Service difficulty reports
1,771,708 reports of malfunctions and defects, newest first. Air carriers must report; 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' 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' 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 AALA202602048516Unknown · odorAIRCRAFT WAS GROUNDED: DIRTY SOCK ODOR ON DESCENT APPROXIMATELY 14000' NORMAL PACK CONFIGURATION APU OFF. (OPEN)SDR AALA202602042244Unknown · odorAIRCRAFT WAS GROUNDED: DURING DESCENT STRONG ODOR PRESENT IN FLIGHT DECK AND AFT GALLEY. MOSTLY ASSOCIATED WITH POWER CHANGES. IMPROVED IN FLIGHT DECK AFTER CROSS-BLEED SELECTED TO SHUT. STRONGER IN AFT GALLEY AFTER CROSS-BLEED SHUT. (OPEN)SDR AALA202602043667Diaphragm · leakingAIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. MAINTENANCE REPLACED THE DIAPHRAGM ON THE L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00-610-001-A.SDR AALA202602040697Actuator · trippedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INTO DFW DUE TO THE FLIGHT CREW REPORTING A SLAT / FLAPS FAULT DISPLAYED AND THE SLATS WOULD NOT EXTEND ON APPROACH. THE AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT WING #1SDR AALA202602049130Girt Bar · out of positionAIRCRAFT WAS GROUNDED: 1L DOOR SLIDE NOT ARMING. MAINTENANCE FOUND THE L1 DOOR SLIDE GIRT FLAP WAS NOT POISITIONED CORRECTLY, REPOSITIONED SLIDE GIRT FLAP PER AMM 25-62-44-400-006-A, A SATISFACTORY OPERATIONAL CHECK OF THE DOOR SLIDE ARMING SYSTEM WAS ACCOMPLISDR JJBA20260204003Fuse · failedLH FORWARD OF WING EMERGENCY LIGHT INOPERATIVE. INSTALLED NEW BULB. DID NOT FIX. INSTALLED NEW EMERGENCY LIGHT ASSEMBLY. DID NOT FIX. PUT BACK TO ORIGINAL CONFIGURATION. REMOVED AND REPLACED BAD FUSE ON FWD BATTERY CHARGE ASSEMBLY. REMOVED AND REPLACED LH FWD SDR JJBA20260204002Switch · inoperativePFD, MFD 2 WENT BLANK. FMS 1 WENT BLANK. AVIONICS 1 WENT OFFLINE (LIGHT ON). TURNED AVIONICS 1 BACK ON. FMS 1 SINGLE MODE TRIED TO GET FMS 1 BACK ON LINE AND IT DISPLAYED WHAT APPEARED TO BE A TEST PATTERN (COLORS ALPHABET) CA WENT TO REV MODE PFD BUT DATA DISSDR DXTA2026020406771Unknown · odorSTRONG ODOR OF FUMES ON DEPARTURE WITH TAKEOFF POWER. PER EMB CC ACCOMPLISH FIM TASK 21-20-00-810-801-A. C/W EMB-505 FIM TASK 21-20-00-810-801-A WITH NFF C/W HIGH POWER RUNS AND COULD NOT DUPLICATE THE SQK. PER MOC REQUEST POWERED ON ALL GALLEY/CABIN IFE EQUSDR DXTA2026020406773Seal · out of positionMAIN CABIN DOOR WILL NOT OPEN. HANDLE POPS OPEN HALF INCH AND ROTATES RIGHT A HALF INCH AND LOCKS UP. UNABLE TO MOVE THE HANDLE. ARRIVED TO ACFT. INSPECTED OUTER HANDLE, AND IT WAS DETERMINED THAT THE SECURITY SEAL, WHEN INSTALLED ON THE HANDLE RATHER THAN OSDR DXTA2026020406775Battery Pack · dischargedWHEN EMERGENCY LIGHTS ARE IN ARMED POSITION, ALL EMERGENCY LIGHTS ILLUMINATE. THEN AFTER A FEW MINUTES ALL LIGHTS START TO FLASH. SET BATTERY SWITCH TO ARM POSITION. EMERGENCY LIGHTS ILLUMINATED FOR ABOUT ONE MINUTE, FLASHED THEN EXTINGUISHED. CHARGED BATTERSDR YENA2026020400148Warning Message · illuminatedFLT 1190, SAN- JFK, (ETOPS). ELT CLASS II MSG, CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY FAULT INDICATED BY ELT. RESET ELT. CHECK GOOD REF AMM 25-60-00. MX4 UPDATED MDDR CLEARED.SDR YENA2026020400146Unknown · odorFLT 1229, EWR-CUN. DURING ENG RUN WITH NR 1 ENG AND NR 2 PACK. INFLIGHT IMMEDIATELY NOTICED SIGNIFICANT FUMES ODOR IN VICINITY OF ROW 22. INBOUND CREW HAD 2 FUME INCIDENTS ON INBOUND FLIGHT TO CUN. CREATING NEED FOR ENG RUN PRIOR TO BOARDING. ACCOMPSDR YENA2026020400145Lavatory · contaminatedFLT 2601, HON-SJU. ACFT EXPERIENCED A FUMES RELATED EVENT ON INITIAL TO SAN JUAN.; ACCOMPLISHED FIM TASK BD500-A-J21-00-04-AAA-423A-A. ISOLATED ODOR TO VINEGAR ON FWD LAV. CLEANED AND OPERATED PACKS FOR MORE THAN 40 MINS WITH NO ODOR PRESENT. NO FURTHER DEFESDR YENA2026020400142Panel · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND AT KEEL BEAM BOTTOM PANEL FASTENER HOLES 5, CRACK DEPTH 0.105 INCHES FWD DIRECTION; REF AEROMAN NR 2025-682674 WO 2025 413/1 ACCOMPLISHED REPAIR OF CRACK DAMAGE ON HOLE #5 ON THE CENTER FUSELAGE KEEL BEAM BOTTOMSDR YENA2026020400141Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER OPOST LOWER ATTACHMENT, VERTICAL FLANGE AREA RH SIDE. CRACK LENGTH 0.196 INCHES APPROX; REF AEROMAN NR 2025-682430 WO 2025 413/1 ERFORMED REPAIR TO CRACKS AFFECTING THE WINDSHIELD FRAME CENTSDR YENA2026020400140Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FR 36 IN FASTENER HOLE LOC Y1292 MORE 2 INCH UPPER SURFACE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX CRACK AT 12 O'CLOCK CRACK DEPTH 0.157 INCH APPROX IN FWD CARGO COMPARTMENT; PERFORMED REPAIR IAW EC A26-01SDR YENA2026020400139Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN OPEN HOLE FASTENER LOC Y1292 MORE 4 INCH UPPER SURFACE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX CRACK AT 5 O'CLOCK, CRACK DEPTH 0.160 INCH APPROX IN FWD CARGO COMPARTMENT (1 EA); PERFORMED REPAISDR YENA2026020400138Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 36 IN OPEN HOLE FASTENER LOCATION Y1292 MORE 5 INCH UPPER SURFACE OF THE PRESSURE DECK MEMBRANE TO CENTER WING BOX CRACK AT 6 O'CLOCK POSITION, CRACK DEPTH 0.131 INCH APPROX IN FWD CARGO COMPARTMENT (1EA); PESDR YENA2026020400137Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FR 36 IN OPEN FASTENER LHOLE LOC Y1292 MORE 8 INCH UPPER SURFACE OF THE PRESSURE DECK MEMBRANE TO CNETER WING BOX. CRACK AT 1 O'CLOCK CRACK DEPTH 0,140 INCH APPROX IN FWD CARGO COMPARTMENT (1 EA); REF AEROMAN NR 2SDR YENA2026020400136Fitting · crackedDURING HEAVY MAINTENANCE: CRACK ON CONTINUITY FITTING LH AT COCKPIT; REF AEROMAN NR 2025-682704 WO 2025 413/1 PERFORMED REPAIR TO CRACKS AFFECTING THE WINDSHIELD FRAME CENTER POST LOWER NODE AREA R/H VERTICAL FLANGE AND CONTINUITY FITTINGS ASPER AEROMAN EA# 53SDR YENA2026020400135Structure · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 1, POSITION 4 OF VERTICAL STRINGER RADIUS IN CENTER FUSELAGE ON FR 36, CRACK DEPTH 0.129 INCH CRACK DIRECTION 3 AND 4 O'CLOCK VIEW LOOKING AFT; REF AEROMAN NR 2025-682309 WO 2025 413/1 PERFORMESDR YENA2026020400134Stringer · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 1 POSITION 6 OF VERTICAL STRINGER REDIUS IN CNETER FUSELAGE ON FRAME 36 CRACK DEPTH O.085 INCH CRACK DIRECTION 6 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC NO. A25-1157-01 AND EA NO. 57-SDR YENA2026020400133Stringer · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE W1, POSITION 1 OF VERTICAL STRINGER RADIUS IN CENTER FUSELAGE ON FRAME 36 CRACK DEPTH 0.100 INCH CRACK DIRECTION 12 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC A25-1157-01 AND EA 57-117-SDR YEN2026F00001Stringer · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 2, POSITION 2 OF VERTICAL STRINGER RADIUS IN CENTER FUSELGAE ON FRAME 36, CRACK DEPTH 0.130 INCH. CRACK DIRECTION 8 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC A25-1157-01 AND EA 57-0017-SDR YENA2026020400131Stringer · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 2, POSITION 5 OF VERTICAL STRINGER RADIUS IN CENTER FUSELAGE ON FRAME 36. CRACK DEPTH 0.127 INCH, CRACK DIRECTION 8 AND 9 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC A25-1157-01 AND EA 5SDR YENA2026020400132Stringer · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLDE ZONE 2, POSITION 5 OF VERTICAL STRINGER RADIUS IN CENTER FUSELAGE ON FRAME 36. CRACK DEPTH 0.127 INCH CRACK DIRECTION 8 AND 9 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC NO. A25-1157-01 AND SDR YENA2026020400130Stringer · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 2, POSITION 5 OF VERTICAL STRINGER RADIUS IN CNETER FUSELAGE ON FRAME 36. CRACK DEPTH 0.127 INCH, CRACK DIRECTION 8 AND 9 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC A25-1157-01 AND EA 5SDR YENA2026020400129Seat Track · brokenDURING HEAVY MAINTENANCE: BROKEN SEAT TRACK Y1292, -Y765 AND -Y1292 BOLT AT LEVEL FR47 IN PASSENGER CABIN (3EA); REF AEROMAN WO# 2025-413/1 WCC# 2025-682634 FOR WORK PERFORMED; REMOVED AND REPLACED SEAT TRACK BOLTS LOC. Y1292, -Y765 AND -Y1292 AT LEVEL FR47 ISDR YENA2026020400128Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOC BTW FR 56 TO FR 57 IN AFT CARGO COMPARTMENT (CPCP FINDING); REF AEROMAN NR 2025-682543 WO 2025 413/1 REMOVED AND REPLACED STRINGER 43LH LOC BTW FR 54 TO FR 60 IN AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11, SDR YENA2026020400127Structure · crackedDURING HEAVY MAINTENANCE: CRACK FLOOR STRUCTURE UPPER SECTION CONNECTION LOC FR 66 AT LEVEL STR 23KH AT AFT GALLEY AREA (1EA); REMOVED AND REPLACED FLOOR STRUCTURE UPPER SECTION CONNECTION LOC FR 66 AT LEVEL STR 23LH SIDE AT AFT GALLEY AREA (1EA)IAW A320 SRM 5SDR YENA2026020400126Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOC BTW FR 57 TO FR 58 IN AFT CARGO COMPARTMENT (CPCP FINDING); REF AEROMAN NR 2025-682544 WO 2025 413/1 REMOVED AND REPLACED STRINGER 43LH LOC BTW FR 54 TO FR 60 IN AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11, SDR YENA2026020400125Stringer · corrodedDURING HEAVY MAINTENANCE:CORROSION STRINGER 43L LOC BTW FR 54 TO FR 56 IN AFT CARGO COMPARTMEN T (CPCP FINDING); REF AEROMAN NR 2025-682549 WO 2025 413/1 REMOVED AND REPLACED STRINGER 43LH LOC BTW FR 54 TO FR 60 IN AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11, SDR YENA2026020400124Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION FALSE SPAR BOX LOWER SKIN UPPER SURFACE AT LEVEL RIB 6A ON RH WING (CPCP FINDING); ACCOMPLISHED REPAIR OF CORROSION DAMAGE ON THE RH WING, BOTTOM SKIN PANEL 3 UPPER SURFACE AT LEVEL RIB 6A, FALSE SPAR BOX AREA I.A.W AEM AE SDR YENA2026020400123Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION SKIN PANEL INTERNAL STRUCTURE LOC BTW FR 16 AND 17 LOWER AREA ON LATERAL AVIONIC COMPARTMENT LT SIDE. PERFORMED PERMANENT REPAIR IAW EA# 53-0089-25, EC# A26-029-0. REPAIR IS CAT A AND NO FURTHER INSPECTION IS REQUIRED. WORSDR YENA2026020400122Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION ON SPIGOT LOWER FITTING ON LH PYLON; (RESOLVED ON W/O: 1420259 TASKCARD: NR-00037) REF AEROMAN NR 2025-682782 WP 2025-413/1. REMOVED AND REPLACED THE SPIGOT LOWER FITTING ON LH PYLON IAW SRM 54-51-283-002, SRM 51-44-11-801, SDR YENA2026020400121Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION IN THE SPIGOT LOWER FITTING ON RH PYLON; (RESOLVED ON W/O: 1420259 TASKCARD: NR-00038) REF AEROMAN NR 2025-682784 WP 2025-413/1. REMOVED AND REPLACED THE SPIGOT LOWER FITTING ON RHPYLON IAW SRM 54-51-283-002, SRM 51-44-11-80SDR YENA2026020400120Web · corrodedDURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE WEB LOC. BTW FR69/70 AT LEVEL STR23L AT AFT GALLEY AREA (1 EA) (CPCP FINDING); REF AEROMAN NR 2025-682631 WO 2025 413/1 REMOVED AND REPLACED FLOOR STRUCTURE WEB LOC BTW FR69 TO FR70 AT LEVEL STR23L AFT GALLEYSDR YENA2026020400119Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION SKIN PANEL INTERNAL STRUCTURE LOC BTW FR 16 AND 17 LOWER AREA ON LATERAL AVIONIC COMPARTMENT LH SIDE; PERFORMED PERMANENT REPAIR IAW EA# 53-0089-25, EC# A26-029-0. REPAIR IS CAT A AND NO FURTHER INSPECTION IS REQUIRED. WORKSDR YENA2026020400118Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE BOTTOM SKIN PANEL NO. 3, BTW REAR SPAR AND FA LSE REAR SPAR, AND BTW WX2825 STIFFENER DATUM AND RIB DATUM INBOARD DI AGONAL ON LH WING (CPCP FINDING); REF AEROMAN NR 2025-682418 WO 2025 413/1 CCOMPLISH REPAIR OSDR YENA2026020400117Doubler · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / NLG COMPARTMENT REINFORCEMENT DOUBLER AT FR16-17 AND Y+250 / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEM EA 53-0089-25 REV 0 (COVER AND PARTS 1 - 5) /2/ AIRBUS RDAF 81702470/003/2025#A /3/ REPAIR ISDR YENA2026020400116Floorbeam · crackedDURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / FRONT SPAR VERTICAL STRINGERS & HORIZONTAL FLOOR BEAMS / @ LEVEL OF FR36 & Y-1292, Y-765, Y-254, Y+254, Y+765 & Y+1292 / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 57-0117-25 REV. 0 (COVER + PARTS SDR YENA2026020400115Skin · corrodedDURING HEAVY MAINTENANCE: WINGS / LH WING / BOTTOM SKIN PANEL 3 / RIBS 6A, REAR SPAR-FALSE REAR SPAR / CORROSION - TEMPORARY REPAIR; REFERENCES: /1/ AEROMAN EA 57-0122-25 COVER & PARTS 1-11 /2/ AIRBUS RDAF 81692663/023/2025 ISSUE A /3/ AIRBUS TD/81692663/012/2SDR YENA2026020400114Pressure Deck · crackedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / PRESSURE DECK PANEL / FR36 RHS / ATTACHMENT HOLES / CRACKS – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0085-25 REV. 0 (COVER + PARTS 1-8) /2/ AIRBUS DOSSIER 81696490 /3/ AIRBUS RDAF 81696490/003/2SDR YENA2026020400113Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CTR POST LOWER NODE AREA VERTICAL FLANGE RHS & CONT. FITTING LHS / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0081-25 (COVER + PARTS 1-5) /2/ AIRBUS DOSSIER 81689336 /3/ SDR CALA2026020413580Skin · corrodedETOPS PREDEPARTURE SERVICE CHECK PROCEDURE, AFT WASTE SYS VACUUM BLOWER VENT PORT HAS AREA WITH SKIN BULGE AND POSSIBLE CORROSION. . CUT-OUT OF CORRODED SKIN, HFEC OF CUT-OUT , & MATERIAL VERFICATION WERE ACCOMPLISHED. IAW SRM 53-60-01-2R-3. VERIFIED HFEC OF SDR CALA2026020413548Outflow Valve · defectiveSAFETY VALVE STUCK OPEN CPC 1 TESTS OK. SUGGEST REPLACING CAB PR SAFTEY VALVE 6HL AND CPC 2. REF AMM 21-31-52/401 CONFIG 00. ENSURE SAFETY VALVE 7HL IS CLOSED UNLESS IT CAN BE POSITIVELY DETERMINED WHICH SAFETY VALVE OPENED, PER TSM 21-31-00-810-808-A, NEED TSDR CALA2026020413547Web · corrodedMAIN CABIN AFT WET AREA WEB HAS CORROSION ON UPPER SURFACE BETWEEN BS 986.5 AND BETWEEN LBL-24 & LBL-45. R & R NEW WET SUPPORT IAW DWG 147A5116, REV.A, SRM 51-40-02.SDR CALA2026020413546O-Ring · damagedFOUND WATER DRIPPING FROM BELLY DRAIN FWD OF FWD CARGO DOOR CONTROLS. WATER POOLING BELOW 80VU RACK. TRACED WATER BACK FROM BELOW 80VU RACK TO A WIGGINS FITTING FWD OF ACCLRM 12CE1 AND 12CE3. DISSASEMBLED FITTING REF AMM 20-23-38-000-001-A, FOUND FITTING COVERSDR CALA2026020413545Idg · faultedAFTER TAKEOFF LOST L GEN. CREW FOLLOWED FM AND DISCONNECTED IDG .BPCU READ OUT DISPLAYED L IDG HIGH DELTA TEMP. NR 1 ENG C DUCTS OPENED TO INSPECT IDG FOUND NO LEAKS OR EXTERNAL DEFECTS, FOUND DURING IDG SERVICING 1,5 QT OF OIL ON OVERFLOW CAME OUT. NO OTHER SDR SWIA2026020275117Pressure Switch · faultedPRKG BRK NOT RELEASED CAUTION MSG DURING DESCENT. CYCLE OF PRKG BRK LEVER IAW THE QRH CLEARED THE MSG INITIALLY, BUT THEN IT CAME BACK. UPON LANDING, NO ISSUES, NORMAL LANDING AND BRAKING. CAUTION MSG EXTINGUISHED AND REPLACED BY EMER BRK FAULT ADVISORY MESSAG