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 SWAA2026072999375Seal · out of adjustLEFT UPPER STAB PANEL 333AT SLIDING SEAL NOT IN GUIDE. INSTALLED 333AT IAW SRM 51-40-02, REF IPC 55-10-52.SDR UIEA2026072400646Generator · faultedCREW SET UP IAW DDG 49-11-01. CREW ISOLATED THAT LT PNEUMATIC & RT UTILITY. CREW STARTED NR 4 ENG. DURING START, AT THE TIME, NR 4 ENG GOING TO TAKE OVER POWER BY GEN FROM ENGINE. THE ACFT STARTED TO SHED LOAD POWER. THEN LT SIDE WHICH IS POWERED BY LT EXT POSDR YENA2026072700625Elec Connector · damagedFLT # 354, DUB-BOS. (ETOPS) "CONNECTORS J4 J6 J14 ON ENG # 2 EEC AND PHMU J10 REMOVED FPR W03 HARNESS REPLACEMENT.; INSTALLED CONNECTORS J4 J6 J14 J10 ON ENG#2 EEC AND PHMU IAW AMM 77-31-01, 73-21-01.SDR CALA2026072918088Engine · vibration2 ENGINE VIB 4.0SDR DALA2026072804385Oxygen Mask · unwanted deployFWD LAV O2 MASK DEPLOYED IN FLIGHT. REPACKED OXYGEN MASK ASSY IAW AMM 35-21 PROCEDURES. OK FOR SVC. (LP: 9583816, AIRCRAFT WAS GROUNDED)SDR DALA2026072804384Fitting · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPLACEMENT CENTER WINDOW FRAMES AND CONTINUITY FITTINGS PER ER/A 635072-14AD. SECTION I IS LIMITED TO 60000 TOTAL AIRCRAFT FLIGHT CYCLES. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE ASSSDR SWAA2026072889051Fire Detector · false activationNR 2 ENGINE OVERHEAT LIGHT ILLUMINATED ON START. R & R NR 2 ENGINE FAN UPPER FIRE DETECTOR, ENGINE FAN LOWER FIRE DETECTOR, ENGINE CORE RT FIRE DETECTOR, AND ENGINE CORE LT FIRE DETECTOR IAW AMM 26-11-01. PREFORMED NR 2 ENGINE IDLE RUN, ENGINE RUN GOOD, SDR SWAA2026072805125Fire Detector · false activationNR 2 ENGINE OVERHEAT LIGHT ILLUMINATED ON START. R & R NR 2 ENGINE FAN UPPER DETECTOR FIRE, ENGINE FAN LOWER DETECTOR FIRE, ENGINE CORE RT FIRE DETECTOR, AND ENGINE CORE LT FIRE DETECTOR IAW AMM 26-11-01. PREFORMED NR 2 ENGINE IDLE RUN, ENGINE RUN GOOD, SDR SWAA2026072854375Slide · dislodgedL1 SLIDE FELL OUT OF BUSTLE. REPACKED FWD ENTRY EMERGENCY SLIDE REF MT 72561-06.SDR SWAA2026072881565Fire Detector · false activationNR 2 ENGINE OVERHEAT LIGHT ILLUMINATED ON START. R & R NR 2 ENGINE FAN UPPER DETECTOR FIRE ENGINE FAN LOWER DETECTOR FIRE ENGINE CORE RIGHT FIRE DETECTOR AND ENGINE CORE LEFT FIRE DETECTOR IAW AMM 26-11-01. PREFORMED NR 2 ENGINE IDLE RUN ENGINE, RUN GOOD, NOSDR SWAA2026072855851Compensator · leakingINFLIGHT, NR 2 FUEL IMBALANCE CLIMBING THROUGH FL 250, NOTICED NR 2 FUEL QTY DECREASE BELOW NR 1 ENGINE QTY. FUEL IMBALANCE WAS GREATER THAN 3,000 LBS. CREW RAN QRH & SHUTDOWN THE ENGINE. UPON ACFT REACHING THE GATE, INSPECTED FOR OBVIOUS SIGNS OF A FUEL LEAKSDR SWAA2026072864092Fire Detector · illuminated#2 ENGINE OVERHEAT LIGHT ILLUMINATED ON START_ REMOVED AND REPLACED NR 2 ENGINE FAN UPPER DETECTOR FIRE DETECTOR IAW AMM 26-11-01. PREFORMED NR 2 ENGINE IDLE RUN ENGINE RUN GOOD, NO FAULTS OR INDICATIONS FOUND. ENGINE RUN NORMAL IAW AMM 71-00-00.SDR SWAA2026072884652Lens · looseMID CABIN EMERGENCY EXIT SIGN LENS WILL NOT STAY ATTACHED. SECURED PER M-EA M-24-133-00396SDR SWAA2026072809480Tank Unit · leakingINFLIGHT NR 2 FUEL IMBALANCE CLIMBING THROUGH FL 250, NOTICED NR 2 FUEL QUANITY DECREASE BELOW #1 ENGINE QUANITY. FUEL IMBALANCE WAS GRATER THAN 3,000LBS. CREW RAN QRH AND SHUT DOWN THE ENGINE. UPON A/C REACHING THE GATE INSPECTED A/C FOR OBVIOUS SIGNS OF A FUSDR SWAA2026072847033Tank Unit · leakingINFLIGHT NR 2 FUEL IMBALANCE CLIMBING THROUGH FL 250, NOTICED NR 2 FUEL QTY DECREASE BELOW NR 1 ENGINE QTY. FUEL IMBALANCE WAS GREATER THAN 3,000LBS. CREW RAN QRH & SHUTDOWN ENGINE. UPON A/C REACHING THE GATE INSPECTED A/C FOR OBVIOUS SIGNS OF A FUEL LEAK IN RSDR SWAA2026072841242Lens · missingEXIT SIGN OVERHEAD ISLE MISSING. INSTALLED FWD MIDDLE LENS COVER IAW AMM 33-51-01.SDR SWAA2026072864134Light · inoperativeINTERIOR EMERGENCY AREA LIGHT INOP ROW 14DEF. R & R OF EMERGENCY AISLE LIGHT ASSY IAW AMM 33-51-03. OPS CHECKED GOOD.SDR SWAA2026072828842Tank Unit · leakingINFLIGHT, NR 2 FUEL IMBALANCE CLIMBING THROUGH FL 250, NOTICED NR 2 FUEL QTY DECREASE BELOW NR 1 ENG QTY. FUEL IMBALANCE WAS GREATER THAN 3,000LBS. CREW RAN QRH & SHUTDOWN ENG. ON ACFT REACHING GATE, INSPECTED ACFT FOR OBVIOUS SIGNS OF A FUEL LEAK IAW AMM 28SDR SWAA2026072837576Cover · missingPASSENGER CABIN AFT SERVICE DOOR SLIDE COVER END CAP MISSING. INSTALLED PASSENGER CABIN AFT SERVICE DOOR SLIDE COVER END CAP IAW AMM 25-66-01.SDR SWAA2026072842871Door · crackedLEFT MLG CENTER DOOR CRACKED. REMOVED LT CTR & INNER MLG GEAR DOOR IAW AMM 32-13-11, OK FOR CONTINUED SERVICE IAW CDL 32-10-3XC. REINSTALLED L/H MLG CENTER DOOR IAW AMM 32-13-11 REINSTALLED L/H MLG WING DOOR IAW AMM 32-13-21.SDR DALA2026072804376Fitting · damagedA.A. WORKCARD 2515-01014-02B, LOWER FUSELAGE ELECTRONICS RACK FIN 80VU, RT LOWER LATERAL FITTING WITH MATERIAL BURRED ( OVALIZATION) ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. PERFORMED MAJOR REPAIR ON FWD FUSELAGE EQUIPMENT / RSDR J7SA2026072800496Radio · faultedCREW REPORTS MULTIPLE HSDB FAULTS, GRD SPOILER FAIL CAS, AND YELLOW “X’S” ON ENGINE INSTRUMENTS. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH P/N 011-03177-10 XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THSDR QXEA2026072800169Mau · faultedFLIGHT 2107. ON THRUST REDUCTION FOR LANDING AT APPROX 30 FEET A.G.L. AIRCRAFT STARTED AN UNCOMMANDED ROLL TO THE LEFT. NO SIGNIFICANT CROSSWIND WAS PRESENT DURING LANDING & FLARE. LANDING UNEVENTFUL. REMOVED FROM SERVICE INTERROGATED CMC FOUND FC 32530104NWS,SDR QXEA2026072800168Relay · failedFLIGHT 2117. RECIRC 2 FAN FAILED. PLACED ON MEL 21-24-01A. MEL CLEARED BY CHECKED AND FOUND NO VOLTAGE AT RECIRCULATION FAN 2. REPLACED RELAY K7 IN RIGHT ICC IAW EMBRAER B175 SWPM 20-32-02 PER FIM TASK# 21-24-00-810-802-A. RECIRCULATION AIR SYSTEM OPERATIONASDR VNAA2026072821401Windshield · crackedFO SIDE WINDSHIELD CRACKING, PERFORMED DAMAGE CHECK OF THE FO SIDE WINDSHIELD IAW AMM 56-11-01-210-801-PSA AND FOUND INTERLAYER BUBBLING IN THE TOP OUTBOARD CORNER. DAMAGE IS WITHIN LIMITS. PERFORMED OPS CHECK OF THE RH WINDSHIELD/SIDE WINDOW TEMP CONTROLLER SDR KY7A20260724001Relay · faultedFLIGHT IDLE UNLOCKS NOT RELEASING UPON TOUCHDOWN AND NO LIGHT ILLUMINATION. R&R RELAY 204 & 205 IAW EMB120 76-10-00 RTS CK C/WSDR FDEA202607241029Floor Panel · puncturedTWO PUNCTURES ON FLOOR PANEL 231FFF ON MAIN DECK CARGO COMPARTMENT. FLOOR PANEL 231FFF ON MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG.201 SHEET 2 PAR 4.B REV.94 DEC 15/2025SDR FDEA202607241028Floor Panel · crackedFOUR CRACKS ON FLOOR PANEL 242SFF ON MAIN DECK CARGO COMPARTMENT. FLOOR PANEL 242SFF ON MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.94 DEC 15/2025SDR FDEA202607241027Floor Panel · crackedPUNCTURE ON FLOOR PANEL 231DFF ON MAIN DECK CARGO COMPARTMENT. FLOOR PANEL 231DFF ON MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG.201 SHEET 2 REV.94 DEC 15/2025SDR KC8A202607240004Fire Warning · false activationAPU FIRE WARNING BEFORE TAKEOFF. VISUALLY CHECKED APU AND AFT COMPARTMENT, NO EVIDENCE OF SMOKE OR FIRE NOTED. FIRE DETECTION SYSTEM CHECKS GOOD PER THE FALCON 20-F5 MM 26-10-00. SUSPECT APU WAS RUNNING DURING TAKEOFF.SDR DALA2026072804354Warning Message · false activationDE/FCNT- DUE T/E FLAP DISAGREE MESSAGE. T/S PER FIM. INSPECTED TORQUE LIMITERS. CHECKED ADJUSTMENT OF FLAP TRANSMITTERS. RAN FLAPS THROUGH SEVERAL CYCLES. SYSTEM OPERATES NORMAL.(9207254)(AIRCRAFT GROUNDED)SDR DALA2026072804351Cam · out of adjustCAM OF THE GIRT BAR MECHANISM DO NOT GO INTO THE SLOT ON THE GIRT BAR SLIDER. ADJUSTMENT THE CAM OF THE GIRT BAR MECHANISM GIRT BAR SLIDER WAS PERFORMED PER B757-300 AMM 52-11- 25 (1717922)(AIRCRAFT GROUNDED)SDR DALA2026072804350None · noneDTA MONITOR INSPECTION LOG REF ERA 635477-14. ASSOCIATED ER/A 00-635477 (1717471)(AIRCRAFT GROUNDED)SDR DALA2026072804349Slide · low pressureFOUND 2L ESCAPE SLIDE PRESSURE LOW OUT OF GREEN BAND. REPLACED 2L DOOR SLIDE PER WC 2566-901-2L. (9127157)(AIRCRAFT GROUND)SDR DALA2026072804347Frame · dentedDENT ON FRAME STA 1440 BTW S-26L TO S-25L AT AFT CARGO COMPARTMENT. REPAIRED PER PRI 635477-14AD REV. 3 AND PER ER/A 635477-14AD (1717896)(AIRCRAFT GROUNDED)SDR DALA2026072804345Frame · crackedMLG WHEEL WELL, LH SIDE, CRACK ON FRAME WEB AT BS 1147, LBL 70, WL 175. REPAIRED PER PRI 635758-14 REV. 3 AND ER/A 63578-14 (1716741)(AIRCRAFT GROUNDED)SDR CALA2026072818062Oven · smokeSMOKE CAME OUT OF OVEN 204. OVEN TURNED OFF. SMOKE FIRE FUMES CHECKLIST PERFORMED. SMOKE DISSIPATED. SYSTEMS RESTORED. FLIGHT CREW SMOKE/ODOR QUESTIONAIRE OVEN 204 IS INOP DO TO SMOKE IN CABINE. OPEN CB, AND INOP DECAL. NOC.APPROVED NEF 2520P INOP OVEN 204 CB SDR CALA2026072718061Engine · no discrepancyLEFT ENGINE BIRD STRIKE. PERFORMED ENG BIRD STRIKE COMPLETED, ENGINE FOREIGN OBJECT DAMAGE AND BIRDSTRIKE INSPECTION IAW AMM 71-00-00-200-802-G00. NO DEFECTS NOTED.SDR CALA2026072718053Web · scratchedE&E COMPARTMENT DOOR CUTOUT LT INTERCOSTAL WEB UPPER AREA AND FASTENER HAS DEEP SCRATCHES. REMOVED, FABRICATED AND REPLACED NEW WEB AT E&E DOOR CUTOUT IAW SRM 53-10-15-1A-3, 51-40-02-0G-0, 53-10-15-0I-3, 51-40-05-0G-0, 51-20-01-0G-0, 51-40-04-0G-0, AMM 20-60SDR CALA2026072718051Oven · smokeOVEN 606 GENERATED HEAVY BLACK SMOKE WHEN OPERATING. REMOVED TRAYS FROM OVEN & CLEARED DEBRIS FROM BOTTOM AND BACK TO PERFORM OPS TEST IAW AMM 25-32-02-200-802-001. WHITE SMOKE CAME OUT WITHIN ONE MINUTE OF STARTING WARMING CYCLE. REMOVED AND REPLACED THE OSDR SWAA2026072705973Engine · failedAT APPOX 30 KTS ON T/O ROLL WITH T/O PWR SET NR 2 ENG FAILED WITH AUDIBLE BANG AND RIGHT SWERVE. PERFORMED RTO. HAD ENG FAILED ON NR 2 EGT DISPLAY. AIRPORT OPS REPORTED DEBRIS BEHIND AIRCRAFT ON RUNWAY. REMOVED AND REPLACED NR 2 ENGINE IAW AMM 71-00-02. PERFSDR I5PA2026072488803Module · faultyAPU INOP. R & R FLOW SENSING MODULE PER AMM, OPS CHECK NORMAL.SDR I5PA2026072488802Controller · faultyFWD CAB TEMP, AFT CAB TEMP, FLT DECK TEMP EICAS MSG. R & R ZONE TEMP CONT PER AMM, OPS CHECK NORMAL.SDR DALA2026072704342Stop · out of adjustMAIN CABIN DOOR WOULD NOT CORRECTLY LATCH INTO GUST LOCK. READJUST DOOR LATCH MECH/RUBBER STOP IAW AMM 52-12 GUST LOCK ENGAGES/ DISENGAGES AS NORMAL. DOOR OPS CHK NORMAL. A/C OK FOR SVC. (8792584) AIRCRAFT GROUNDED.SDR DALA2026072704340Skin · wornWORN LOWER WING SKIN AT RT WING. REPAIRED PER ER/A 635223-14AD. (1718237) AIRCRAFT GROUNDED.SDR DALA2026072704337Valve · faultyDIVERTED TO LAX DUE TO AN ANTI-SKID FAULT LIGHT. R & R NRML A/S VALVE V7, CKS GOOD. (9626624) AIRCRAFT WAS GROUNDEDSDR DALA2026072704334Floorbeam · corrodedAFT WET AREA STA 947 R/H O/B HARDPOINT HAS CORROSION ON T-CAP. REPAIRED AFT WET AREA STA 947 R/H O/B HARDPOINT T-CAP AREA AS PER REF B737-900 SRM 53-70-51-2R-8 FIG 205. (1717483) AIRCRAFT WAS GROUNDEDSDR DALA2026072704330Stringer · damagedSTRINGER 3L, FR 61 TO FR 62, TOOLING DAMAGE. REPAIRED PER ERA 631893-14. (1718116) AIRCRAFT WAS GROUNDED.SDR DALA2026072704329Stringer · damagedSTRINGER 4L, FR 61 TO FR 62, TOOLING DAMAGE. REPAIRED PER ERA 631895-14. (1717916) AIRCRAFT WAS GROUNDED.SDR DALA2026072704327Wire · damagedSEATS 41,42,43 AB EMERGENCY LIGHTS OUT. REPAIRED WIRING PER A330 AMM 33-52. (9202627) AIRCRAFT WAS GROUNDED.