS, AND PRESENT UNTIL LANDING. USING COCKPIT/CABIN ODOR RECOGNITION AND ISOLATION CHECKLIST- SDR AALA202309019022Bottle · deactivatedAIRCRAFT WAS NOT GROUNDED DURING TROUBLE SHOOTING OF THE L1 DOOR INDICATION FAULT FOUND DOOR ASSIST BOTTLE SAFETY WIRED IN DISARMED POSITION. MAINTENANCE RE-ARMED L1 DOOR ASSIST BOTTLE PER AMM 52-10-00.SDR CALA2023083002661Brake Sys · faultedBRAKES SYS 2 FAULTCYCLED A/SKID SWITCHGOT BRAKES SYS 1 FAULTCOUL D NOT CLEAR REMOVED AND REPLACED BSCU PER AMM 32-42-34-000/400-001-A. OPS 1711515,QTY :1 CHECK GOOD. RANG WIRES FROM BSCU PINS 1A/1B 102.0 OHMS, AND PINS ROTABLE PARTS CHANGE WAS INDICATED - TT #SDR YENA2023090101029Unknown · unknownFLT#2625, RDU-FLL. 'FORWARD CABIN HAS AN "OILY" SMELL, NOT NOTED IN MID OR AFT CABIN; ACCOMPLISHED INFO NOTICE 2017T-T015J PART B2 & TSM 05-50-810-831-A DETERMINED IS LEVEL 2 FOUND ROOT CAUSE APU DUE TO LOW OIL LEVEL & EVIDENCE OF OIL IN COMPRESSOR SECTION & DSDR YENA2023090101009Unknown · unknownFLT#1079, LAS-LAX. ' CABIN CREW REPORTED TO NEW FLIGHT CREW ABOUT FUME EVENT DURING INBOUND FLIGHT FUME WERE EXPERIENCED BY CREW & PAX & CLEANERS DURING CLIMB, DESCENT AND LANDING THROUGHOUT CABIN; PERFORMED INFO NOTICE 2017-T015J. FOUND APU BAY CONTAMINATED WSDR GTIA2023083137450Unknown · unknownAFTER ARRIVING TO GATE, AFT FA.S REPORTED MUSTY ODOR FROM TOP OF DESCENT TO LANDING. FUME EVENT-PERFORMED TSM 05-50-00-810-831, CABIN ODOR . INSPECTED APU AREA , BOTH ENGINES NO DEFECT NOTED. RUN PACK1 AND PACK2 IAW AMM 21-61-00, COULDN'T DUPLICATE OROR SYTEMSDR YENA2023083001007Unknown · unknownFLT #943, RNO-LAX." "DIRTY SOCK" ODOR WAS NOTICED ON DESCENT INTO LAX AT 2500FT IN COCKPIT, WAS EXTREMELY STRONG, IN CABIN NOTICED BY FA'S AND CUSTOMERS; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION B2. DECONTAMINATION LEVEL C WAS ACCOMPLISHED PER TSM SDR GTIA2023083137449Unknown · unknownFUME EVENT ON DESCENT THROUGH 10,000FT. FA'S SAID THEY DID NOT SMELL ANYTHING-INSPECTED PER TSM 05-50-00-810-831-A, NO ODOR DETECTED. A/C GOOD FOR RETURN TO SERVICESDR GTIA2023083137448Megaphone · inoperativeR2 DOOR MEGAPHONE INOP-REPLACE MEGAPHONE PER SPIRIT AIRLINE DRAWING A320-EMER EQUIP.SDR YENA2023083001006Unknown · unknownFLT#348, SLC-BOS. 'CHEMICAL SMELL LIKE DEICING FLUID ON DESCENT PASSING THROUGH 13,000 UNTIL LANDING; COMPLIED WITH INFO NOTICE 2107-T015 SECTION A ISOLATED TO TYPE 10, (A) 1, C, PER TSM 05-50-00-810-085-B AIRCRAFT IS OK FOR SERVICE.'SDR CALA2023083002666Bolt · missing#2 MLG WHEEL HAS 1 MISSING TIE BOLT. WHEEL, TIRE, AS OFF 31-3245-9-9001 0456 ON 0000 WHEEL, TIRE, AS OFF 31-3245-9-9001 0456 ON 31-3245-9-9001 1217 RAR #2 MLG WHEEL AND TIRE ASSY IAW AMM 32-41-11. PARTS USED: 31-3245-9-9001,QTY :1 ROTABLE PARTS CHANGE WAS INDISDR GTIA2023083137447Unknown · unknownINBOUND FLIGHT ATTENDANTS AND INSTRUCTOR REPORTED SMELLING A BURNING OR CHEMICAL SMELL MAKING SOME FA'S FEEL ILL ( PACKS - A320 WITH MOD. 30626/MP K6443 (ENHANCED ECS) OR A321 WITH MOD. 157080/MP K17996 (PACK FLOW SELECTOR) AND WITH MOD. 30626/MP K6443 (ENHANCSDR YENA2023083001004Terminal · failedFLT#268, PUJ-JFK. 'ELECTRICAL BURNING SMELL EMENATING FROM OVERHEAD FWD GALLEY LIGHT FIXTURE (S) TURNED LIGHTS OFF SMELL DISAPATED ( THALES-AVANT IFE (ENTIRE SYSTEM) ); REMOVED AND REPLACED ICMT IAW AMM 44-21-11 AND PSB IAW AMM 44-22-44 DUE TO BURNING SMELL FRSDR AALA202308296116Screw · looseAIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR IS DIFFICULT TO OPEN AND SHUT IN FLIGHT. MAINTENANCE FOUND METALLIC PLATE ON FLOOR ATTACHMENT SCREW LOOSE AND RESECURED IT PER AMM 20-21-11. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.SDR GTIA2023082837444Battery · no testEPSU BATT 11WL FAILS CAPACITANCE CHECK SDR SUBMITTED -REMOVED AND REPLACED EPSU BATTERY PACK 11WL IAW A320AMM 33-51-38-000-002A/33-51-38-400-002A. SYSTEM OPS CHECK GOOD IAW AMM 33-51-00-710-001A AND 23-73-00-740-005BSDR GTIA2023082837443Skin · damagedREF 3318852-1 DURING AIRCRAFT JACKING DENT CREATED AT AFT JACK SAFETY AREA FR 71-76. DAMAGE MEASUREMENTS FR73 BETWEEN STR 25L-25R 16", FR74 BETWEEN STR 25L-25R 25.5", STR 32L 65", STR 32R 46.5". RAF CREATED-PERFORMED REPAIR IN AFT JACK SAFETY AREA FR 71-76 IAWSDR YENA2023082800995Unknown · unknownFLT#577, FLL-SFO. 'FLT ATTENTS REPORTED DIRTY SOCK ODOR RIGHT AFTER T/O LEVEL 1 ODOR THAT LASTED 3 MINUTE; PER TSM TASK 05-50-00-810-831-A & AMM 71-00-00 RAN #1 ENGINE FOR 5 MINUTES DURATION AND ALTERNATED PACK 1 & 2 FOR DETERMINATION OF ODOR IAW INFORMATION NSDR YENA2023082800994Unknown · unknownFLT#914, FLL-HPN. 'FUMES ON TAKEOFF IN COCKPIT. APPLIED ODOR ISOLATION PROCEDURE, TURNING #1 PACK OFF AND FUMES DISSIPATED; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10, (A), 1, C PER TSM 05-50-00-810-805-B, TSM 05-50-00-810SDR CALA2023090802738Slide · unwanted deployDEPLOYED OVERWING SLIDE ON AIRCRAFT LEFT. PICS OF DEPLOYED SLIDE. REMOVED LH OFFWING SLIDE INFLATION RESERVOIR REF AMM 25-62-46-000-001-A. INFLATION RESERVOIR REMOVED PLACED IN AFT CGO PIT LT O/W WING SLIDE REMOVED REF AMM 25-62-42-000-002-A. BOTTLE, ASSY, O OSDR CALA2023082802649Profile · crackedEMERGENCY EXITS INTERNAL STRUCTURE, R/H FWD HATCH Z843, AFT LOAD TRANSMITTING PROFILE, CRACKS EXTENDING FROM FASTENER HOLES, MULT IPLE LOCATIONS. (A3NB-52-4-6031) GENERATED AT HAECO LCQ PER NR 9 296234 (20234) REMOVED AND REPLACED R/H FWD EE HATCH, AFT LAND TSDR CALA2023082802648Profile · crackedEMERGENCY EXITS INTERNAL STRUCTURE, R/H AFT HATCH Z844, FWD LOAD TRANSMITTING PROFILE, CRACKS EXTENDING FROM FASTENER HOLES, MULT IPLE LOCATIONS. (A3NB-52-4-6031) GENERATED AT HAECO LCQ PER NR 9 296235 (20235) REMOVED AND REPLACED R/H AFT EE HATCH, FWD LOAD TSDR CALA2023082802647Profile · crackedEMERGENCY EXITS INTERNAL STRUCTURE, L/H AFT HATCH Z834, FWD LOAD TRANSMITTING PROFILE, CRACKS EXTENDING FROM FASTENER HOLES, MUL TIPLE LOCATIONS. (A3NB-52-4-6031) GENERATED AT HAECO LCQ PER NR 9296233 (20233) REMOVED AND REPLACED L/H AFT EE HATCH, FWD TRANSMISDR CALA2023082802646Profile · crackedEMERGENCY EXITS INTERNAL STRUCTURE, R/H AFT HATCH Z844, AFT LOAD TRANSMITTING PROFILE, CRACKS EXTENDING FROM FASTENER HOLES, MUL TIPLE LOCATIONS. (A3NB-52-4-6031) GENERATED AT HAECO LCQ PER NR 9296236(20236) REMOVED AND REPLACED R/H AFT EE HATCH, AFT LOAD TRASDR CALA2023082802645Profile · crackedEMERGENCY EXITS INTERNAL STRUCTURE, L/H AFT HATCH Z834, AFT LOAD TRANSMITTING PROFILE, CRACKS EXTENDING FROM FASTENER HOLES, MUL TIPLE LOCATIONS. (A3NB-52-4-6031) GENERATED AT HAECO LCQ 9296237 (20237) BY MECH V920443 REMOVED AND REPLACED L/H AFT EE HATCH, AFTSDR CALA2023082802644Profile · crackedEMERGENCY EXITS INTERNAL STRUCTURE, L/H FWD HATCH Z833, AFT LOAD TRANSMITTING PROFILE, CRACKS EXTENDING FROM FASTENER HOLES, MULT IPLE LOCATIONS. (A3NB-52-4-6031) GENERATED AT HAECO LCQ PER NR 9 296238 (20238) BY MECH V920443 REMOVED AND REPLACED L/H FWD EE HASDR CALA2023082802639Door Frame · crackedEMERGENCY EXITS INTERNAL STRUCTURE, L/H FWD HATCH Z833, FWD LOAD TRASMITTING PROFILE, CRACKS EXTENDING FROM FASTENER HOLES,MULT IPLE LOCATIONS. (A3NB-52-4-6031) GENERATED AT HAECO LCQ PER NR 9 296232 (20232) BY MECH V920443 REMOVED AND REPLACED L/H FWD HATCH, SDR GTIA2023082837441Transmitter · faulted"LOW OIL PRESSURE INDICATION IN FLIGHT #1 ENG 1 LOW OIL PRESSURE ECAM FLIGKER ON AND OFF OIL PRESSURE INDICATED FROM AMBER XX TO 200 PSI -R/R #1 XMTR OIL PRESSURE SENSOR 4003EN, PERFORMED OPS LEAK TEST IAW 79-33-15 NO DEFECTS NOTED, OPS TEST GOOD"SDR YENA2023082800997Selector · failedFLT#2005, BOS-MCO. 'L/G DOORS NOT CLOSED UPON CYCLING L/G DOWN; REMOVED AND REPLACED LANDING GEAR DOORS SELECTOR VALVE (41GA)IAW AMM CH 32-31-34. PERFORMED FUNCTIONAL TEST OF THE NORMAL EXTENSION & RETRACTION OF THE L/G. TEST OK. REF AMM 32-31-00.'SDR YENA2023082800996Unknown · unknownFLT#2356, MBJ-EWR. 'OIL FUMES DIRTY SOOCK SMELL STARTED AT 3K ON ARRIVAL WITH POWER SETTING CHANGES MULTIPLE TIMES DISSIPATED BY LANDING; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION A ISOLATED FAULT TO TYPE 10 (A) 1 C PER TSM 05-50-00810-085-B TSM 05-50SDR AALA202308291566Proximity Sensor · defectiveAIRCRAFT WAS GROUNDED: UPON SELECTING GEAR UP AFTER TAKEOFF, LANDING GEAR DOORS DID NOT RETRACT, FLIGHT CREW RECYCLED GEAR PER ECAM PROCEDURE GEAR AND DOORS RETRACTED NORMALLY. **SUPPLEMENTAL REPORT FOR AALA202308281566: REPLACED MAIN LANDING GEAR PROXIMITY SSDR AALA202308281566Unknown · unknownAIRCRAFT WAS GROUNDED: UPON SELECTING GEAR UP AFTER TAKEOFF, LANDING GEAR DOORS DID NOT RETRACT, FLIGHT CREW RECYCLED GEAR PER ECAM PROCEDURE GEAR AND DOORS RETRACTED NORMALLY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED **(OPEN)SDR YENA2023082400988Unknown · unknownFLT#8356, MBJ-EWR. 'ODOR RETURNED IN DESCENT MORE NOTICEABLE IN THE CLOUDS STARTED AT ABOUT FL 270,' (SUPPLEMENTAL INFORMATION TO FOLLOW)SDR GTIA2023082437437Spar · damagedDURING HMV FOUND A GOUGE @ PYLON #1 LOWER SPAR. MDL 337.13MM MDW 8.5MM MDD 0.49 OST 3.75MM RAF 3329127-01. OPEN SDR ITEM.-VERIFIED NR # 5001257255-0010 AND TC # 1004054607-0010. REPAIR HAS BEEN ACCOMPLISHED AS PER SPIRIT EA 5451-2333 REV 00 REINSPECTION REQUIRSDR GTIA2023082437436Spar · damagedDURING HMV FOUND A GOUGE @ PYLON #2 LOWER SPAR. MDL 340.45MM MDW 6.37MM MDD 0.31MM OST 3.75. RAF # 3329126-02 OPEN. SDR ITEM.-VERIFIED NR # 5001257257-0010 AND TC # 1004054608-0010. REPAIR HAS BEEN ACCOMPLISHED AS PER SPIRIT EA 5451-2334 REV. 00 REINSPECTION RSDR GTIA2023082437435Structure · corrodedDURING HMV FOUND CORROSION ON FWD GALLEY. MDL 100MM MDW 135MM MDD 2MM OST 2MM RAF 3329126-01 CREATED.-VERIFIED NR # 5001256442-0010 AND 1004054579-0010. REPAIR HAS BEEN ACCOMPLISHED AS PER SPIRIT EA 2531-2339 REV 00.SDR AALA202308246053Fitting · stickingAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS DOOR 1R DIFFICULT TO ARM AND DISARM. MAINTENANCE CLEAN DEBRIS FROM GIRT BAR FITTINGS AND LUBRICATED THE FITITNGS. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.SDR YENA2023082400986Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON AFT FRAME SEGMENT (2) OF THE EMERG EXIT HATCHES 843 (1) CRACK LENGTH 0.360 INCH (2) SEGMENT CRACK LENGTH 0.375 INCH; REF: AEROMAN W/O 2023-272/1 N/R 2023-424625 REMOVED AND REPLACED FWD FRMAE SEGMENT (1) OF TSDR YENA2023082400985Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD FRAME SEGMENT (2) OF THE EMERG EXIT HATCHES 844, CRACK LENGTH (1) L= 0.281 INCH (2) CRACK LENGTH L= 0.400 INCH; REF: AEROMAN W/O 2023-272/1 N/R 2023-424627 AND 2023-424628. REMOVED AND REPLACED FWD AND ASDR YENA2023082400984Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD FRAME SEGMENT (2) OF THE EMERG EXIT HATCHES 844, CRACK LENGTH (1) L= 0.281 INCH (2) CRACK LENGTH L= 0.400 INCH; REF: AEROMAN W/O 2023-272/1 N/R 2023-424627 AND 2023-424628. REMOVED AND REPLACED FWD AND ASDR YENA2023082400983Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD FRAME SEGMENT (2 EA) OF THE EMERG EXIT HATCHES 834 CRACK (1) L= 0.425 INCH AND (2) L= 0.410 INCH; REF: ARM W/O 2023-272/1 N/R 2023-424625 AND N/R 2023-424626. REMOVED AND REPLACED FWD AND AFT FRAMES IAW SDR YENA2023082400982Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 AT AFT GALLEY AREA (CRACK INDICATION FROM HOLE 3 OF FRAME 68 LH DOOR STOP FITTING 1 AT AFT GALLEY AREA. CRACK D EPTH IS 0.076 INCH AND CRACK DIRECTION IS 9 O CLOCK (LOOKING AFT)); AEROMAN WO# 2023-272/1 20SDR YENA2023082400981Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD FRAME SEGMENT (2) OF THE EMERG EXIT HATCHES 833 CRACK (1) L=0.350" (2) CRACK L= 0.400 INCH; REF: ARM W/O 2023-272/1 N/R 2023-424631 AND 2023-424632. REMOVED AND REPLACED FWD AND AFT FRAMES ON TASK CARD A
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