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 CALA2026081218514Access Panel · misinstalledFUEL LEAK FROM LT WING SURGE TANK DOOR ASSY, PRESSURE RELIEF VALVE ACCESS PANEL LEAKING FUEL. SUMPED SURGE TANK VIA PIDDLE DRAIN, REMOVED ACCESS PANEL 542AB DUE TO VISIBLE FUEL LEAK. PANEL REMOVED IAW AMM 28-11-01-004-013, AND REF ECRA 2810-10336. FOUND SDR CALA2026081218512Support Bracket · crackedLEFT MLG WHEEL WELL, AFT BULKHEAD BS 1180 LOWER SECTION LBL12, SUPPORT BRACKET CRACKED. REMOVED AND REPLACED CHANNEL ON LT MLG WHEEL WELL AFT BULKHEAD IAW SRM 51-90-02-0G-0 AND DWG 199N2503.SDR CALA2026081218510Support Bracket · crackedRIGHT MLG WHEEL WELL, AFT BULKHEAD BS 1180 LOWER SECTION, RBL 12, SUPPORT BRACKET CRACKED. REMOVED AND REPLACED THE CHANNEL IAW SRM 51-40-02-OG-0, AND DWG 144N 2503.SDR DALA2026081104626Power Supply · inoperativeFOUND AFT BULKHEAD DOOR EMERGENCY LIGHT INOPERATIVE. R & R AFT CENTER EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW AMM 33-51. CHECKS GOOD. OK FOR SVC.SDR QR9R2026081100001Sensor · failedOVSP SYSTEM 1 FAILED DURING START RUN-UP. MAINTENANCE ARRIVED AND PULLED CB AND CAUTION LIGHT WAS STILL ILLUMINATED AFTER RESETTING CB. DURING TROUBLESHOOTING, FOUND #1 ENGINE OVERSPEED SENSOR BAD. PINS 1-2 OP AND PINS 4-5 HIGH RESISTANCE. REMOVED AND REPLACEDSDR JR2R20250811132Skin · gougedFWD AVIONICS DOOR EXTERNAL SKIN HAS SEVERAL GOUGES AT L/H SIDE OF VENT FLAP OUT OF LIMITS. REPAIREDSDR IPXA2026081116362Bleed Air Sys · odorUPON TURNING ON APU BLEED AIR, NOTICED A STRONG FUEL ODOR COMING OUT OF THE VENTILATION AREAS IN COCKPIT AND SUPERNUMARY COMPARTMENT. T/S AND FOUND TORQUE MOTOR ON APU FUEL CONTROL LEAKING FUEL INTO THE APU INTAKE. R/R TORQUE MOTOR SEAL PER CMM 49-31-61. OPS ASDR 2026FA0000636Pivot Assy · shearedLEFT MAIN LANDING GEAR COLLAPSED AFTER LANDING, THEN ROLLING OUT 2000' AT THE START OF A RIGHT TURN ONTO A TAXIWAY. WHEN AIRCRAFT WAS JACKED FOR TESTING, THE GEAR WOULD RELEASE FROM EITHER THE UP/LOCKED OR DOWN/LOCKED POSITION BUT WOULD NOT CONTINUE TO THE POSSDR F3LA202608110444Power Supply · failedDISCREPANCY: OCCURED DURING A RON MAINTENANCE VISIT, NO FLIGHT DELAY. REFERENCE LP704938 ITEM 3, PERFORMED EPSU TEST AND FOUND 12WL BATTERY FAILED. REMOVED AND REPLACED THE BATTERY ON 12WL PER AMM REF. 33-51-38-400-002-A. PERFORMED EPSU TEST AGAIN. TEST PASSSDR AALA202608112139Battery · no testAIRCRAFT WAS NOT GROUNDED: BATTERY FAULT FOR EMERGENCY POWER SUPPLY UNIT 11WL DISPLAYED DURING SYSTEM TEST - MAINTENANCE REPLACED THE BATTERY FOR EMERGENCY POWER SUPPLY UNIT 11WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECKSDR KCSA202608111194Battery Pack · dischargedL/H SIDE UPPER DECK DOOR BATTERY HAS LOW VOLTAGESDR KCSA202608111193Battery Pack · no testEMERGENCY LIGHT POWER SUPPLY AT APPROX STA 830 BEHIND GALLEY FAILS OPS CHECKEDSDR KCSA202608111192Stringer · corrodedCORROSION FOUND AT BS 1965 ON STRINGER 51R.SDR KCSA202608111191Stringer · corrodedPOSSIBLE CORROSION ON S-48L IN AFT CARGO AT BS 1920-1940SDR KCSA202608111190Stringer · corrodedPOSSIBLE CORROSION ON S-49L IN AFT CARGO AT STA 1860-1880.SDR KCSA202608111189Floor Support · corrodedUNDER SIDE OF PANEL SUPPORT HAS CORROSION IN AFT BULK CARGO COMPARTMENT APPROX STA 2160 RBL 12SDR IXXA20260811002Duct · crackedINBD CORE COWL EXHAUST DUCT IS CHAFED ON THE LEADING EDGESDR IXXA20260811001Frame · gougedPANEL 573BB AFT FRAME IS SEVERELY GOUGEDSDR KCSA202608111188Floorbeam · corrodedUNDERSIDE OF FLOOR PANEL SUPPORT HAS CORROSION IN AFT BULK CARGO COMPARTMENT APPROX STA 2160 LBL 5-12SDR KCSA202608111187Floor Support · corrodedUNDER SIDE OF PANEL SUPPORT HAS CORROSION IN AFT BULK CARGO COMPARTMENT APPROX STA 2160 RBL 38-48SDR KCSA202608111186Stiffener · corrodedEVIDENCE OF CORROSION ON R/H WING IN L/E CAVITY ON FWD SPAR STIFFENER APPROX WS 1513SDR KCSA202608111185Seat Track · corrodedUPPER DECK SEAT TRACK CORRODED AT STA 720 LBL 24SDR KCSA202608111184Seat Track · corrodedUPPER DECK SEAT TRACK FOUND TO BE CORRODED AT STA 720-780 LBL 30SDR KCSA202608111183Tension Tie · crackedINNER FRAME DOUBLER CRACKED AT STA 1160 R/HSDR KCSA202608111182Tension Tie · cracked2 EACH CRACK INDICATIONS IN FASTENER HOLES IN THE FRAME COMMON TO THE TENSION TIE AT STA 1160 R/H SIDESDR FDEA202608111112Rivet · looseRIGHT WING INBD FLAP UPPER SKIN, FOUND SEVERAL RIVETS LOOSE AT XIFH 276.36. RT WING INBOARD FLAP UPPER SKIN LOOSE RIVETS AT XIFH 276.36 CARRIED OUT REPAIR AS PER EA 1-5750-T0308240 B P2. REPAIR CLASSIFIED AS MAJOR, IAW GMM 6-2-100.SDR FDEA202608111108Floor Panel · puncturedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251UFF HAS PUNCTURE DAMAGE. FLOOR PANEL REPAIRED IAW SRM 53-00-50-2R, FIG 201, SHEET 1. MAJOR REPAIR.SDR KCSA202608111181Floorbeam · corrodedFLIGHT DECK FLOORBEAM UPPER SURFACE CORRODED AT WEB SEAM BS 330 LBL 41 TO RBL 41.SDR KCSA202608111180Panel · crackedL/H CANTED PRESSURE DECK COMPOSITE PANEL STA 1240 LBL 70-80 DAMAGEDSDR KCSA202608111179Stringer · crackedUPPER DECK R/H SIDE STRINGER 8R UPPER SURFACE HAS POSSIBLE CRACK BY HILOK FASTENER JUST FWD OF BODY FRAME 460SDR KCSA202608111178Splice Plate · corrodedEVIDENCE OF CORROSION ON RT WING IN L/E CAVITY APPROX WS 1454 TWO INCHES FWD OF FRONT SPARSDR KCSA202608111177Stringer · corrodedPOSSIBLE CORROSION ON STRINGER 48L IN AFT CARGO AT BS 1920-1940.SDR JR2R20260811149Sill Drain · corrodedAFT CABIN RT MOP SILL AT FR84 RBL40 IS CORRODED. REPLACEDSDR KCSA202608111176Stringer · corrodedPOSSIBLE CORROSION ON STRINGER 49L IN AFT CARGO AT BS 1860 - 1880.SDR JR2R20260811158Strap · corrodedAFT CABIN UPPER STRAP AT LBL11 BETWEEN FR 85 - 86 IS CORRODED. REPLACED.SDR JR2R20260811152Floor Support · crackedAFT CABIN FLOOR SUPPORT BRACKET AT FR 86, RBL 24 IS CRACKED. REPLACED.SDR JR2R20260811166Angle · crackedFLIGHDECK UNDER FLOOR AT FR12 BL0 ANGLE CLIP CRACKED. REPLACED.SDR KCSA202608111175Seat Track · corrodedUPPER DECK SEAT TRACK APPROX RBL 40 STA 450 HAS EVIDENCE OF CORROSIONSDR JR2R20260811163Doubler · corrodedFWD CABIN FLOOR DOUBLER AT RBL36 BETWEEN FR12 - FR14 CORRODED. REPLACEDSDR CALA2026081118469Threshold · dentedRAMP REPORTED AFT CARGO BIN THRESHOLD HAS A DENT. DENT IS LOCATED AT CENTER BULLNOSE MEASURES 1.5" W, Y=.150" W/Y=10 & IS OUT OF LIMITS IAW SRM 53-60-15-1A-1, FIG 103, DETAIL H. PERFORMED INTERIM REPAIR IAW ECRA 5310-04013, REV. J. INSPECTED INTERIM REPAIR PSDR SWIA2026081077822Attach Angle · crackedPAX DOOR AFT DRAG ANGLE SIGNS OF CRACK AT FS34725 NEAR INTERCOSTAL DD3. PERFORMED REPAIR PAX DOOR AFT DRAG ANGLE AT FS34725 NEAR INTERCOSTAL DD3 IAW SRM 52-11-04, 51-21-11, 51-25-06, 51-25-16, 51-42-13, 51-42-06, & 51-42-22SDR IPXA2026102312775Structure · crackedPYLON #1, TOP SECTION AT RIB 3A, EXTERNAL SURFACE IS CRACKED AND HAS TWO DAMAGED RIVETS.SDR IPXA2026102314263Fan Cowl · damagedLEFT ENG I/B FAN COWL AFT HINGE FWD LUG HAS DAMAGED.SDR HNAA2026092200883Skin · corrodedRT INLET HAS PITTING ON LIP SKIN. R/H INLET REMOVED AND REPLACED ON WO# H10452 S/N 00912 QUANTUM# 4600.SDR REXA2026092101861Plate · worn"WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES FLAP FITTING (2EAS) AND PLATE SUPPORT (2EAS) OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01,SRM 51-42-SDR REXA2026092101860Plate · worn"WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES FLAP FITTING (2EAS) AND PLATE SUPPORT (2EAS) OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01,SRM 51-42-SDR REXA2026092101859Fitting · worn"WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES FLAP FITTING (2EAS) AND PLATE SUPPORT (2EAS) OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01,SRM 51-42-SDR REXA2026092101858Fitting · worn"WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES FLAP FITTING (2EAS) AND PLATE SUPPORT (2EAS) OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01,SRM 51-42-SDR REXA2026092101842Web · corrodedWEAR AND CORROSION ON SETTLEMENT AREAS (4 LOCATIONS) OF MLG BINS AT LH/RH WHEEL WELL AREA MACHINED WEB LH ON MLG BINS AT LH WHEEL WELL AREA P/N CC670-39221-3 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-21-001-001-A01.SDR REXA2026092101841Angle · corrodedWEAR AND CORROSION ON SETTLEMENT AREAS (4 LOCATIONS) OF MLG BINS AT LH/RH WHEEL WELL AREA ANGLE PN: (SH670-36386-16) WAS REPLACED PER CRJ 900 SRM 51-42-10-001-001-A01.