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 FDEA202608051086Lug · corrodedNR 3 ENGINE PYLON AFT BULKHEAD LUG BORE HOLE FOUND WITH CORROSION AND DAMAGE AFTER SPHERICAL BEARING REMOVED. REPAIRED IAW EA 1- 5440 -T0388311, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6 -2-100.SDR KCSA202608051114Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 652FB HAS CORROSIONSDR KCSA202608051113Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 652EB HAS CORROSIONSDR 2026FA0000620Pad · wrong partRECEIVED EMERGENCY EVACUATION SLIDE USED ON 737 ACFT FWD AND AFT DOORS. MAINTENANCE CHECKED THE COMPLIANCE FOR ALL APPLICABLE AIRWORTHINESS DIRECTIVES AND SERVICE BULLETINS. DURING THE INSPECTION OF THE AIRCRAFT COMPONENT AND VERIFICATION OF INCORPORATION OF SSDR KCSA202608051112Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 652BB HAD CORROSION.SDR KCSA202608051111Skin · corrodedRIGHT WING FUEL TANK ACCESS PANEL CUTOUT 652DB HAD CORROSION.SDR KCSA202608051110Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 653FB HAD CORROSION.SDR KCSA202608051109Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 653HB HAD CORROSION.SDR KCSA202608051108Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 653GB HAD CORROSION.SDR KCSA202608051107Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 646BB HAD CORROSION.SDR KCSA202608051106Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 652AB HAD CORROSIONSDR CALA2026080518307Lamp · inoperativeEMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPS CHECK, FWD RIGHT OVERWING DOOR LOWER EXIT SIGN HAS ONE LIGHT INOP. ACCOMPLISHED EXIT SIGN LAMP REPLACEMENT PER MM33-51-01-960-801, OPS CKD OK.SDR CALA2026080418250Control Unit · faultedSTABILIZER R2 ADVISORY THIS MESSAGE IS SET WHEN THE R2 CONTROL CHANNEL NOT AVAILABLE FOR TRIM OR WHEN 1ST OFFICER'S TRIM SWITCH HAS BEEN DISAB LED BY COLUMN CUTOUT. R2 REFERS TO ELECTRICAL BUS. DB 27 FCM OPS (RIGHT) DB 27 FCM OPS (CENTER) DB 27 FCM OPS (LT) DESDR VNAA202610280022Bushing · corrodedSECONDARY NRC: AFTER REMOVAL BUSHINGS AND BEARINGS ON AILERON LH IN REF TRFKE00BN353 CORROSION WAS FOUND ON HINGUE FITTING 4 UPPER SIDE, AND CENTER HIGUE FITTING L2 AND L5. HINGE FITTING 4 UPPER SIDE WAS PER SRM 51-26-00-001-001-A01 THEN INSPECTIONED PER NDT SDR SWIA2026080477531Floorbeam · damagedLH FLOOR SILL AT FS 280 HAS 4EA OVERSIZE HOLES WHERE IT ATTACHES TO FS280 CROSSBEAM C-CHECK RO 10062026REPAIRED LH FLOOR SILL AT FS280 WHERE IT ATTACHES TO FS280 CROSSBEAM IAW REO 670-53-21-2945 REV-- DATED 2026-08-08 COMPLETED TASK CARD 51-900-1003-SKY AND SDR SWIA2026080477212Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE RA107424-55-10-01AD02 MXCODEID118926-PR - COMPLY WITH PERMANENT REPAIR ON RA ID 107424INSPECTED DENT DAMAGE ON UNDERSIDE OF LT HORIZONTAL STAB JUST FWD OF PREVIOUSLY MAPPED DENTS PER SRM 55-10-01AD02 AND FOUND DAMAGE TO BSDR IXXA2026091601Skin Panel · delaminatedL/H UPPER SKIN PANEL OF L/H HORIZONTAL STABILIZER FROM STA 250-350 AT I/N END IS DELAMINATEDSDR REXA2026091101799Door · crackedLH AFT EMERGENCY EXIT DOOR UPPER FORMER CRACKED AT AFT LUG. PERFORMED LPI OF LH AFT EMERGENCY EXIT FORMER AT AFT LUG IAW REO 670-52-21-103 REV -, STEP 1 FOUND FORMER HAS INDICATION NOTED 1.2 INCHES LONG FAILED NDT AREA MARKED ON FORMER. COMPLETED STEPS 2, 3 ASDR REXA2026091001794Door · cracked"LH FWD EMERGENCY EXIT DOOR UPPER FORMER CRACKED AT AFT LUG. PERFORMED LPI OF LH FWD EMERGENCY EXIT FORMER AT AFT LUG IAW MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-06 STEP 1 FOUND FORMER HAS INDICATION NOTED 1.2 INCHES LONG FAILED NDT AREA MARKED ON FORMER.SDR IPXA2026090420255Gusset · corrodedAPU COMPARTMENT FWD BULKHEAD FWD SIDE BS 1885.2, LBL-12 & RBL-9. EXTENSIVE CORROSION. INSTALLED ONE SPLICE RING, ONE LOWER FRAME, ONE INNER TEE CHORD & TWO BRACKET ASSY (GUSSETS LT, RT) AT APU COMPARTMENT FWD BULKHEAD FWD SIDE BS 1885.2 LBL-12 & RBL-9 IAW SRM SDR SWAA2026090812381Support Bracket · crackedCRACKED SUPPORT BRACKET BS 540, LBL 6 IN THE A/C BAY. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.SDR SWAA2026090845565Support Beam · crackedCRACKED SUPPORT BEAM NR 4 FWD GALLEY DOOR. REPLACED THE SUPPORT BEAM IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 141A6535, SHEET 13, REV-.SDR SWAA2026090816087Plate · damagedELONGATED HOLE ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 321 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 321 AT RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02 AND DWG 115A3712, SHEET 7, REV A.SDR SWIA2026080477108Antenna · demodificationCOMPLY WITH LH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44) COMPLIED WITH LH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44). WEIGHT OF REPAIR PARSDR SWIA2026080477105Antenna · demodificationCOMPLY WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44) COMPLIED WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44). WEIGHT OF REPAIR PASDR SWIA2026080477104Antenna · demodificationCOMPLY WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44) COMPLIED WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93. REPAIR PARTS WEIGH 330.1 GRAMS NO CHANGE TO WEIGHT AND BALASDR SWIA2026080477102Antenna · demodificationCOMPLY WITH AFT ATG ANTENNA PERMANENT REPAIR IAW DWG 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44). COMPLIED WITH AFT ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44). WEIGHT OF REPAIR PARTS LESS THAN SDR SWAA2026090735916Web · crackedCRACKED WEB, ORSS 275, RT WING T/E. REPLACED THE WEB & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2512, SHEET 16, REV- .SDR SWAA2026090219960Fastener · looseFWD ENTRY DOOR SLIDE AFT GIRT BAR RETAINING BRACK FASTNERS LOOSE FWD ENTRY DOOR SLIDE AFT GIRT BAR WAS ACCESSED ON ROUTINE FWD EQUIPMENT CARD TTG8Q019FT9F STEP 20 TO F.O.M. AND WILL BE REINSTALLED ON ROUTINE FWD EQUIPMENT CARD TTG8Q019SFEG STEP 60. VERIFIED ITSDR SWAA2026090103788Floor Panel · elongatedELONGATED HOLE ON FLOOR PANEL 120CF IN THE FWD CARGO BAY FABRICATED FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT IAW AMM 25-52-01-201-801 PARAGRAPH 1.F AND DWG 453A1610 SHEET 2, REV D.SDR SWAA2026090142229Stringer · crackedSTRINGER18AL BS 727 UPPER FASTENER HOLE COMMON TO INNER CHORD INDICATES A CRACK DEFECT IN STR.18A PER BOEING NDT MANUAL PART6, 51-00-00 PROC.16. L/H STR.18A STA.727 UPPER FASTENER HOLE COMMON TO INNER CHORD INDICATES A CRACK DEFECT IN STR.18A PER BOEING NDT MASDR SWAA2026083172202Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BS 663 AT LEVEL RBL 8 AT AIR CONDITION BAY 2026-456227 EQUIPMENT USED HARDNESS TESTER P/N : GYZJ-934-1-250 S/N: 211123-28 DUE DATE : 16-MAR-27 AND ELECTRICAL CONDUCTIVITY METER : P/N : AUTOSIGMA3000DL S/N:567930/04 DUE DATE : 0SDR IPXA2026083107009Rib · crackedCRACKED RIB, AFT SIDE OF LT WING, INBD AILERON, INBD WEB UPPER CHORD, WBL 445. ACCOMPLISHED A REPAIR IAW EO-98460-REQ1, REV 1, & EGAT EI F2026A57M-1655, REV 1. MAJOR REPAIR.SDR VNAA202608310024Bushing · abnormalIN REFERENCE TO TRFKE00BN3TB: FABRICATE BUSHINGS ON LUGS L2 & R2 FROM AILERONS RT & LT. BUSHINGS ON LUGS L2 & R2 FROM AILERONS RT & LT WERE FABRICATED IAW REO 670-57-61-237, REV -.SDR IPXA2026082620255Bulkhead · corrodedAPU COMPARTMENT FWD BULKHEAD FWD SIDE BS 1885.2, LBL 12 & RBL 9. EXTENSIVE CORROSION.SDR SWAA2026082572025Support Angle · corrodedCORROSION FOUND ON FWD CARGO BAY AFT BULKHEAD SUPPORT ANGLE, BS 500I, LBL 31, WL 163. R & R THE BULKHEAD SUPPORT ANGLE, BS 500I, LBL 25 - 45, WL 163 IAW SRM 51-40-02, & DWG 143A9481, REV -.SDR SWAA2026082591219Scuff Plate · crackedFORWARD CARGO BAY AFT CORNER SCUFF PLATE CRACKED. R & R THE AFT CORNER SCUFF PLATE IAW SRM 51-40-02,SDR IPXA2026082507009Rib · crackedCRACKED RIB, AFT SIDE OF LT WING INBD AILERON INBD WEB UPPER CHORD, WBL 445.SDR REXA2026082401626Stringer · corrodedCORROSION WAS FOUND ON STGR 26R BTW FS 1015.00 TO 1031.00 AT INTERNAL FUSELAGE STRUCTURE. CORROSION ON STGR 26R BTW FS 1015.00 TO 1031.00 AT INTERNAL FUSELAGE STRUCTURE WAS REPAIRED PER EA NO. CRJ953-22756 REV. IRSDR REXA2026082401609Stringer · corrodedAFTER SPLICE REMOVAL, CORROSION WAS FOUND ON STGR 23R BTW FS 333. STRINGER SECTION 23RH BTW FS 333.00 TO 379.00 WAS REMPLACED PER CRJ 900 SRM 51-42-21-001-001-A01 6. C. AND SRM 51-42-13-001-001-A01 PAR 6SDR DALA2026082104766Door Frame · corrodedFWD CARGO DOOR AFT FRAME LOWER CORNER METAL PLATE CORRODED. EVALUATED &REPLACED FWD CARGO DOOR AFT FRAME PLATE IAW SRM 53-30-15. (1737995) AIRCRAFT WAS GROUNDEDSDR SWAA2026081919226Switch · inoperativeFUNCTIONAL CHECK, ALL EMERGENCY LIGHTS, OUTGOING, PERFORMED A GOOD OPS TEST OF ALL EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. FOUND EMERGENCY EXIT LIGHT INTEGRATED SWITCH ASSY DOES NOT OPERATE AND WILL BE ADDRESSED ON CCN: TTG8Q01DNVD2, LT AFT OVERWING EXISDR IPXA2026081903745Skin · crackedMAJOR REPAIR, SKIN , DURING PERFORM T/C : EO-24301-JIC001 FOUND SKIN CRACK AT BS 1725.5 , S-7R. ACCOMPLISH THE REPAIR I.A.W EO-24301-JIC3 REV7 AND SRM 53-80-01-2R-5 REV.95 AND EGAT WORK SHEET NO.60614 AND EO-98363-REQ1 REV1.SDR FXTA20260804001Strut · damagedDURING PREFLIGHT, IT WAS DISCOVERED THAT THE RH UPPER WING STRUT MISSING PART OF METAL FAIRING. APPEARS THAT DURING MANUFACTURE THE SEAMS WERE OFFSET CAUSING A STRESS IN THE SKIN ALLOWING IT TO CRACK.SDR SWAA2026081733004Floorbeam · crackedFLOORBEAM CRACKED, BS 537.45, LBL1, WL208. FLOORBEAM REMOVED AND REPLACED IAW SRM 51-40-02-0G, & DWG 143A0060, REV A.SDR SWAA2026081775452Tee Fitting · crackedECS BAY SUPPORT TEE FITTING CRACKED AT BS 649.9, RBL 40.9. LOCATED AND DRILLED A REPLACEMENT TEE FITTING IAW SRM 51-40-02, TREATED IAW SRM 51-20-01, & PRIMED IAW SOPM 20-41-02. REMOVED & INSTALLED A NEW SUPPORT TEE FITTING IAW SRM 51-40-02.SDR IPXA2026081706832Ring · crackedFOUND NR 1L T/R AFT CASCADE SUPPORT RING CRACK. COMPLETED THRUST REVERSER AFT CASCADE SUPPORT RING (ACSR) REPLACEMENT IAW EO-87822-REQ01L-REPL REV3.SDR IPXA2026081706840Ring · crackedFOUND NR 1R T/R AFT CASCADE SUPPORT RING CRACK. COMPLETED THRUST REVERSER AFT CASCADE SUPPORT RING (ACSR) REPLACEMENT I.A.W EO-87822-REQ01R-REPL REV4.SDR SWAA2026081442797Lamp · burned outL2 AND R2 DOOR EMERGENCY LIGHT BULBS ON THE DOWNLIGHTS REQUIRES RE-LAMP DO TO BURNT OUT BULBS RELAMPED L2 AND R2 DOOR EMERGENCY LIGHT BULBS OPS CHECK GOOD IAW AMM 33-51-01-960-802.SDR IPXA2026081303363Angle · crackedFOUND THE FIRE DETECTION LOOP FASTENER STRIP CRACKED AT BS 1562 LBL 76 IN BULK CARGO COMPARTMENT. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.95. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 218T4100 SH 3 REV: B AND BOEING DWG NO: 218T4