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 SWAA2026050482579Floorbeam · crackedCRACK BRAKE PANEL FLOOR STRUCTURE BS540 AND LBL4 AT PASSENGER CABIN. ] REPLACED BRAKE PANEL FLOOR STRUCTURE BS540 AND BL0 TO LBL24.75 AT PASSENGER CABIN IAW SRM 51-10-02-0G-0 ITEM 9 AND DWG# 143A0060; SHEET:64; REV:- .SDR SWAA2026050482580Floorbeam · crackedCRACK SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND RBL 1. REPLACED SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND RBL 1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 273A9110 SHEET 6 REV A.SDR SWAA2026050482581Floorbeam · corrodedCORRODED FLOORBEAM BS 986.5, LBL 43, WL 208.1 PASSENGER CABIN. PERFORMED REPAIR ON FLOORBEAM IAW SRM 53-70-51-2R-6.SDR VNAA20260501020Seat Track · corrodedCORROSION ON SEVERAL POINTS SEAT RAIL BTW FS667 TO FS720.85 AND FS744.15 TO FS761.85 AT RBL15 CAB PAX. CORROSION ON SEVERAL POINTS SEAT RAIL BTW FS667 TO FS720.85 AND FS744.15 TO FS761.85 AT RBL15 CAB PAX WAS EVALUATED WITH EXCESSIVE DAMAGE PER CRJ900 SRM 53-SDR VNAA20260501019Fitting · corrodedCORROSION ON FWD RH FITTING (1EA) UNDER WASTER CONTAINER AT FWD LAV. NEW FWD RH FITTING (1EA) UNDER WASTER CONTAINER AT FWD LAV WAS REPLACED SAFRAN CMM 25-40-40 REV. NO. 20SDR VNAA20260501018Fitting · corrodedCORROSION FLOOR FITTING IN FRONT ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FRONT ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-32-02SDR SWAA2026042882452Support Angle · crackedCRACKED SUPPORT ANGLE, BS 380 - 400, LBL 52, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02 AND DWG 143A5400, SHEET 7, REV-.SDR SWAA2026042882450Rib · crackedCRACKED RIB NR 8 LOCATED STRUCTURE OF DORSAL FIN ACCESS PANEL 321A. REPLACED RIB NR 8 LOCATED STRUCTURE OF DORSAL FIN ACCESS PANEL 321A IAW B737-800 SRM 51-40-020-G-0; DWG 174A1008 SHEET 3 REV- AND DWG 174A0103 SHEET 15 REV-.SDR SWAA2026042782594Support Beam · crackedCRACKED SUPPORT BEAM NR 4, FWD GALLEY DOOR. REPLACED THE NR 4 SUPPORT BEAM IAW SRM 51-40-02, SRM 51-10-02-0G-0, ITEM 9, AND DWG 141A6516, SHEET 142, REV-, DWG 141A6535, SHEET 13, REV-.SDR SWAA2026042482451Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1 AT PASSENGER CABIN . REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 AND DWG 143A5400 SHEET:38 REV:A.SDR SWAA2026042282587Nut Plate · crackedCRACKED RAIL NUT PLATE LOCATED LEADING EDGE INTERNAL CAVITY OFSS 574 AT RT WING. REPLACED RAIL NUT PLATE LOCATED LEADING EDGE INTERNAL CAVITY OFSS 574 AT RT WING IAW SRM 51-40-02 AND DWG 112A4402, SHEET 14, REV-.SDR SWAA2026042282588Rail · crackedCRACK ON RAIL NUT PLATE LOCATED LEADING EDGE INTERNAL CAVITY OFSS 487 AT RT WING. REPLACED RAIL NUT PLATE LOCATED LEADING EDGE INTERNAL CAVITY OFSS 487 AT RT WING IAW SRM 51-40-02 AND DWG#112A4402 SHEET 13 REV-.SDR SWAA2026042282589Angle · crackedCRACK ON ANGLE LOCATED AUXILIARY TRACK SLAT 8 AT RT WING. REPLACED ANGLE LOCATED AUXILIARY TRACK SLAT 8 AT RT WING IAW SRM 51-40-02-0G AND SRM 51-10-02 ITEM 9.SDR HNAA2026042100340Floor Support · crackedLH OMEGA BEAM IS CRACKED AT THE FR35 STANTION. ACCOMPLISHED REPAIR TO LH OMEGA BEAM AT THE FRAME 35 STATION IAW EMB 145 SRM 51-75-00, ETD2026-145-005461 AND EO1-53-26-0150.SDR HNAA2026042100339Floor Support · crackedLEFT OMEGA BEAM IS CRACKED AT THE FR 27 STANTION. REPAIRED THE LH OMEGA BEAM AT FR. 27 STANTION IAW EMB ETD2026-145-005372 REV A AND PIEDMONT EO1-53-26-0151SDR HNAA2026042100338Floor Support · crackedLH OMEGA BEAM IS CRACKED AT THE FR26 STANTION. ACCOMPLISHED REPAIR ON LH OMEGA BEAM AT FR 26 STANCHION IAW ETD 2026-145-005348 AND PIEDMONT EO1-53-26-0172.SDR HNAA2026042100337Floor Support · damagedCENTER OMEGA BEAM IS BLENDED BEYOND ALLOWABLE LIMITS JUST FWD OF THE FR29 CENTER AISLE CROSSBEAMSDR HNAA2026042100336Floor Support · crackedCENTER OMEGA BEAM IS CRACKED AT THE FR27 STANTION. ACCOMPLISHED PERMANENT REPAIR TO CRACKED CENTER OMEGA BEAM AT FR 27 STATION IAW ETD2026-145-005460 AND EO-1-53-26-0162.SDR HNAA2026042100335Floor Support · crackedCENTER OMEGA BEAM IS CRACKED AT THE FR25 STANTION. REPAIRED THE CENTER OMEGA BEAM AT THE FR. 25 STANTION IAW SRM 51-40-02, ETD2026-145-005274A AND PIEDMONT EO1-53-26-0154.SDR AALA202604146607Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT BS 947 BETWEEN LBL 52 AND RBL 52. REPAIRED CHORD PER SRM 53-70-51-2R-5.SDR SWAA2026041382548Scuff Plate · crackedACD AFT CORNER SCUFF PLATE IS CRACKED. REPAIRED ACD AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1 STEP 4.B.(4).SDR SWAA2026041382445Fitting · out of limitsTRANSITION FITTING HAS OVERSIZED NUTPLATE HOLES R/H WING WBL 658.17 AND REQUIRES REPLACEMENT REF: TTG8Q00Y6CF2. NO ALLOWABLE LIMITS GIVEN PER SRM THEREFORE PART REMOVED, DRILLED AND REPLACED IAW SRM 51-10-02-0G-0 PAR 9.C, SRM 51-40-05-0G-0, SRM 51-40-02-0G-SDR AALA202604102309Tie Down · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR FORWARD GIRT BAR TIEDOWN AT STA 312 AND LBL 55. REPLACED TIEDOWN PER AARD 51-00-05-1.SDR AALA202604105282Wedge · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT ENGINE AFT STRUT FAIRING TAIL SECTION WEDGE, INBOARD SIDE SKIN. REPLACED WEDGE PER AARD 51-00-05-1.SDR SWAA2026040182628Shield · crackedNR 2 ENGINE OTBD SHIELD AT 12 O'CLOCK, CRACKED. REMOVED AND REPLACED THE NR 2 ENGINE OTBD SHIELD IAW AMM 70-51-00-800-801-G00, STEP 2. D. (1).SDR SWAA2026040183482Shield · crackedNR 1 ENGINE SHIELD AT 9:30, CRACKED. REMOVED AND REPLACED THE NR 1 ENGINE SHIELD IAW AMM 70-51-00-800-801-G00, STEP 2. D.SDR SWAA2026040183484Shield · crackedNR 1 ENGINE SHIELD AT 10 O'CLOCK, CRACKED. REMOVED AND REPLACED NR 1 ENGINE SHIELD IAW AMM 70-51-00-800-801-G00, STEP 2.D, (1).SDR SWAA2026040183772Shield · crackedNR 1 ENGINE SHIELD AT 1 O'CLOCK, CRACKED. REMOVED AND REPLACED THE NR 1 ENGINE SHIELD IAW AMM 70-51-00-800-801-G00, STEP 2.D (1).SDR SWAA2026040183483Shield · crackedNR 1 ENGINE SHIELD AT 10:30, FOUND CRACKED. REMOVED AND REPLACED THE NR 1 ENGINE SHIELD IAW AMM 70-51-00-800-801-G00, STEP 2, D.(1).SDR IPXA2026032822628Filler · brokenBROKEN FILLER, RT HORIZONTAL STAB TIP AFT OTBD CORNER. INSTALLED A NEW FILLER IAW SRM 51-40-02-0G, REV 94, AND DWG 189T0001, SHT 1, REV E.SDR IPXA2026032822558Filler · damagedLIGHTNING STRIKE, FILLER, LT HORIZONTAL STAB TIP AFT OTBD CORNER. INSTALLED A NEW FILLER IAW SRM 51-40-02-0G, REV 94, AND DWG 189T0001, SHT 1, REV E.SDR SWAA2026033182627Cover · tornR2 AFT ESCAPE SLIDE COVER SURFACE IS TORN. VERIFIED R2 AFT ESCAPE SLIDE COVER SURFACE IAW SRM 51-10-02 PAR. 4.D.(1). ONLY THE SURFACE FINISH IS MISSING. NO DAMAGE NOTED. R2 AFT ESCAPE SLIDE COVER SURFACE NEEDS TO BE PAINTED. APPLIED CHEMICAL CONVERSION COATINSDR AALA202603310711Light · burned outAIRCRAFT IN BASE MAINTENANCE: BURNED LED CABIN EMERGENCY LIGHT ASSY ON UPPER DOOR FRAME RH S IDE AT AFT GALLEY AREA. MAINTENANCE REPLACED LED CABIN EMERGENCY LIGHT ASSY ON UPPER DOOR FRAME RH AT AFT GALLEY AREA FOR INSTALLATION REFER TO JOB CARDS 26C26125004,SDR AALA202603319441Light · burned outAIRCRAFT IN BASE MAINTENANCE: BURNED LED CABIN EMERGENCY LIGHT ASSY ON UPPER DOOR FRAME LH S IDE AT AFT GALLEY AREA. MAINTENANCE REPLACED LED CABIN EMERGENCY LIGHT ASSY ON UPPER DOOR FRAME LH SIDE AT AFT GALLEY AREA FOR INSTALLATION REFER TO JOB CARDS 26C2612SDR REXA2026033100278Skin · chafedFUSELAGE OUTER SKIN IS CHAFED AT FS 913.00 STGR 27. REPAIRED FUSELAGE LOWER SKIN IAW MHIRJ REO 690-53-00-651 REV -- DATED 2026-03-2023 AND BOMBARDIER REO 670-53-00-290 REV F DATED 2019/04/26.SDR SWAA2026033182438Battery · inoperativeEMERGENCY BATTERY PACK REQUIRES REPLACEMENT. REMOVED, REPLACED AND PERFORMED AND GOOD CHECK OF M1673 BATTERY IAW SWA B737 MAX 8 AMM 33-51-06;[02] REMOVED; REPLACED AND PERFORMED AND GOOD CHECK OF M1673 BATTERY IAW SWA B737 MAX 8 AMM 33-51-06. VERIFIED ALLL GSDR CALA2026033014920Paint · missingDURING INSPECTION FOUND MISSING PAINT ON NOSE RADOME. DURING PHASE 2 INSPECTION FOR LIGHTNING STRIKE. FOUND MISSING PAINT ON RADOME MEASURING APPROX. 1 SQ INCH. NO STRUCTURAL DAMAGE FOUND. APPLIED CLEAR TAPE TO EXPOSED AREA PER EC/RA 5350-02074. ACCOMPLISH ASDR CALA2026033014893Floorbeam · corrodedFLIGHT DECK FLOOR SUPPORT UPPER SURFACE CORROSION BS 270 BETWEEN LBL 10" TO RBL 10" REF AAR N/R 100003259 INSTALLED REPAIR ANGLE AND REPAIR STRAP AT FLIGHT DECK FLOOR SUPPORT UPPER STA 270 REF B737-800 SRM 51-40-02-0G-0 & ECRA 5321-01566. INSTALLED REPAIR ASDR 2DYA202603230006Battery Pack · inoperativeDURING POST FLT CHECK 4 OVERHEAD EMERGENCY AISLE LIGHTS DID NOT TEST. APPLIED MEL 33-51-01-CAT "C" EXP.2-APR-26 DMI# 771-26-0052. 23-APR-26 LP 43474. DURING TROUBLE SHOOTING FOUND CANNON PLUG LOOSE AT BATTERY. RE-SECURED CANNON PLUG. OPS CHECKED GOOD. 28-MAR-2SDR 8HBR20260329078Bearing · brinelledPILOTS EXPERIENCED ERRATIC CYCLIC MOVEMENT. UPON INSPECTION IT WAS FOUND THAT THE SPINDLE BEARINGS IN ONE MAIN ROTOR BLADE WERE BRINELLED.SDR 2DYA202603150006Battery Pack · inoperativeFME REPORTED EMERGENCY OVER HEAD LIGHTS BETWEEN ROW 20-30 INOP ON L SIDE. XFERRED TO MEL 33-51-01 CAT "C" EXP. 2-APR-26 DMI# 771- 26-0052..23 MAR-26 LP 43474.T/S ON GOING.SDR SWAA2026032782412Engine · faultyON TAKEOFF, JUST AFTER TOGO WAS PUSHED AIRPLANE WAS PULLING TO THE RIGHT. REJECTED THE TAKEOFF, IT WAS BELOW 45 KTS. TAXI BACK TO THE GATE. PERFORM A TOGA BITE CHECK, OPS CHECKED GOOD, CHECKED NOSE STEERING CABLES TENSION IAW AMM 32-50-00. LOW SPEED TAXI,SDR AALA202603276348Insulation · soiledAIRCRAFT WAS NOT GROUNDED: REPEATED ISSUES WITH DURING CRUISE PASSENGERS COMPLAINING OF STRONG ODOR COMING FROM BUSINESS CLASS AREA. FLIGHT ATTENDANT REPORT ODOR SMELLS LIKE TRASH DUMPSTER COMING FROM NEAR CARPET BY SEATS 1DF. REPLACED DRAIN "T" TUBE IN ELECTSDR AALA202603279349Drain Line · tornAIRCRAFT WAS NOT GROUNDED: REPEATED ISSUES WITH DURING CRUISE PASSENGERS COMPLAINING OF STRONG ODOR COMING FROM BUSINESS CLASS AREA. FLIGHT ATTENDANT REPORT ODOR SMELLS LIKE TRASH DUMPSTER COMING FROM NEAR CARPET BY SEATS 1DF. REPLACED DRAIN "T" TUBE IN ELECTSDR AALA202603275592Drain Line · collapsedAIRCRAFT WAS NOT GROUNDED: REPEATED ISSUES WITH DURING CRUISE PASSENGERS COMPLAINING OF STRONG ODOR COMING FROM BUSINESS CLASS AREA. FLIGHT ATTENDANT REPORT ODOR SMELLS LIKE TRASH DUMPSTER COMING FROM NEAR CARPET BY SEATS 1DF. REPLACED DRAIN "T" TUBE IN ELECTSDR AALA202603270681Engine · failedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: LEVELING OFF AT FL310 NUMBER 1 ENGINE N1 DIPPED AND SURGED AT LEAST 3 TIMES. THIS WAS ACCOMPANIED BY A BANGING NOISE HEARD IN THE COCKTAIL. FLIGHT ATTENDANT REPORTED SEEING SPARKS COMING FROM THE NUMBER SDR AALA202603276981Tube · cloggedAIRCRAFT WAS NOT GROUNDED: REPEATED ISSUES WITH DURING CRUISE PASSENGERS COMPLAINING OF STRONG ODOR COMING FROM BUSINESS CLASS AREA. FLIGHT ATTENDANT REPORT ODOR SMELLS LIKE TRASH DUMPSTER COMING FROM NEAR CARPET BY SEATS 1DF. REPLACED DRAIN "T" TUBE IN ELECTSDR DALA2026032702041Sensor · faultedRIGHT AFT ENTRY DOOR MSG AND LIGHT CLIMBING THRU 7000 FT. R & R R4 ENTRY DOOR WARNING SENSOR PER AMM 52-71. (8394626)SDR AALA202603272567Solenoid Valve · leakingAIRCRAFT WAS GROUNDED: SOF EVENT. SMELL WAS REPORTED BY CABIN CREW AS BURNT RUBBER OR VERY HOT PLASTIC. MILD ODORS WERE NOTED FOLLOWING TAKEOFF BUT WERE NOT OBTRUSIVE OR IMPAIRING AND APPEARED TO DISSIPATE. THE ODOR RETURNED ON DECENT. MAINTENANCE REPLACED ASDR GTIA2026032639321Oil System · overservicedFLIGHT ATTENDANT REPORTED AN ODOR OF HUMIDITY & VOMIT, ODOR IN FRONT & AFT CABIN ON FINAL APPROACH, ABOUT 2,000 FT. FOUND APU OVERSERVICED DURING INSPECTION OF THE APU UPON ODOR IN THE CABIN IAW TSM 05-50-00-810-831-A, & AMM 49-00-00-200-811-A , DRAINED APU