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 CALA2024080102147Stringer · corrodedNO DOT AFT CARGO COMP L/H STRING 33 BTW FR59-61 HAS SIGNS OF COR ROSION (CLEAN EVALUATE,REPAIR, IF NECCESARY)SDR GTIA2024071938239Ecs · contaminatedDIRTY SOCKS SMELL ON CLIMBOUT PACK1-PERFORMMED LEVEL A DECONTAMINATION OF THE ECS IAW AMM 21-00-00. A/C OK FOR SERVICE.SDR YENA2024071901006Unknown · odorFLT#1696, SJO-MCO. 'DIRTY SOCK SMELL REPORTED BY INFLIGHT UPON ARRIVAL AT GATE. SMELL WAS ON FINAL DECENT MID AFT CABIN; COMPLIED WITH INFO NOTICE 2017-T015 SECTION B2. IDENTIFIED ODOR TRANSIENT ENVIRONMENTAL ODOR. PERFORMED "ECS" DECONTAMINATION PER TSM 05-5SDR YENA2024071601003Smoke Detector · false activationFLT#353, BOS-DUB. (ETOPS) 'CLASS II MAINTENANCE MESSAGE "SMOKE" ON LOWER ECAM; RESET & PREFORMED A BITE TEST OF SMOKE DETECTION SYSTEM PER AMM 26-14-00. OPS CHECK NORMAL. MX-4 UPDATED, MCC NOTIFIED, PLACARD REMOVED.SDR CALA2024071902065Skin · abnormalR/H ELEVATOR TOP SIDE HAS LIQUID INGRESS AT 91 INCHES FROM I/B 5 1/2 INCHES FROM TRAILING EDGE 2 INCHES IN DIAMETER. DRILLED WITNESS HOLES ON RH ELEVATOR UPPER SURFACE 91 IN FROM VB 5.5 IN FROM T/E 1.5 IN DIA ZONE C IAW A320 AMM 55-20-00-200-006 A PAR 4 A(6) SDR AALA202407169595Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: 1L DOOR EMERGENCY ACCUMULATOR BOTTLE PRESSURE OUT OF LIMITS. PRESSURE 1000 PSI. TEMP 90F. CHARGED EMERGENCY ACCUMULATOR BOTTLE PER AMM 52-10-00.SDR YENA2024071601002O-Ring · leakingFLT#2357, EWR-MBJ. (AIRCRAFT PERFORMED AN AIR TURN BACK TO EWR). 'HYD B RSVR LO LVL ECAM IN FLIGHT LOST ALL FLUID IN BLUE SYSTEM; UPON INSPECTION OF THE T FITTING ASSY WHERE THE ELEC PUMP PRESS. SWITCH(2074GJ) IS INSTALLED, FOUND THE O-RING OFF THE PRESSURE SWSDR CALA2024071602045Skin · damagedACCOMPLISH INSPECTION REQUIREMENTS ON THE LH FWD FUSELAGE FR4-6 SKIN PANEL REPAIR PER PART 2 OF THE LATEST REVISION OF ECRA 5311-03240. 5311-03240 ON OR BEFORE 96,489 TOTAL AIRCRAFT FLIGHT CYCLES OR 211,952 TOTAL AIRCRAFT FLIGHT HOURS, WHICHEVER OCCURS FIRST. SDR GTIA2024071538234Flashlight · inoperativeCA FLASH LIGHT INOPERATIVE ( FLASHLIGHT AND HOLDERS (FLIGHT DECK OR CABIN) )-R/R CA FLASHLIGHT IAW CMM 25-60-21. OPS CHECK GOOD. THIS CLEARS DMI #3417075-1. PLACARD REMOVED MOC NOTIFIED.SDR CALA2024072602115Skin · corrodedLOWER FWD FUS, INSIDE AND SKIN AROUND OF HARDWARE HOLES WITH CORROSION EVIDENCE ON TCAS ANTENNA PERFORMED REPLACED OF DAMAGES PART AND REPAIRED I.A.W. EC/RA 532 1-02146 FORM 44-0008 ATTACHED WORK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 106734SDR YENA2024071601025Proximity Sensor · faultedDURING HEAVY MAINTENANCE: L/H FWD OVERWING EMERGENCY EXIT DOESNT DISARM WITH LATCH PIN RELEASED; REMOVED AND REPLACED L/H FWD EMERGENCY EXIT PROX SENSOR IAW AMM 52-73-11 OPS CK GOOD.SDR YENA2024071600999Landing Gear · faultedFLT#939, JFK-SJD. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO JFK). 'AFTER TAKEOFF BROUGHT GEAR UP AND NOSE GEAR STAYED DOWN.RECYCLED THE GEAR AND GEAR CAME UP SUCCESSFULLY THE SECOND TIME; REF LOGPAGE 3998665-2 (RESECURED NLG SUPPORT ON SDR YENA2024071600998Filter · warning messageFLT#2536, STI-JFK. (AIRCRAFT PERFORMED AN AIR TURN BACK TO STI) .' SMOKE DETECTION FAULT. MULTIPLE FALSE FIRE WARNINGS, LAVATORY B. ( LAVATORY SMOKE DETECTION SYSTEM ); REMOVED AND REPLACED LAV FLEECES FILTER IAW AMM 26-17-00. MDDR CLEARED, MX-4 UPDATED. PLACASDR AALA202407155274Lgciu · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED ON APPROACH INTO DFW DUE TO THE FLIGHT CREW REPORTED RECIEIVEING AN LGCIU #2 FAULT ECAM MESSAGE. THE FLIGHT CREW PERFORMED A GO AROUND AND ACCOMPLISHED THE CHECKLIST PROCEDURES AND NOTED THERE WAS NO COMPUTER RESDR AALA202407150513Bolt · missingAIRCRAFT WAS NOT GROUNDED: UPON LANDING GEAR EXTENSION, THE LEFT MAIN DOOR DID NOT CLOSE. LANDING GEAR DOORS NOT CLOSED ECAM DISPLAYED. FOUND PROX SENSOR (27GA) SWITCH-TARGET PROXIMITY HAD A MISSING LOWER MOUNT BOLT AND A LOOSE UPPER MOUNT BOLT CAUSING ERRATICSDR AALA202408278149Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL AT AFT GALLEY AREA BETWEEN FR 66 AND FR 68 AT S23R. REPLACED LOWER SILL PER SRM 51-72-11.SDR AALA202407315872Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION AFT CABIN FLOOR BEAM AT FR 66 AND -Y1732. REPLACED FLOOR BEAM PER SRM 51-42-11.SDR AALA202407314900Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION AFT CABIN FLOOR BEAM AT FR 68 AND -Y1162. REPLACED FLOOR BEAM PER SRM 51-42-11.SDR YENA2024071601029Hinge Arm · damagedDURING HEAVY MAINTENANCE: RUDDER HINGE ARM FITTING ASSY FORK END #2 DAMAGED; EC A24-798-01 ASSIGNED FOR TIME LIMITED REPAIR. DURING THE CURRENT (6/2024) C9 CHECK FOR A/C N510JB @ MEX, MEXICANA REPORTED 2 GOUGES AND ALL HOLES ELONGATED (#1-9) ON THE VERTICAL SDR YENA2024071601028Hinge Fitting · crackedDURING HEAVY MAINTENANCE: RUDDER ASSY HINGE FITTING BR1 WITH CRACK INDICATION; EC A24-811-01 ASSIGNED TO THIS REPAIR. DURING C9 CHECK ON N510JB (MSN 01280) AT MXA DATED JUN 2024, WHILE ACCOMPLISHING FORK END FITTING REPLACEMENT, CRACKED AND ELONGATED HOLE WERSDR YENA2024071601027Hinge Arm · damagedDURING HEAVY MAINTENANCE: RUDDER HINGE ARM FITTING #7 DAMAGED; EC A24-791-01 ASSIGNED TO THIS REPAIR.REFERENCES: DURING THE CURRENT (6/2024) C9 CHECK FOR A/C N510JB (MSN 01280) AT MXA, 4 ELONGATED HOLES WERE FOUND ON THE VERTICAL STABILIZER HINGE ARM BR7 DURINSDR YENA2024071601026Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER LOWER NODE & CONTINUITY FITTINGS / CRACKS - TEMPORARY REPAIR DURING C9 CHECK ON N510JB (MSN 01280) AT MXA DATED JUN 2024, WHILE ACCOMPLISHING REF /2/ SB NDT INSPECTIONS ON THE WSDR YENA2024071601021Hinge Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 5 ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1307953 TASKCARD: NR-00035) REMOVED AND REPLACED HINGE FITTING #5 LOCATED ON VERTICAL STABILIZER IAW A320 SRM 51-72-11-911-001 AND DRAWING #D 5571052 ISSDR YENA2024071601020Hinge Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 4 ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1307953 TASKCARD: NR-00036) REMOVED AND REPLACED HINGE FITTING #4 ON VERTICAL STABILIZER IAW A320 SRM 51-72-11-911-001 AND DRAWING #D 55371052 ISSUE E. SDR YENA2024071601019Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR 843; REF: ARM W/O 2024-178/1 N/R 2024-314581 ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON EMERGENCY EXIT DOOR 843 IAW EC# A320-52-1144 AND R&R SEGMENTS ISDR YENA2024071601018Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION IN FRAME SEGMENT 1 AT DOOR 834; REF: ARM W/O 2024-178/1 NR 2024-314582. ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON EMERGENCY EXIT DOOR 834 IAW EC# A320-52-1144 AND REMOVED AND REPLACED SEGMENTS IAW A320 SRM 5SDR YENA2024071601017Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION IN FRAME SEGMENT 1 AT DOOR 833; REF: ARM W/O 2024-178/1 NR 2024-314583. ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON EMERGENCY EXIT DOOR 833 IAW EC# A320-52-1144 AND REMOVED AND REPLACED SEGMENTS IAW A320 SRM 5SDR YENA2024071601016Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION IN FRAME SEGMENTS 1 AT DOOR 844; REF: ARM W/O 2024-178/1 NR 2024-314584 ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON EMERGENCY EXIT DOOR 844 IAW EC# A320-52-1144 AND REMOVED AND REPLACED SEGMENTS IAW A320 SRM 5SDR YENA2024071601015Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE OF TOP SKIN OVERHANG LOCATED ON RIB 14 ON RH WING;(RESOLVED ON W/O: 1307953 TASKCARD: NR-00047) REF AEROMAN WO 2024 178/1 NR 2024-3114797 REMOVED CORROSION LOC. ON RIB 14 PLUS 15 INCHES LOWER SURFACE OF TOP SKISDR YENA2024071601014Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT AFT GALLEY AREAA, DOOR STOP 1 INBOARD LOWER HOLE. CRACK INDICATION LOCATED A 5 OCLOCK VIEW LOOKING FROM FWD. DEPTH IS 0.067 INCHES; (RESOLVED ON W/O: 1307953 TASKCARD: NR-00053) ACCOMPLISHED REPSDR YENA2024071601013Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STG 37L FR 60 +19 INCHES TO STG 37L FR 62 +20 INCHES. FOUND OUT OF LIMITS; (RESOLVED ON W/O: 1307953 TASKCARD: NR-00054)(RESOLVED ON W/O: 1307953 TASKCARD: NR-00054 ) ACCOMPLISHED REPAIR IAW EC 24-790-01. REF AEROMAN NR 2024SDR YENA2024071601012Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE ON TOP SKIN OVERHANG ON RIB 8 ON RH WING; ACCOMPLISHED REPAIR IAW AEROMAN EA 57-9004 REV 0. AND AIRBUS RDAF 81405159/020/202#A. REF AEROMAN NR 2024-314659. (CONSIDERED A MAJOR REPAIR)SDR YENA2024071601011Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE OF TOP SKIN OVERHANG ON RIB 7 ON RH WING; ACCOMPLISHED REPAIR IAW AEROMAN EA 57-9004-24 REV 0 AND AIRBUS RDAF 81405159/020/202#A REF AEROMAN NR 2024-314659.SDR YENA2024071601010Support · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOCATED BTW FRAME 60 AND FRAME 62 IN BULK CARGO COMPARTMENT; PERFORMED REPAIR ON LOWER SILL BULK CARGO COMPARTMENT LOACTED BTW FR 60 PLUS 19 IN IAW A320 SRM 53-41-49-300-003. THIS REPAIR IS CATEGORY B AT DEFINED ISDR YENA2024071601009Support · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL EXISTING REPAIR LOCATED AT STR 23L FR 68 AFT GALLEY AREA; PERFORMED REPAIR LOCATED ON LOWER SILL AT STR 23L AND BETWEEN FR 67 TO FR 68 AFT GALLEY AREA IAW A320 SRM 53-41-14-300-001 FIGURE 001(SHEET) 3. REF AEROMANSDR YENA2024071601008Skin · crackedDURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / FR54-64 & STGR 37L-38L / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-9012-24 COVER AND P1-P3 /2/ AIRBUS RDAF 80524263/050/2024 ISSUE A /3/ AIRBUS TD/80524263/054/2024#A /4/ AIRBUS RDAF 8052426SDR YENA2024071601007Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / FR68 RHS / DOOR STOP FITTING #1 / LOWER INBOARD HOLE / CRACK - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-9007-24 REV. 0 (COVER + PART 1) /2/ AIRBUS RDAF 81404539/004/2024#A/3/ AIRBUS DOSSIER 81404539 /4SDR YENA2024071600997Pressure Switch · failedFLT#1691, JFK-LIR. (AIRCRAFT DIVERTED TO MCO) 'APU AUTO SHUTDOWN IN CRUISE FLIGHT -ATTEMPTED RESTART IN COORDINATION WITH MCC BUT IT WAS NOT SUCCESSFUL UNIT REMAINED OFF FOR DURATION OF FLIGHT; PER TSM 49-00-81-810-819A REMOVED AND REPLACED LOW OIL PRESSURE SSDR AALA202408271661Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SHEAR PLATE AT AFT GALLEY AREA BETWEEN FR 69 AND FR 70 AT S23R. REPLACED LOWER SILL PER SRM 51-72-11.SDR AALA202408143684Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON SHEAR PLATE LOCATED AT STR 23L AND BETWEEN FR 69 AND FR 70 IN AFT GALLEY AREA. REPLACED SHEAR PLATE AND FASTENERS PER SRM 51-42-11-801.SDR AALA202407262828Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER /CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.SDR AALA202407244626Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 68 AND -Y464.8. REPLACED FLOOR BEAM PER SRM 51-42-11.SDR CALA2024071502036Profile · gougedEMERGENCY EXIT INTERNAL STRUCTURE R/H FWD HATCH GOUGES ON AFT LO AD TRANSMITTING PROFILE. REMOVED AND REPLACED AFT FRAME SEGMENT ON FWD O/W HATCH RH IAW A 320 SRM 51-72-11-911-001SDR CALA2024071502035Profile · gougedEMERGENCY EXIT INTERNAL STRUCTURE R/H FWD GOUGES ON FWD LOAD TRA NSMITTING PROFILE. REMOVED AND REPLACED FWD FRAME SEGMENT ON FWD O/W HATCH IAW A320 SRM 51-72-11-911-001SDR YENA2024071100952Unknown · odorFLT#131, MCO-LAX. 'ON FINAL APPROACH FLIGHT ATTENDANT NOTED BR/EF DIRTY SOCK TYPE ODOR. THIS WENT AWAY SHORTLY AFTER LANDING ROLL-OUT. NEITHER CAPT NOR F/O NOTICED ANYTHING; SEE LOG PAGE 4087210, ITEM 2 (COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION A ISOSDR GTIA2024071238225Unknown · odorSUSPECTED FUEL LEAK AT TOP OF CLIMB FA CALLED AND REPORTED SMELL OF FUEL MID CABIN BACK-PERFORMED GVI OF EXTERIOR OF A/C AND ENGINES RAN ENGINES WITH CREW PERFORMED NITE TEST OF FQIC NO DISCREPENCIES NOTED NO LEAKS NOTED AT THIS TIME AMM 71-00-11/28-42-00 NO OSDR GTIA2024071238224Fan · odorDURING CRUISE AT FL380 ELECTRICAL BURING SMELL IN CABIN AND FLIGHTDECK WENT AWAY IN APPROXIMATELY 2 MINUTES. AMBER FAN MESSAGE ON CONDITION PAGE AND LOWER ECAM AFT COMPARTMENT.-PERFORMED TSM 05-50-00-810-831-A. FOUND CAUSE OF ODOR TO BE R RECIRC FAN. REF 34033SDR GTIA2024071238223Megaphone · inoperativeAFT MEGAPHONE INOP -REMOVED AND REPLACED AFT MEGAPHONE IAW SPIRIT AIRLINES DRAWINGS A320 CEO EMERGENCY EQUIPMENT LAYOUT DRAWING MOC # 114724SDR YENA2024071100987Shear Tie · corrodedDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 32 BTW STR 39R AND STR 40R IN FWD CA RGO COMPARTMENT (CPCP FINDING ); (RESOLVED ON W/O: 1280173 TASKCARD: NR-00048) REF AEROMAN WO# 2024 38/1 NR# 2024-32806. REMOVED AND REPLACED SHEAR TIE LOCATED AT SDR YENA2024071100986Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON HOLE C, FR 16 DOUBLE JOGGLE AREA, CRACK DIRECTION AT 9 OCLOCK RH SIDE, CRACK DEPTH 0.145 INCHES, CONFIRM EACH INDICATION USING BOROSCOPE VIEW AS PER NTM 51-90-00; (RESOLVED ON W/O: 1280173 TASKCARD: NR-00024)
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