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 AALA202603208380Light · brokenAIRCRAFT IN BASE MAINTENANCE: FORWARD EMERGENCY FLOOR PROXIMITY LIGHT ON G7 CLOSET IS BROKEN. INSTALLED FORWARD EMERGENCY FLOOR PROXIMITY LIGHT ON G7 CLOSET. PER B737NG CMM 25-32-08 FOR BROKEN LIGHT LENS. PERFORMED SATISFACTORY EEPL OPS CHECK, PER B737-NG AMM SDR IPXA2026031187997Transition Duct · crackedMDC TRANSITION PANEL CRACKED AT THE R/H SIDE OF FUSELAGE AT FR 38.1. . INSTALLED TRANSITION PANEL IAW SRM 51-40-21SDR IPXA2026031187976Floor Support · crackedMDC FLOOR SUPPORT IS CRACKED AT RT SIDE OF FUSELAGE AT FR 38.2. REMOVED AND REPLACED THE FLOOR SUPPORT BRACKET, IAW SRM 51-40-21-001. INSTALLED TRANSITION PANEL AT MDC FLOOR STRUCTURE RT SIDE OF FUSELAGE AT FR 38.2., IAW SRM 51-40-21-001.SDR SIMA20260224003Crossbeam · corrodedCENTER FUSELAGE, RT CROSSBEAM CORRODED AT FR 84. (MAJOR REPAIR) ACCOMPLISHED A PERMANENT REPAIR ON CENTER FUSELAGE, RT CROSSBEAM IAW ERS-EJ-53MR-5387SDR R61A2026031100062Doubler · corrodedWHILE ON HEAVY CHECK, FOUND THAT THE LT COCKPIT FLOOR DOUBLER HAD CORROSION AND WAS MISSING SURFACE PROTECTION FROM FR 8 - FR 12.SDR SWAA2026031373999Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561BB, LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR IPXA2026031187841Floor Support · crackedMAIN CARGO FLOOR STRUCTURE RH SIDEWALL AREA BETWEEN FR37 AND FR38 SUPPORT BRACKET (DOG BONE) IS CRACKED. REMOVED AND REPLACED SUPPORT BRACKET (DOG BONE) P/N A5378103821500 BATCH 0004468444, IAW SRM 51-40-21-001. VERIFIED SUPPORT BRACKET REPLACED PER SRM 51-SDR CALA2026031314560Window Frame · crackedCRACKS FOUND FWD AND AFT AT HOLE#3 OF L/H SIDE NUMBER 3 WINDOW FRAME POST. CRACKS FOUND FWD AND AFT AT HOLE#3 OF L/H SIDE NR 3 WINDOW FRAME, PERFORMED REPAIR TO LEFT-HAND NR 3 WINDOW FRAME E - F POST IAW EA 5310-08195 REVISION C OPERATION 003 ALONG WITH THE ASDR IPXA2026031287931Adapter · crackedMAIN DECK FLOOR STRUCTURE, CLS ADAPTER IS BROKEN AT FR 38.1, BTWN -Y2462 AND -Y1959 AT PANEL 242YK LOCATION. REMOVED CLS ADAPTER AT FR 38.1, BTWN -Y2462 AND -Y1959 AT PANEL 242YK LOCATION IAW SRM 51-40-21. INSTALLED CLS ADAPTER AT MAIN DECK FLOOR STRUCTURE, SDR SWAA2026031173563Seal · crackedLEFT HORIZONTAL STAB FWD UPPER SLIDER SEAL CRACKED. ATTACHED THE TIE- BAR AND CORNER PLATES TO REPLACEMENT UPPER SEAL IAW SRM 51-40-02 & AMM 53-31-31.SDR SWIA2026022475505Support Beam · gougedCARGO DOOR TRACK SUPPORT BEAM ASSY HAS GOUGE AT BS 575.70. REPAIRED THE SUPPORT BEAM IAW REO 601R-53-61-8475, SRM 51-42-06, SRM 51-42-20, SRM 51-42-36, SRM 51-24-16, SRM 51-40-11, SRM 51-21-11, SRM 51-25-06, SRM 51-25-16, SRM 51-42-21.SDR AALA202603114408Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202603103703Angle · out of toleranceAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLES IN FORWARD MOST SEAT TRACK MOUNT CLIP AT STA 1455 AND RBL 74. REPLACED CLIP PER AARD 51-00-05-1.SDR SIMA20260224002Seat Track · corrodedSSI 53-23-005 CENTER FUSELAGE III RH CENTER SEAT TRACK BEAM CORRODED AT FR 84 (MAJOR REPAIR) (LEVEL 2 CORROSION). PERFORMED A PERMANENT REPAIR ON CENTER FUSELAGE III RH CENTER SEAT TRACK BEAM CORRODED AT FR 84 IAW ERJ 175 SRM 53-23-10 RE04SDR SIMA20260224001Seat Track · corrodedSSI 53-10-027 RH CENTER FLOOR BEAM HAS MULTIPLE AREAS OF CORROSION FROM FR 13-17. (MAJOR REPAIR) (LEVEL 2 CORROSION). BLENDED TO REMOVE CORROSION IN MULTIPLE AREAS ON RH CENTER FLOOR BEAM FROM FR 13- TO THE MIDDLE OF FR16 IAW ERJ 175 SRM 51-10-03. MULTIPLE ARESDR SWAA2026030973931Stringer · crackedCRACK INDICATION ON STRINGER 7L OF AFT PRESSURE BULKHEAD CENTER WEB. REPAIRED THE STRINGER IAW EA 26-153-00539.SDR SWAA2026030973597Stiffener · crackedLEFT HORIZONTAL STAB RIB NR 4, HSS 120, STIFFENER NR 4 LOWER RADIUS CRACKED. REPAIRED IAW SRM 55-10-09-2R-4, REPAIR 4 ON THE LT HORIZONTAL STAB RIB NR 4, STIFFENER NR 4.SDR IPXA2026030681012Adapter · corrodedUPPER MAIN CARGO FLOOR PANEL 241LJ, BENEATH SIDE SEAT TRACK HAD CORROSION. REMOVAL CORROSION UPPER MAIN CARGO FLOOR PNL # 241LJ BENEATH SIDE SEAT TRACK IAW A300-600 SRM 53-10-19 PAG 103. VERIFIED CLS ADAPTER INSTALLATION IAW A300-600 SRM 51-40-21-001.SDR IPXA2026030687536Adapter · corrodedFAULT-STR-Z200 MAIN CARGO FLOOR STRUCTURE SEAT TRACK ADAPTER ON FR34 Y0 (LH) IS CORRODED AND DELAMINATED. REMOVED ADAPTER ON FR34 Y0 (LH) AT MAIN CARGO FLOOR STRUCTURE SEAT TRACK IAW SRM 51-40-21. VERIFIED CLS ADAPTER INSTALLATION IAW SRM 51-40-21-001.SDR IPXA2026030688084Seat Track · corrodedMAIN DECK FLOOR STRUCTURE, SEAT TRACK BTWN FR 38.1 AND FR 38.2, -Y450 HAS CORROSION (PANEL 242VK LOCATION). VERIFIED EWIS PROTECTED DURING REPAIRS.SDR IPXA2026030688786Floor Support · corrodedMAIN DECK SUPERNUMERARY AREA FLOOR STRUCTURE, BTWN FR 11 AND FR 12A AT Y1456, WEB UPPER TEE FLANGE HAS CORROSION. REMOVED CORROSION AT AREA FLOOR STRUCTURE, BTWN FR 11 AND FR 12A AT Y1456, WEB UPPER TEE FLANGE IAW SRM 51-74-10. INSTALLED NEW TEE ANGLE AT MCDSDR AALA202603074808Light · inoperativeAIRCRAFT IN BASE MAINTENANCE: GALLEY NR 2, EMERGENCY PATH LIGHT IS INOP LOCATED LEFT ISLE SIDE, BOTTOM FWD LIGHT MAINTENANCE REPLACED EPL IAW AMM 33-51-06.SDR AALA202603068478Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202603064593Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202603063050Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202603065534Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202603060420Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.SDR AALA202603069362Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER J-CHANNEL ABOVE THE FORWARD SPAR TERMINAL FITTING RIGHT HAND LUG IS CRACKED ON THE AFT SIDE OF THE RELIEF CUTOUT. REPLACED J-CHANNEL WITH SERVICEABLE J-CHANNEL ABOVE THE FORWARD SPAR TERMINAL FITTING RIGHT HANDSDR IPXA2026030567301Indicator · damagedNUMBER 17 LEFI DAMAGED. GVI CHECKED FLAP ADJUSTMENT IAW AMM 27-81-00-825-012, ALL CLEARANCES WITHIN LIMITS COMPLETED INSTALLATION OF NR 17 VCF IAW AMM 27-81-02-404-010 UP TO AND INCLUDING SUBTASK 27-81-02-420-003, PARA 3.D.(6).SDR AALA202603058293Floorboard · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT WET AREA FLOORBOARD P/N 151W8716-6 HAS CORRODED INSERTS A NEW FLOORBOARD P/N 151W8716-6 WAS INSTALLED IAW AMM 53-01-01.SDR AALA202603056078Floorboard · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT WET AREA FLOORBOARD P/N 151W8718-18 HAS CORRODED INSERTS INSTALLED FLOORBOARD IAW AMM 53-01-01.SDR AALA202603057841Floorboard · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT WET AREA FLOORBOARD P/N 151W8716-7 HAS CORRODED INSERTS HELPED WITH THE INSTALL OF FLOORBOARD P/N 151W8716-7 IAW AMM 53-01-01.SDR AALA202603055483Floorboard · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT WET AREA FLOORBOARD P/N 151W8715-28 HAS CORRODED INSERTS INSTALLED A NEW FLOORBOARD IAW AMM 53-01-01.SDR AALA202603046504Transmitter · failedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: WHEN EXTENDING THE FLAPS, TRAILING EDGE FLAPS STUCK ASYMMETRICAL BETWEEN 0 AND 1 WITH LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT TPA. REMOVED AND REPLACED NRSDR AALA202603044477Floorboard · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT WET AREA FLOORBOARD P/N 151W8710-50 HAS CORRODED INSERTS. MAINTENANCE INSTALLED NEW FLOORBOARD P/N 151W8710-50 IAW AMM 53-01-01 SO DY0V.SDR AALA202603049026Floorboard · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT WET AREA FLOORBOARD P/N 151W8716-5 HAS CORRODED INSERTS. MAINTENANCE INSTALLED NEW REPLACEMENT FLOORBOARD ASSEMBLY WITH NEW FLOORBOARD INSERTS IAW AMM 53-01-01.SDR AALA202603041738Floorboard · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT WET AREA FLOORBOARD P/N 151W8718-15 HAS CORRODED INSERTS. MAINTENANCE REMOVED DAMAGED FLOORBOARD & INSTALLED A NEW FLOORBOARD P/N 151W8718-15 IAW AMM 53-01-01 SO DW76.SDR AALA202603040119Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING BEARING FOR THE UPPER ACTUATOR ATTACHMENT HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW CMM 52-81-18.SDR AALA202603049487Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING BEARING FOR THE UPPER ACTUATOR ATTACHMENT HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW CMM 52-81-18.SDR DALA2026030201418Skin · corrodedCORROSION ON SKIN STA 737 X: -15 TO -30 APROX AT FUSELAGE. REPAIR INSTRUCTIONS AND PRI 631685-14 (1466288)SDR DALA2026030201417Skin · crackedCRACK ON FUSELAGE SKIN STA Y =1037 LONG 13 LH-14LH SIDE. REPAIRED PER PRI 631741-14 (1466248)SDR DALA2026030201416Skin · crackedSHIP 9500 BENT, ALSO CRACK ON RUDDER SKIN AT LH LOWER EDGE XR -5.000 CANT. CORRECTIVE ACTION: REPAIRED PER PRI 631766-14 (1466225)SDR FDEA202602240303Safety Wire · wrong partFOUND LH ESCAPE SLIDE WITH INCORRECT SAFETY OF PACK RELEASE MECHANISM. COMPLIED WITH E.A. 9-2560-T0386431. CORRECT SAFETY WIRE INSTALLED ON L1 DOOR ESCAPE SLIDE PACK RELEASE MECHANISM.SDR VNAA2026022813001Pcb · failedL VIB FAULT, R VIB FAULT, STATUS MESSAGE AT FL230. REMOVED AND REPLACED JB2, PCB2 IAW CRJ 700 AMM 24-01-05-000/400-801-A01. OPS CHECK GOOD AT THIS TIME.SDR SWAA2026022773707Handle · crackedPASSENGER CABIN AFT GALLEY SERVICE DOOR HANDLE COVER CRACKED. R & R PASSENGER CABIN AFT GALLEY SERVICE DOOR HANDLE COVER IAW AMM 52-41-31.SDR AALA202602270090Bottle · low pressureAIRCRAFT WAS GROUNDED: CAUTION CHECK DOOR PRESSURE 4L ON CIDS PANEL. MAINTENANCE SERVICED THE 4L DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.SDR AALA202602274387Sliding Window · scratchedAIRCRAFT WAS GROUNDED: FLIGHT DECK RIGHT HAND SLIDING WINDOW HAS THIN SCRATCHES AND SWIRLS MAKE VISIBILITY DIFFICULT. REPLACED SLIDING WINDOW IAW AMM 56-12-11.SDR DXTA2026022707028Pressure Switch · illuminatedWHEN SELECTING THE CROSSFEED FROM L TANK TO RIGHT ENGINE, RECEIVED AMBER CAS MESSAGE: FUEL BOOST PUMP R. FOLLOWED THE QRH. MESSAGE DID EXTINGUISH. THIS CONDITION HAS HAD A PREVIOUS HISTORY OF SUCH. SENT ARES TO CESSNA TEAM680 FOR EVALUATION. FOUND LH FUEL LOWSDR DXTA2026022707024Bearing · defectiveAFTER TAKEOFF, GEAR RETRACTED NORMALLY. DURING CLIMB OUT (APPROXIMATELY 10000-12000 FEET) THE RED GEAR UNLOCK LIGHT ILLUMINATED. RAN QRH. DURING THE GVI OF THE NLG ASSEMBLY FOUND THE UPLOCK BEARING WAS COMPLETLY MISSING FROM THE NOSE GEAR CAUSING THE UPLOCK SSDR NX422026022700010Stud · displacedUPON DISASSEMBLY FOR IT'S FIRST OVERHAUL, DAMAGE WAS FOUND ON ONE OF THE THRU STUDS. THE DAMAGE APPEARS TO BE DISPLACED STEEL UNDER THE THREADED PORTION ON THE SHOULDER OF THE THRU STUD. THE DAMAGE IS MINOR BUT DUE TO THE SIMILAR LOCATION AND SEVERITY OF THE D