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 FDEA202607231004Seat Track · wornMAIN DECK CARGO SEAT TRACK AT BS 810, X= -8.5, FOUND CROWN WORN. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT BS 811 TO EXISTING SPLICE BS 745, X = - 8.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA202607231003Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541, X= 47.5" CROWN FOUND WORN. EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED BY SECTIONAL REPLACEMENT AT STATION 1571 TO EXISTING SPLICE STATION 5-123/1SDR FDEA202607231002Seat Track · wornMAIN DECK CARGO BAY SEAT TRACK AT BS 1541, X= 27.5" CROWN FOUND WORN. EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT BS 1571 TO EXISTING SPLISDR FDEA202607231001Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541, X= 8.5" CROWN FOUND WORN. SEAT TRACK STATION 1541, X = 8.5 EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SESDR FDEA202607231000Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541, X= -8.5" CROWN FOUND WORN. SEAT TRACK STATION 1541, X = - 8.5 EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONASDR FDEA202607230999Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541, X= -27.5" CROWN FOUND WORN. SEAT TRACK STATION 1541, X = - 27.5 EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTSDR FDEA202607230998Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541, X= -47.5" CROWN FOUND WORN. SEAT TRACK STATION 1451, X = - 47.5 EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTSDR FDEA202607230997Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10, X= -27.5" CROWN FOUND WORN. MAIN DECK CARGO COMPARTMENT WORN SEAT TRACK AT STATION 5-10, X = -27.5 EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROSDR FDEA202607230996Seat Track · wornCABIN- MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-11, X= -47.5" CROWN FOUND WORN. MAIN DECK CARGO COMPARTMENT WORN CROWN AT SEAT TRACK STATION 5-11, X = - 47.5 EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLESDR FDEA202607230995Seat Track · wornCABIN- MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1421, X= 47.5" CROWN FOUND WORN. MAIN DECK CARGO COMPARTMENT WORN CROWN AT SEAT TRACK STATION 1421, X = 47.5 EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DASDR FDEA202607230994Seat Track · wornCABIN- MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1421, X= 8.5" CROWN FOUND WORN. MAIN DECK CARGO COMPARTMENT, WORN CROWN AT SEAT TRACK STATION 1421, X= 8.5 EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGESDR FDEA202607230993Seat Track · wornCABIN- MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1421, X= -8.5" CROWN FOUND WORN. MAIN DECK CARGO COMPARTMENT WORN CROWN AT SEAT TRACK STATION 1421, X = - 8.5 EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMSDR FDEA202607230992Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1421, X= -27.5" CROWN FOUND WORN. MAIN DECK CARGO COMPARTMENT WORN CROWN AT SEAT TRACK STATION 1421, X = - 27.5 EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGESDR FDEA202607230991Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1421, X= -47.5" CROWN FOUND WORN. MAIN DECK CARGO COMPARTMENT WORN CROWN AT SEAT TRACK STATION 1421, X= -47.5 EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CRSDR QR9R2026072300003Bolt · crackedNDI REVEALED HEX BOLT WAS CRACKED IN THREAD AREA AROUND COTTER KEY HOLE.SDR QR9R2026072300002Sensor · fluctuatesAFTER REFUEL, DURING PRE-TAKEOFF CHECK, GENERATOR AMPS WERE NOT WITHIN 10 & STAYED AT 15-20+ WITH THE NR 2 BETWEEN 35-40 AND NR 1 SOLID AT 20. A TEST FLIGHT EVAL SHOWED AFTER START AND IN FLIGHT IDLE, BOTH SIDES INDICATED 28.4V. AMPS WERE 25-30 ON NR 1 AND 40 SDR QR9R2026072300001Sensor · faultyNR 2 GENERATOR AMPS DROPPED TO 5 AMPS DURING RUN-UP. NR 1 SIDE REMAINED STEADY AT 30 AMPS. REMOVED AND REPLACED NR 2 GENERATOR HALL SENSOR IAW 24-30-00, 4-6. T/F MOC SUCCESSFULLY COMPLETED.SDR SWIA2026072277269Cup · corrodedPASSENGER DOOR CUTOUT AFT DOOR HANDLE FLOOR CUP HAS CORROSION. REMOVED CORROSION ON PASSENGER DOOR CUTOUT AFT DOOR HANDLE FLOOR CUP AND FOUND OUT OF LIMITS REPLACED WITH 1 EA OF NEW FLOOR CUP IAW SRM 51-42-06 REV 39 AND DWG 601R31527 REV AM, COMPLIED WITH TSDR SWIA2026072277262Cam · wornCABIN DOOR CAM FITTING WAS WORN AT BS 310. BLENDED THE DAMAGE ON THE CAM FITTING AND FOUND OUT OF LIMITS, REMOVED AND REPLACED THE CAM FITTING IAW SRM 51-42-21, REV 39, & DWG 600-31900, REV K. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SWIA2026072277245Cup · corrodedPASSENGER DOOR CUTOUT, FWD DOOR HANDLE FLOOR CUP WAS CORRODED. REMOVED AND REPLACED PASSENGER DOOR CUTOUT FORWARD DOOR HANDLE FLOOR CUP IAW SRM 51-42-06, SRM 51-42-13, & DWG 601R31527, REV AM. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SWIA2026072277234Striker · dentedPASSENGER DOOR SURROUND STRUCTURE BS 310 SEAL STRIKER DENTED NEXT TO UPPER PIN STOP FITTING. REPAIRED THE PAX DOOR SEAL STRIKER IAW REO 601R 53-22-033, REV D. REPAIR TYPE 1, LEAK CHECKED GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR IPXA2026092197676Door Frame · crackedUPON REMOVAL OF SEAL RETAINER AT RT WW CUTOUT BS 1060 FOUND CHANNEL SUPPORT WITH ELONGATED HOLE AND CRACKED. INSTALLED SUPPORT CHANNEL AT RT WW CUTOUT BS 1060 IAW SRM 51-40-02-0G-0.SDR AALA202609159973Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: FOUND GALVANIC CORROSION ON STR 27L 6" AFT OF FS 807. INSTALLED NEW STRINGER SPLICE IAW SRM 53-00-03-2R AND IAW DWG 146A3234.SDR IPXA2026090806015Frame · dentedMAJOR REPAIR, AFT CARGO BAY INTERNAL FUSELAGE STRUCTURE, FRAME HAS 2 EA DENT APPROX AT BS 1500, BTW STGR 25R AND STGR 26R, ACCOMPLISHED REPAIR PER EO-98513-REQ1 AND STE-SAA EA 757-5360-01-B0804, REV. I/RSDR IPXA2026083005688Floorbeam · corrodedMAJOR REPAIR, MAIN DECK CARGO BAY FLOORBEAM LOWER FLANGE HAD CORROSION APPROX AT BS 1560, RBL 26, ACCOMPLISHED THE REPAIR PER EO-98392-REQ1 AND STE-SAA EA 757-5310-01-B0795, REV. I/RSDR IPXA2026090705909Floorbeam · corrodedMAJOR REPAIR, MAIN DECK CARGO BAY FLOORBEAM LOWER FLANGE HAS MULTIPLE NUT PLATE CORRODED APPROX AT BS 1480, BL 0 THRU RBL 62, ACCOMPLISHED THE PERMANENT REPAIR PER EO-98517-REQ1 AND STE-SAA EA 757-5360-01-B0797, REV. I/RSDR IPXA2026072906421Sidewall Panel · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL HAS CORROSION ON MULTIPLE AREAS APPROX BTW BS 1200 AND BS 1310, LBL 20 THRU LBL 24, INSTALLED AFT CARGO LT SIDE PANEL TO FLOOR STUCTURE AT BS 1200 - 1310 AND DISPLACED FRAME SUPPORT IAW SRM 51-40-02-0G-0SDR SWAA2026090285513Strap · corrodedCORROSION INTERNAL CAVITY LEADING EDGE STRAP BTW OFSS 296 TO OFSS 300 AT LT WING 2026-446638 TOOL USED ON STEPS 12 AND 13: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S/N: 250592609 DUE DATE: 03-OCT-26. PERFORMED REPAIRE ON INTERNAL CAVITY LEADING EDGE STRAP BTW OSDR AALA202609023994Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: FOUND GALVANIC CORROSION ON STRINGER LOCATION BS 787 AND LBL 21. REMOVED AND REPLACED SECTION OF STRINGER BAC1498-159 USING AN INTERNAL DOUBLER AND HAT SPLICE BAC1498-116; IAW SRM 53-00-03-2R-1.SDR AALA202609019989Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: FS 947 FLOOR BEAM T-CAP CORRODED IN 4 SEPARATE AREAS REQUIRING REPLACEMENT OF THE EXISTING T-CAP. REMOVED AND REPLACED FS 947 FLOOR BEAM T-CAP IAW SRM 53-70-51-2R.SDR VNAA202608310012Seat Track · corrodedCORROSION ON THE SEAT TRACK LBL 9, BS 364 - 480.50, AS WELL AS ON THE SEAT TRACK AT RBL 9, BS 349 - 480.50. SEAT TRACK LBL 9, BS 364 - 480.50. AS WELL AS ON THE SEAT TRACK AT RBL 9, BS 349 - 480.50. WERE EVALUATED WITH EXCESIVE DAMAGE IAW SRM 53-21-49-101-SDR VNAA202608310011Seat Track · corrodedCORROSION ON RT SIDE SEAT TRACKS (4EA) BTW BS 379 TO 669. DUE TO EXCESIVE DAMAGE ON RH SIDE SEAT TRACKS (4EA) BTW STA FS 379 TO FS 669, SEAT TRACKS WERE REPLACED IAW SRM 53-21-49-101-001-A01 AND SECTION OF SIDE SEAT TRACKS RT (4EA) WERE INSTALLED BTW BS 379 SDR VNAA202608310010Seat Track · corrodedCORROSION ON LT SIDE SEAT TRACKS (5 EA) BTWN BS 379 - 669. DUE TO EXCESSIVE DAMAGE ON THE SEAT TRACKS WERE REPLACED IAW SRM 53-21-49-101-001-A01, & AMM 53-00-49-400-801, (CONFIG A12).SDR ASAA2026072268334Floorbeam · corrodedAFT WET BS 986.5 FLOORBEAM CORRODED ON UPPER FLANGE AT RBL-42. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1, REPAIRED FLOORBEAM IAW SRM 53-70-51-2RSDR ASAA2026072268294Sill Drain · corrodedAFT WET L/2 MOPSILL CORRODED IN MULTIPLE AREAS. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW BOEING 737-800 SRM 53-70-15-1A-1, REMOVED AND REPLACED INNER CHORD (MOPSILL) IAW BOEING 737-800 SRM 51-40-02-0G-1 W= 2" O= .080 R= .063 L= 1" D= .01SDR ASAA2026072268291Support · corrodedAFT WET AREA FLOOR SUPPORT HAS CORROSION BETWEEN STA 907-927 LBL 20. GROUNDED - YES. REPAIRED AFT WET AREA FLOOR SUPPORT BETWEEN STA 907-927 LBL 20 IAW EA 800-53EA-30625 W= 1.0" O= .076" R= .055" L= 1.0" D= .021.SDR HNAA2026082700807Shear Tie · crackedSHEAR TIE CRACKED AT FR 13, BTWN STR 6 - 7R. R & R THE SHEAR TIE IAW SRM 51-40-02SDR AALA202608265281Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: GALVANIC CORROSION LOCATED AT STATION 787, STRINGER 22L. MAINTENANCE REPAIRED DEFECTIVE PART LOCATED AT STATION 787, STRINGER 22L PER SRM 51-10-02G AND REPLACED ON N/R 996.SDR ASAA2026072268290Floor Support · corrodedAFT WET AREA FLOOR SUPPORT HAS CORROSION BETWEEN STA 907-927 LBL 30. GROUNDED - YES. REPAIRED AFT WET AREA FLOOR SUPPORT AT STA 907-927 LBL 30 IAW EA 800-53EA-30625 W= 1.0" O= .076" R= .060" L= 1.0" D= .016.SDR ASAA2026072268261Angle · corrodedAFT WET ZEE ANGLE BS 990 TO STA 1016 RBL-32 CORRODED ON MULTIPLE AREAS. GROUNDED - YES. AFT WET AERA ZEE ANGLE FOUND TO HAVE NO ALLOWABLE LIMITS, REMOVED AND REPLACED ZEE ANGEL IAW B737-800 SRM 51-40-02-0G-0 W= 1" O= .050 R= .036 L= 1" D= .014.SDR ASAA2026072268260Web · corrodedAFT WET WEB AT BS 987, RBL-44 CORRODED. GROUNDED - YES. AFT WET AREA WEB FOUND TO BE OUT OF LIMITS, NO DAMAE ALLOWED IAW SRM 53-70-51-1A-1, REMOVED AND REPLACED WEB IAW SRM 51-40-02-0.SDR ASAA2026072268259Floorbeam · corrodedAFT WET STA 986.5 FLOOR BEAM CORRODED AT LBL-38 ON UPPER FLANGE. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMTIS IAW B737-800 SRM 53-70-51-1A-1, REPAIRED FLOOR BEAM IAW B737-800 SRM 53-70-51-2R-4 W= 1.5" O= .160 R= .105 L= 3" D= .055.SDR ASAA2026072268258Sill Drain · corrodedAFT WET R/2 MOPSILL CORRODED IN MULTIPLE AREAS. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1. REMOVED AND REPLACED MOPSILL IAW SRM 51-40-02-0G-0. W= 1.200 O= .080 R= .063 L= 4.750 D= .017.SDR ASAA2026072268257Support · corrodedAFT WET INTERCOSTAL (LAV SUPPORT) STA 947 TO STA 967 RBL -50 CORRODED ON UPPER FLANGE. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW BOEING 737-800 SRM 53-70-51-1A-1, REMOVED AND REPLACED SUPPORT IAW BOEING 737-800 SRM 51-40-02-0G-0.SDR IPXA2026082688984Cam · gougedCREW ENTRY DOOR UPPER AND LOWER LATCH CAM HAS GOUGE DAMAGE. INSTALLED CREW ENTRY LOWER LATCH CAM IAW CMM 52-11-08 AND AMM 20-11-00-912-001.SDR IPXA2026082605349Frame · crackedNDT SUSPECTED CRACKS ON FRAME 40 FUEL TANK SIDE VERTICAL STIFFENERS. INSTALLED STIFENER REPAIR, DOUBLER AND FRAME STIFENER WAS INSTALLED IAW SRM 51-40-21 AND SRM 57-10-21/201 PER GMM 04-02.SDR GCXA2026082600670Egt Indication · out of limitsENG 1 EGT OVER LIMIT FLIGHT CREW OBSERVED TEMPERATURE 985DEG C WITH MASTER CAUTION. BASED ON THE REPORTED TEMPERATURE PER THE AMM IT REQUIRED AN ENGINE REMOVAL.SDR HNAA2026082500786Window Frame · crackedLEFT FR10 UNDER WINDOW FRAME ANGLE CRACKED. RAR FRAME ANGLE IAW SRM 51-40-02SDR HNAA2026082500784Window Frame · crackedRT FR 10 UNDER WINDOW FRAME ANGLE CRACKED. R & R ANGLE IAW SRM 51-40-02SDR ASAA2026072268161Floor Support · corrodedAFT WET AREA FLOOR SUPPORT STRUCTURE IS CORRODED BETWEEN STA 927-947 LBL 20. GROUNDED - YES. REMOVED AND REPLACED AFT WET AREA FLOOR SUPPORT STRUCTURE BETWEET STA 927-947 LBL 20, IAW B737-800 SRM 51-40-02-0G-0, STEPS: 4.B & 7.C. W= 2" O= .084" R= .058" L1" D=