Service difficulty reports
1,770,704 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 CALA2026081418621Frame · crackedFRAME 68, STRINGER 22R INNER CAP AND WEB FLANGE HAD A CRACK INDICATION, 5CM LONG AT 100% SH. PERFORMED REPAIR ON INNER CAP IAW EC/RA 5341-01580.SDR CALA2026081418619Rib · crackedRIGHT HORIZONTAL STAB L/E RIB AT HSS 281 AFT SECTION HAD EVIDENCE OF A CRACK. REMOVED AND REPLACED RT HORIZONTAL STAB L/E RIB IAW SRM 51-40-02-0G-0 AND DWG 186A1001.SDR CALA2026081418617Rib · crackedLEFT HORIZONTAL STAB. LEADING EDGE INTERNAL RIB AT HSS 95 HAD EVIDENCE OF A CRACK. REMOVED AND REPLACED LT HORIZONTAL STAB L/E INTERNAL RIB IAW SRM 51-40-02-0G-0 AND DRAWING 186A1001.SDR CALA2026081418615Battery Pack · faultedEMERGENCY LIGHT BATTERY PACK M1676 HAS LOW VOLTAGE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1676. OPS CHKD GOOD IAW AMM 33-51-06-960-805.SDR CALA2026081418613Battery Pack · faultedEMERGENCY LIGHT BATTERY PACK M1670 HAS LOW VOLTAGE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1670. OPS CHKD IAW AMM 33-51-06-960-805.SDR CALA2026081418611Battery Pack · faultedEMERGENCY LIGHT BATTERY PACK M1695 HAS LOW VOLTAGE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1695 AND OPS CHKD GOOD IAW AMM 33-51-06-960-805.SDR CALA2026081418609Battery Pack · faultedEMERGENCY LIGHT BATTERY PACK M2335 HAS LOW VOLTAGE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M2335 AND OPS CHKD GOOD IAW AMM 33-51-06-960-805.SDR CALA2026081418607Battery Pack · faultedEMERGENCY LIGHT BATTERY PACK M1694 HAS LOW VOLTAGE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1694 AND OPS CHECKED GOOD IAW AMM 33-51-06-960-805.SDR CALA2026081418605Battery Pack · faultedEMERGENCY LIGHT BATTERY PACK M1671 HAS LOW VOLTAGE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND OPS CHKD GOOD IAW AMM 33-51-06-960-805.SDR CALA2026081418603Rib · crackedRIGHT HORIZONTAL STAB L/E RIB AT HSS 253.73 AFT SECTION EVIDENCE OF CRACK. REMOVED AND REPLACED RIGHT HORIZONTAL STAB L/E RIB AT STA 253.73 IAW SRM 51-40-02-0G-0 AND DWG 186A1001.SDR CALA2026081418601Rib · crackedRIGHT HORIZONTAL STAB L/E RIB AT STA 235 AFT SECTION EVIDENCE OF CRACK. REMOVED AND REPLACED RIGHT HORIZONTAL STAB L/E RIB AT BS 235 IAW SRM 51-40-02-0G-0 AND DWG 186A1001.SDR CALA2026081418599Rib · crackedRIGHT HORIZONTAL STAB L/E RIB AT STA 263.3 AFT SECTION EVIDENCE OF CRACK. REMOVED AND REPLACED RIGHT HORIZONTAL STAB L/E RIB AT STA 263.3 IAW SRM 51-40-02-0G-0 AND DWG 186A1001.SDR CALA2026081418597Acm · seizedAIR RETURN FOR SMOKE/FUMES IN THE COCKPIT. TROUBLESHOOTING COCKPIT SMOKE/ODOR IAW AMM 05-51-26-800-801-C1. NO SMOKE/ODOR DETECTED. LEFT PACK TRIP LIGHT COMES ON SHORTLY AFTER TURNING ON , UNABLE TO TRIP RESET. BURN ODOR COMING FROM LT PACK BAY. PERFORMED PASDR CALA2026081418595Coffeemaker · faultedFOUND AFT COFFEEMAKER 419 CIRCUIT BREAKER OPEN, CLOSED BREAKER & COFFEEMAKER PRODUCED A POP WITH BRIEF FLAME AND SMOKE. CIRCUIT BREAKER TRIPPED OPEN AGAIN. REPLACED THE COFFEEMAKER IN THE AFT GALLEY, CLOSED CIRCUIT BREAKER, OPS CHKD GOOD. PERFORMED INSP. FSDR FE6R202608130001Feeder Cable · meltedPILOTS REPORTED GENERATOR NO.1 FAIL IN FLIGHT APPROXIMATELY 10 MINUTES AFTER TAKEOFF AND RETURNED TO THE FIELD, UNEVENTFUL LANDING. NO.1 ENGINE DRIVEN GENERATOR FEEDER CABLE PASS-THROUGH IN LH PYLON WAS FOUND MELTED. DAMAGE FOUND ON POSITIVE AND NEGATIVE FEEDESDR IXXA20260813001Bushing · damagedLATCH RECIEVER BUSHINGS ON NR 1 PYLON INBD SIDE HAVE BEEN OVERSIZED.SDR 2026FA0000638Feeder Cable · meltedPILOTS REPORTED GENERATOR NO. 1 FAIL IN FLIGHT APPROX. 10 MINUTES AFTER TAKEOFF AND RETURNED TO THE FIELD, UNEVENTFUL LANDING. NO. 1 ENGINE DRIVEN GENERATOR FEEDER CABLE PASS-THROUGH IN LH PYLON WAS FOUND MELTED. DAMAGE FOUND ON POSITIVE AND NEGATIVE FEEDER CASDR FDEA202608131118Floorbeam · corrodedMAIN CABIN FLOORBEAM AT BS 1200 BETWEEN BL 0 TO LBL 24.75 WITH CORROSION FLOORBEAM SECTION OUT OF LIMITS AT MAIN CABIN B.S 1200 BETWEEN LBL 5 TO LBL 11 WAS REPAIRED IAW B-757 SRM 53-00-51-2R FIG 201 REPAIR 5.SDR QR9R2026081300002Actuator · failedYAW ACTUATOR CAUTION ILLUMINATED IN FLIGHT. MALFUNCTION WAS INDICATED ON THE CAD ONLY. LOWER YAW TRIM LIGHT DID NOT ILLUMINATE. DURING TROUBLESHOOTING, FOUND YAW SEMA BAD, ALSO HAD CODE YAWEMA INVAL. REMOVED AND REPLACED SEMA ACTUATOR IAW AMM 67-20-00, 4-14.SDR QR9R2026081300001Cable · bindingNEW #1 ENGINE N2 CABLE RECEIVED IS BINDING SITTING IN RESTING POSITION AND GETS WORSE AS CABLE IS BENT INTO SIMILAR SHAPE OF IT BEING INSTALLED ON AIRCRAFT. REPLACED #1 ENGINE N2 CABLE IAW 76-12-00, 4-8.SDR DALA2026081304646Battery Pack · inoperativeFOUND EMERGENCY LIGHTS AT SEATS 3,4,10,17,18,21,22. REPLACED 15WL EPSU AND BATTERY PER AMM 33-51-38. OPS CHECK GOOD. (LP 8652914 - AIRCRAFT WAS GROUNDED)SDR 2026F00175Igniter · burnedIGNITORS BURN THROUGH TO ELECTRICAL LEAD WITHIN 100 HOURS OF USE. HOT TURBINE COMBUSTION GASES ESCAPE THROUGH IGNITOR BODY TO BURN CONNECTION AND IGITOR LEAD. LEAD SEIZES IN PLACE AND CANNOT BE REMOVED WITHOUT BEING DESTROYED. IGNITOR FAILS, IGNITION LEAD SDR JR2R20260813162Angle · corrodedAFT CABIN ANGLE THAT ATTACHES TO INTERCOSTAL AT LBL11 BETWEEN FR90 - FR90A IS CORRODED. REPLACESDR JR2R20260813153Shear Panel · corrodedAFT CABIN RH SHEAR PANEL SPLICE DOUBLER AT RBL40 BETWEEN FR87 - FR88 IS CORRODED. REPLACESDR JR2R20260813159Beam · corrodedAFT CABIN EXISTING DOUBLER REPAIR ON LONG BEAM AT LBL11 BETWEEN FR 86 - 88 CORRODED. REPAIREDSDR QMLA2026081320055Blower Motor · burned outODOR OF BURNT ELECTRICAL WIRING. FOUND SMELL COMING FROM AFT AC VENTS. FOUND CONDENSATION/WATER IN ELECTRICAL MOTOR. REPLACED AFT BLOWER MOTORSDR JR2R20260813157Seat Track · corrodedAFT CABIN EXISTING DOUBLER REPAIR AT FR84 LBL11 SEAT TRACK END IS CORRODED. REPAIRSDR JR2R20260813155Sill Drain · corrodedAFT CABIN LH MOP SILL AT FR84 LBL40 CORRODED. REPLACEDSDR 2026F00174Indicator · overheatedAIRCRAFT WAS OPERATING A PART 135 FLIGHT FROM KABI TO KDFW. DURING CRUISE FLIGHT AT APPROX 7,000 FT MSL NEAR THE BOOVE WAYPOINT, THE PILOT DETECTED AN ODOR CONSISTENT WITH SOMETHING BURNING. PILOT CLOSED CABIN VENTS TO DETERMINE WHETHER THE ODOR ORIGINATED WITSDR JR2R20260813858Skin · chafedLH WING LEADING EDGE PANEL ABOVE PYLON CHAFED. REPAIRSDR JR2R20260813859Skin · chafedRH WING LEADING EDGE PANEL ABOVE PYLON CHAFED. REPAIRSDR JR2R2026081114Skin · chafedRIGHT WING LEADING EDGE PANEL ABOVE PYLON CHAFED. REPAIRSDR 2026FA0000637Servo · faultedPILOT REPORTED THE FUEL PRESSURE PEGGED MAX PRESSURE CAUSING THE GAUGE TO BECOME INOP. IT WAS REPLACED AND AGAIN THE GAUGE WENT TO MAX & BECAME INOP, THE FUEL FLOW AT FULL THROTTLE NOW EXCEEDS 30GPH INDICATED WHERE IT USED TO BE 28GPH & ALL THE CYLINDER HEAD TSDR 2A6D20260813002Rib · chafedCHAFE DAMAGE ON BL 1263 RIB ON RH SIDE OF HORIZONTAL STABILIZER.SDR 2A6D20260813001Crossbeam · chafedGOUGE/CHAFE DAMAGE TO THE AFT LANDING GEAR ATTACHMENT FWD CROSSBEAM AND SUPPORT ANGLE.SDR SWIA2026081277826Drag Angle · crackedVERTICAL STAB, RT AFT DRAG ANGLE HAD SIGNS OF A CRACK. REPAIR PERFORMED ON THE RT AFT DRAG ANGLE AT VERTICAL STAB IAW REO 670-55-31-018, REV-A, & SRM 51-26-01. NDT PERFORMED.SDR SWIA2026081277821Drag Angle · crackedVERTICAL STAB LH AFT DRAG ANGLE SIGNS OF CRACK. REPAIR PERFORMED LT AFT DRAG ANGLE AT VERTICAL STAB IAW BOMBARDIER REO 670-55-31-018 REV-A, SRM 51-26-01,SDR IPXA2026102654575Bracket · corrodedMAIN DECK FLOOR STRUCTURE, THRUST BRACKET BETWEEN -Y2462 & -Y1959 AND FR 29 & 28 HAS CORROSION. VERIFIED EWIS PROTECTION REMOVED PER ESPM PGBLK 20-54-50-02.SDR IPXA2026102654515Bracket · corrodedMAIN DECK FLOOR STRUCTURE, THRUST BRACKET BETWEEN -Y2462 & -Y1959 AND FR 30 & 29 HAS CORROSION. VERIFIED EWIS PROTECTION REMOVED PER ESPM PGBLK 20-54-50-02.SDR IPXA2026082154648Seat Track · corrodedMAJOR REPAIR, MDC FLOOR, BTW FR 27 AND 29, Y1456, SEAT TRACK WITH CORROSION AT BOTH SIDES. INSTALLED A NEW SEAT TRACK, EXISTING 4 SPLICES, 6 CONECTION ANGLE AND 12 CLIPSDR IPXA2026091637023Gutter · corrodedAFT CARGO COMP. FLOOR PANEL DRAINAGE PLATE HAS NUMEROUS CORROSIONS (7 SPOTS) IN THE BACK SIDE AT FR.65/. REMOVED AND REPLACED FLOOR PANEL DRAINAGE PLATE AT ZONE 100-STR- AFT CARGO SIDE AT FR.65 AFT CARGO COMP. I.A.W A300-600 AMM 25-55-80/201 AND AIPC 25-55-81SDR IPXA2026100654735Adapter · corrodedMAIN DECK FLOOR STRUCTURE, CLS AT FR 30 BETWEEN Y0 & -Y450 HAS CORROSION. INSTALLED NEW CLS ADAPTER FR30, BTW Y0 AND -Y450 IAW SRM 51-40-21.SDR IPXA2026100654025Adapter · corrodedMDC, CLS AT FR36, BTW Y0 AND Y450 IS CORRODED. VERIFIED INSTALLATION OF NEW CLS ADAPTER AT FR36 BTW Y0 AND Y450 IAW SRM 51-40-21-001.SDR IPXA2026100654726Floorbeam · corrodedMAIN DECK FLOOR STRUCTURE, CLS AT FR 34 BETWEEN Y0 & -Y450 HAS CORROSION INSTALLED NEW CLS ADAPTER P/N UP-B53774136200 IAW A300-600 SRM 51-40-21-001.SDR IPXA2026100654057Adapter · corrodedMDC, CLS AT FR34, BTW Y0 AND Y450 IS CORRODED. VERIFIED INSTALLATION OF NEW CLS ADAPTER AT FR34, BTW Y0 AND Y450 IAW SRM 51-40-21-001.SDR IPXA2026100654048Adapter · corrodedMDC, CLS AT FR35, BTW Y0 AND Y450 IS CORRODED. VERIFIED INSTALLATION OF NEW CLS ADAPTER A TFR35 BTW Y0 AND Y450 IAW SRM 51-40-21-001.SDR IPXA2026100653905Adapter · corrodedMDC, CLS ADAPTER AT FR38.1, BTW Y0 AND Y450 IS EXFOLIATED. VERIFIED INSTALLATION OF NEW CLS ADAPTER AT FR38.1, BTW Y0 AND Y450 IAW SRM 51-40-21-001.SDR IPXA2026100652275Adapter · corrodedMAIN DECK, RH FR35, Y0 CLS ADAPTER HAS CORROSION IN 2EA SPOTS. VERIFIED INSTALLATION OF NEW CLS ADAPTER AT RH FR35, Y0 IAW A300- SRM 51-40-21-001SDR IPXA2026100652219Adapter · corrodedMAIN DECK, RH FR38.1, Y0 CLS ADAPTER IS DAMAGED, VERIFIED INSTALLATION OF NEW CLS ADAPTER AT RH FR38.1 Y0 IAW SRM 51-40-21-001.SDR IPXA2026082154325Seat Track · corrodedMAJOR REPAIR, MDC SEAT TRACK, BTWN FR 30 - 31, Y450, HAD 2 SPOTS OF CORROSION AT L/H LATERAL FACE. REPAIRED IAW SRM 53-10-16-16-201, PAGE207 & 208, FIG 201,REV 43.