Service difficulty reports
1,771,154 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 UIEA2026060100424Stowage Box · no testCAPTAIN SIDE O2 MASK AUDIO INTERCOM WILL NOT TEST. R & R CAPT SIDE O2 MASK STOWAGE IAW AMM 35-11-51 AND IPC 35-11-52-15. OPS CHECK GOOD. NO DEFECTS NOTED.SDR QMLA2026060120033Chip Detector · contaminatedUPON LANDING TO TRANSLOAD A PATIENT, THE TGB CHIP LIGHT ILLUMINATED. DUE TO THIS INDICATION AND SUBSEQUENT ENGINE SHUTDOWN, WE WERE UNABLE TO COMPLETE THE TRANSPORT OF THE PATIENT. THE PATIENT WAS THEN MOVED BY AMBULANCE. CHIP DETECTOR CLEANED, FINDINGS INDICASDR AALA202606017198Power Supply · no testAIRCRAFT IN BASE MAINTENANCE: EPL BATTERY ZONE 2 FAILS 15 MIN TEST (SEATS 7 D/H ,8D/H,9D/H ,10D/H) IAW CARD 72C20033014 STEP 2. MAINTENANCE REPLACED EMERGENCY BATTERY M33098 IAW AMM 33-51-06.SDR AALA202606012910Elec Connector · looseAIRCRAFT WAS NOT GROUNDED: DURING ACCOMPLISHEMENT OF PS CHECK IT WAS FOUND FWD GALLEY FLOOR PROXIMITY LIGHTS INOP. MAINTENANCE FOUND PLUG D911P ABOVE THE GALLEY LOOSE, RECONNECTED THE PLUG OPERATIONAL CHECK DONE WORKS FINE IAW AMM 33-51-05 AND WDM 31-51-51.SDR CALA2026060116709Lens · damagedAFT EXT OVERWING SLIDE EMER LIGHT ON LT AND RT SIDE OF AC WILL NOT ILLUMINATE, RELAMPED LH SIDE EMG LIGHT, OPS CHECK GOOD. RH EMG LIGHT LENSE COVER DAMAGED AND SREWS STRIPPED DURING REMOVAL. WAITING ON NEW PARTS FOR RH SIDE. CORRECTION RH EXT EMG AFT SLIDE LSDR CALA2026060116665Oven · odorFA REPORTS OVEN 105 PRODUCED SMOKE. TURNED OVEN OFF-NO SMOKE N OTED. FOUND BURNT FOOD RESIDUE IN THE OVEN INSERT, OVEN INSERT REMOVED AND OVEN OPERATED FULL CYCLE (25 MINUTES). NO SMOKE OR ODORS OBSERVED. FORM 46-6020 COMPLETED BY CABIN CREW, TOMC CONTACTED IASDR AALA202606011183Threshold · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION UNDER AFT PASSENGER CABIN LAVATORY 4F-1L THRESHOLD. REPAIRED PER EA 374741.SDR DALA2026060103312Unknown · odorONCOMING FA'S REPORTED WET SOCK ODOR. C/W A320 AMDS W/C 0550-2002 STEPS 1-4-CONTACTED MCC-C/W W/C 2100 -2007 LEVEL "A" DECONTAMINATION-ALL CHECKS GOOD-P-TRAK SNIFFER TEST SHOWS IN GOOD/LOW RANGE-A/C OK FOR SERVICE-SEE ITEM LOG 8834161 CONTROL # 1621231 FOR DESDR DALA2026053103303Floorbeam · crackedAD RELATED AA 5711-01036-CENTER WING FRONT SPAR VERTICAL STRINGERS, CRACKS FOUND ON FLOORBEAM SIDE VERTICAL RADIUS AT-Y765 ZONE 1 CRACK L= 0.250 INCHES APPROX AT ZONE 2 CRACK L= 0.400 INCH APPROX, REPAIR IS R EQUIRED PRIOR TO FUTHER FLIGHT. COMPLIED WITH ER/ASDR DALA2026053103302Structure · damagedDURING DVI WAS FOUND EXISTENT REPAIR BUSHING LOCATED ON SPAR VERTICAL STRINGER AT FR 36 ZONE 1 AND 2 -Y765 ( AD RELATED AA 5711-01036). PERFORMED REPAIR INSTRUCTION ON SPAR VERTICAL STRINGER AT FR 36 ZONE 1 AND ZONE 2 ON -Y765 AS PER ER/A 587692-14AD REV. B SSDR DALA2026053103301Structure · damagedDURING DVI WAS FOUND EXISTENT REPAIR BUSHING LOCATED ON SPAR VERTICAL STRINGER AT FR 36 ZONE 1 AND 2 -Y254 (AD RELATED AA 5711-01036). PERFORMED REPAIR INSTRUCTIONS ON SPAR VERTICAL STRINGER AT FR 36 ZONE 1 AND ZONE 2 ON -Y254 AS PER ER/A 587692-14AD REV. B SSDR DALA2026053103284Fitting · corrodedLEVEL 2 CORROSION, CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A319 SRM 54-51-12-300-001. TOOK MEASURE INITIAL CORROSION SPIGOT FITTINGWAS: P1: L:2.418 INCH, P2: L: 2.872 INCH, SEE INDIVIDUAL SIGN OFFSDR DALA2026053103283Fitting · corrodedLEVEL 2 CORROSION, CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON LH PYLON AS PER A319 SRM 54-51-12-300-001. TOOK MEASURE INITIAL ON CORROSION SPIGOT FITTING RECEPTACLE WAS: P1: L:3.058 INCH, P2: L: 1.602 INCH. SEE INDISDR DALA2026053003282Valve · faultyDIV - INTO JFK DUE TO DUAL ENG AIR BLEED FAULTS. REPLACED NR 1 ENGINE HARNESS 4246KS, NR 2 ENGINE THERMOSTAT, TR PRESS SUPPLY VALVE AND PRV 4001HA. OPS AND FLIGHT TEST GOOD. (8635299) AIRCRAFT WAS GROUNDED.SDR SWIA2026052977644Skin · dentedDENT ON ACFT SKIN BETWEEN FS28000 FS29500, STGR14L STGR15L REPAIRED AC SKIN BETWEEN FS28000 FS29500, STGR14L STGR15L MX 32348809 BY COMPLYING WITH ALL STEPS OF REO 690-53-00-657 REV-- DATE 2026-06-11 COMPLIED WITH ALL STEPS OF TASKCARD 51-900-1002-SKYSDR 2026FA0000770Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.SDR SWIA2026052977179Frame · chafedBS 654. 50 FRAME HAD CHAFE DAMAGE AT THE AFT INBD EDGE, APPROX 015 LONG AND 035 DEEP, BTWN STR 13R & 14R. REPAIRED BS 654. 50 IAW REO 601R-53-61-8548, REV -. COMPLETED SKYCARD 51-900-1003-SKY. NO WEIGHT CHANGE. SEE CONTINUE CARD FOR DETAILS OF WORK PERFOSDR CALA2026082718984Skin · damagedINTERIM REPAIR OF LIGHTNING STRIKE DAMAGE AT BS 500A TO 500B STR S-2L TO S-3L. ACCOMPLISH REPEAT INSPECTION REQUIREMENTS OF DOUBLER BETWEEN STA500A TO 500B AND STRINGER S-2L TO S-3L PER ECRA 5310-08866 PART 2 STEP 1 WITHIN 50,000 TOTAL FLIGHT CYCLES.SDR CALA2026082718982Skin · damagedINTERIM REPAIR OF LIGHTNING STRIKE DAMAGE AT BS 500A - 500B AND STRINGER S2L TO S3L IAW ECRA 5310-08866. ACCOMPLISH REPEAT INSPECTION REQUIREMENTS OF DOUBLER BETWEEN STA500A TO 500B AND STRINGER S-2L TO S-3L PER ECRA 5310-08866 PART 2 STEP 2 WITHIN 50,000 TOTSDR SWIA2026052976891Pressure Deck · corrodedRIGHT PRESSURE FLOOR PANEL, BTWN BS 409+128, & BS 559 HAS MULTIPLE AREAS OF CORROSION. REMOVED CORROSION FROM RT PRESSURE FLOOR PANEL BTWN BS 409+128 & BS 559, 16EA SPOTS. IAW REO 601R-53-41-666, REV-C. DISPOSITION 1.2 STEP.A. FOUND TO BE WITHIN LIMITS. COMSDR SWIA2026052976888Pressure Deck · corrodedLEFT PRESSURE FLOOR PANEL, BTWN FS 409+128 & BS 559 HAS MULTIPLE AREAS OF CORROSION. REPAIRED CORROSION DAMAGE ON LT PRESSURE FLOOR PANEL, IAW REO 601R-53-41-666, REV-C, COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.SDR AALA202607227243Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER BETWEEN FR 59 AND FR 60 AT S42L. REPAIRED STRINGER PER EA 376515.SDR AALA202607147542Support Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FALSE REAR SPAR FALSE SUPPORT FITTING BETWEEN RIB 7 AND RIB 8. REPLACED SUPPORT FITTING PER SRM 51-42-11.SDR SWAA2026070607600Floorbeam · corrodedCORRODED FLOORBEAM, BS 986.5, LBL 43, WL 208.1. APPLIED PROTECTIVE TREATMENT ON FASTENER HEADS OF FLOORBEAM IAW SRM 53-70-51-2R-6 REPAIR 6 PARAGRAPH 4.Q. PERFORMED PERMANENT REPAIR ON FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.SDR SWAA2026070607722Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 192HR BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 192HR BODY FAIRING AT LOWER FUSELAGE IAW SRM 51-70-05-2R-10 REPAIR 10.SDR SWAA2026063007668Window Frame · crackedF/O'S NR 1 WINDOW FRAME POST OTBD UPPER CORNER IS CRACKED. F/O'S NR 1 WINDOW FRAME REPAIRED IAW EA 26-153-01462.SDR AALA202606300624Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT BS 947 BETWEEN LBL 23.5 AND LBL 27. REPAIRED CHORD PER SRM 53-70-51-2R-5.SDR AALA202606306678Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT BS 947 BETWEEN LBL 50 AND LBL 53. REPAIRED CHORD PER SRM 53-70-51-2R-5.SDR AALA202606303069Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT BS 947 AND LBL 7. REPAIRED CHORD PER SRM 53-70-51-2R-5.SDR AALA202606304965Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT BS 947 AND RBL 26. REPAIRED CHORD PER SRM 53-70-51-2R-5.SDR SWAA2026062907712Stringer · crackedCRACKED STRINGER 23R, BS 540 IN THE FWD CARGO BAY. PERFORMED PERMANENT REPAIR ON STRINGER 23R LOCATED BS 500D TO BS 540 IAW SRM 53-00-03?2R-1, REPAIR 1.SDR SWAA2026062907594Access Panel · crackedCRACKED BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB. REPLACED BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02.SDR SWAA2026062907716Rib · crackedCRACK ON INSPAR RIB LOWER CHORD LOCATED ON STAB STA 120.30 AND 36 INCHES FROM FRONT SPAR AT RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR LOCATED ON INSPAR RIB 120.30 AT 36 INCHES FROM FRONT SPAR AT LT HORIZONTAL STAB IAW SRM 55-10-09-2R-5. REPAIR 5.SDR HNAA2026062600556Bracket · crackedCARGO DOOR PROP UP POINT HAS CRACKED BRACKET. R & R BRACKET IAW SRM 51-40-02.SDR AALA202606265868Tee Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER TEE ANGLE AT BS 947 AND RBL 49. REPAIRED THE TEE ANGLE IAW SRM 53-70-51-2R-5.SDR SWAA2026062507595Support · corrodedCORROSION ON SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 RBL 22 WL 156.1 AT AFT CARGO BAY. REPLACED SUPPORT ZEE LOCATED WL156 BTW BS727 TO BS767 AND RBL22 WL 156.1 AT AFT CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 146A7500, SHEET 85, REV A.SDR SWAA2026062507597Support · corrodedCORROSION SUPPORT ZEE LOCATED BTW BS 727E TO BS 787 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT. PERFORMED REPAIR LOC BTW BS727E MORE 10 INCH TO BS847 AND (CLIP) SIDE PLATE (1E/A) LOCATED BTW STA 767 TO STA 787 LBL22 AND WL156 AFT CARGO COMPARTMENT IAW SRM 53-00SDR SWAA2026062507596Cargo Track · crackedCRACK ON CARGO TRACK LOCATED BS 767 LBL 17.24 WL 156.1 AT AFT CARGO BAY. PERFORMED PERMANENT REPAIR LOCATED BETWEEN BS 747 MORE 5 INCH TO BS 767 MORE 15 INCH LBL 17.24 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-53-2R-3; REPAIR 3<BR>SEE INDIVIDUAL SIGN SDR SWAA2026062507714Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED AFT FACE BS 500D, STR 28L AT FWD CARGO BAY. REPLACED SUPPORT ANGLE LOCATED AFT FACE BS 500D AT LEVEL STR 28L AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7902 SHEET 126 REV A.SDR SWAA2026062407749Light · deterioratedDETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING STRIP IN THE PASSENGER CABIN. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING STRIP IAW AMM 33-51-15-960-801, AND DWG 33500007, REV 2.SDR SWAA2026062307679Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BS 694 AND RBL 24.82 AT PASSENGER CABIN. REPLACED ANGLE FLOOR STRUCTURE LOCATED BS 694 TO RBL 24.82 AT PASSENGER CABIN IAW SRM 51-40-02-0G-0, AND DRAWING 111A6000, SHEET 208, REV-, AND SRM 51-10-02-0G-0, ITEM 9.SDR SWAA2026062307678Crossbeam · crackedCRACK FLOOR STRUCTURE BREAK PANEL ON BS 540 BTW LBL 0.07 TO RBL 24.82. REPLACED BREAK PANEL LOCATED ON FLOOR STRUCTURE BS 540 AND BTW LBL0 TO RBL 24.82 IAW DWG 143A0060, SHEET 36, REV A, SRM 51-40-02-0G-0, & SRM 51-10-02-0G-0, PARAGRAPH 9.SDR SWAA2026062307680Angle · crackedCRACKED ANGLE FLOOR STRUCTURE LOCATED BS 694 LBL 0.07 IN THE PASSENGER CABIN. REPLACED ANGLE FLOOR STRUCTURE LOCATED BS 694 BTW LBL 24.82 TO LBL 0.07 IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0, PARAGRAPH 9, AND DWG 273A9110, SHEET 6, REV A.SDR SWAA2026062307681Skin Panel · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STAB LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 8 INCH. FROM REAR SPAR. INBD SIDE OF RIB. ON STEP 7 AND 8. PERFORMED REPAIR ON LT HORIZONTAL STAB LOWER SKIN PANEL IAW SRM 55-10-01-2R-11, REPAIR 11.SDR SWAA2026062207613Angle · crackedCRACKED UPPER ANGLE BS 694, BL 0. REPLACED THE UPPER ANGLE & FASTENERS IAW SRM 51-40-02, SRM 51-10-02, & DWG 273A9110, SHEET 6, REV A.SDR SWAA2026062207731Crossbeam · crackedCRACK ON BREAK PANEL LOCATED BS 540, BL 0 - LBL 24.75. REPLACED THE BREAK PANEL IAW SRM 51-40-02, SRM 51-10-02, ITEM 9.SDR SWAA2026062207612Angle · crackedCRACKED LOWER ANGLE, BS 694, BL 0. REPLACED LOWER ANGLE IAW SRM 51-10-02, SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.SDR SWAA2026062207730Crossbeam · crackedCRACKED BREAK PANEL, BS 540, BL 0 - RBL 24.75. REPLACED BREAK PANEL IAW SRM 51-40-02.SDR ASAA2026052966881Skate Angle · crackedCENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE SHOWS SIGNS OF BEING CRACKED AT BS.661.95 LBL+9. GROUNDED - YES. ACCOMPLISHED REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR IAW SRM 57-10-10-2R-5, REPAIR 5.SDR ASAA2026052966880Skate Angle · crackedCENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE SHOWS SIGNS OF BEING CRACKED AT BS.661.95 RBL+9. GROUNDED - YES. ACCOMPLISHED REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR IAW SRM 57-10-10-2R-5 REPAIR 5.