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 FDEA202608151133Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1671 X= 27.5" FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT WORN CROWN AT SEAT TRACK STATION 1671 X = 27.5" EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMSDR HNAA2026081700725Light · inoperativeLH FWD EXT EMER LITGHT WILL NOT ILUMINATE. R & R EMER LIGHT ASSY IAW AMM 33-50-10-000/400-801-A. OPS CHECK GOOD, OK FOR SERVICESDR 141A2026081500001Tire · blownWHILE LANDING IN JONESBORO, MADE A NORMAL TOUCHDOWN AT ABOUT 70 - 75 KNOTS WITH FULL FLAPS & STARTED TO PUT ACFT IN FULL REVERSE THRUST & STARTED GETTING ON BRAKES. TOUCHDOWN STRAIGHT & ON CENTER LINE. ACFT WAS NOT SIDE LOADED. RT SIDE, FELT WEIRD UPON TOUCHDSDR SIMA20260815001Light · inoperativeEMERGENCY PHOTOLUMINESCENT STRIPS LIGHTS FWD CABIN BY CLOSET INOPERATIVE. R & R FWD MOST PHOTOLUMINESCENT STRIP LIGHT BY CLOSET IAW AMM 33-50-21.SDR CALA2026081718691Acoustic Panel · inflt separationNR 1 ENGINE ACOUSTIC PANEL NR 6 DEPARTED THE ACFT. MEASUREMENT 33 INCHES LONG & 21.5 INCHES WIDE. TOTAL 709 SQ INCHES. WORK ACCOMPLISHED REF LOG 9970963 & GMM 02-30-95 3C(1) NR 1 ENGINE INSPECTION, FOUND ACOUSTIC LINER PANEL 6 O'CLOCK MISSING & BROKEN OFF ATSDR CALA2026081718683Power Supply · inoperativeEMERGENCY LIGHTS FROM ROW 28 TO 34 INOP. REMOVED AND REPLACED POWER SUPPLY FOR M3378 IAW AMM 33-51-06-960-803. OPERATIONAL CHECK GOOD.SDR CALA2026081718676Floor Support · corrodedCORROSION ON AFT WET AREA FLOOR SUPPORT, BS 947 - 967, WITH CORRODED AREA AROUND HARD POINT FITTING, RBL 50. R & R FLOOR SUPPORT BETWEEN BS 947 - 967, RBL 50 IAW SRM 51-40-02-0G-0 & DWG 147A5650.SDR CALA2026081718673Skin · crackedLEFT WING LOWER SKIN AT STR 9, DURING HFEC INSPECTION, A CRACK WAS FOUND AT OTBD MOST FASTENER. REF EA5725-01143 REVISION B OP. 003, SEQ 4. REFERENCE LP9951108 DIP GENERATED. PERFORMED REPAIR ON LT WING LOWER SKIN AT STR 9 AREA, ALL WORKS WERE ACCOMPLISHED ISDR CALA2026081718670Acm · failedSTRONG ACRID ODOR WHEN APU RUNNING. CREW DEBRIEFED. ON ENG SHUTDOWN, RT PACK ACM FAILED AND CAUSED BURNING ODOR IN CABIN ALONG WITH ASSOCIATED STATUS MESSAGES. TESTING SHOWED RT ACM FAILED & MEL APPLIED ON LP 9971449. CONDITIONAL INSPECTION FOR SMOKE/ODOR IASDR CALA2026081518643Fuel Cap · missingMISSING FUEL CAPSDR DALA2026081604677Light · faultedDURING SVC CHECK FOUND EXTERIOR AFT LIGHT FAULT DURING EPSU TEST. REMOVED 4R DOOR SLIDE IAW AMDS W/C 2561-4002-RA. OK TO INSTALL 4R SLIDE QC5458. INSTALLED 4R DOOR SLIDE IAW AMDS W/C 2561-4002-RA. (LP 8620311 - AIRCRAFT WAS GROUNDED)SDR DALA2026081604676Light · faultedDURING SVC CHECK FOUND EXTERIOR AFT LIGHT FAULT DURING EPSU TEST. REMOVED ORIGINAL SLIDE 4L TO T/S FAULT IAW AMDS WORK CARD 2561-4001-LA,. OK TO INSTALL ORIGINAL SLIDE. REINSTALLED ORIGINAL DOOR SLIDE 4L IAW AMDS WORK CARD 2561-4001-LA. (LP 8620310 - AIRCRAFSDR I5PA2026081588803Control Unit · intermittentMGE305 - ETOPS : LT WINDOW HEAT EICAS MESSAGE ON DESCENT. REPLACED THE LT FWD WINDOW HEAT CONTROL UNIT IAW AMM.SDR 2026FA0000643Stringer · debondedDISBOND, LH WING, UPPER SKIN BOND ASSY, S-2 @ CWS 117.60 AND S-3 @ CWS 201.25. THE SKIN AND COMMON STRINGERS MAY ALSO EXHIBIT A GRADUAL DEVIATION FROM CONTOUR IN THESE AREAS. THE EXTENT OF THE DEFECT IS LOCATED USING ULTRASOUND INSPECTION AND CORRECTED BY ADSDR JR2R20260815234Attach Angle · corrodedWING TO BODY LANDING AT FR 52 IS CORRODED OUT OF LIMITS. REPLACED.SDR SWIA2026081477829Access Panel · damagedFADEC ACCESS PANEL 431AL HAD A DAMAGED FASTENER HOLE. REPAIRED THE DAMAGED FASTENER HOLE ON FADEC PANEL 431AL IAW REO 690-54-11-636, REV-P1, REV--.SDR SWAA2026092362109Support · corrodedCORRODED LOWER SILL BTWN BS 794.5 - 847, RBL 23, WL 156. REMOVED CORROSION AND EVALUATED REWORKED AREAS LOWER SILL IAW SRM 53-60-15-1A-1.SDR 2026FA0000756Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.SDR SWAA2026092167397Vapor Barrier · crackedCRACKED VAPOR BARRIER, BS 663.75, LBL 27. REPAIRED THE VAPOR BARRIER IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026092181079Vapor Barrier · crackedCRACK VAPOR BARRIER BS 663.75 AND RBL 32 AT MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER BS 663.75 AND RBL 32 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026092169457Crossbeam · crackedCRACKED FLOOR CROSSBEAM, BS 540, BTWN BL 0 - RBL 24.75. REPLACED THE CROSSBEAM IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A0060, SHEET 46, REV -.SDR SWAA2026092105704Support Angle · crackedCRACKED SUPPORT ANGLE, BS 663.75, RBL 7. INSTALLED A PERMANENT REPAIR TO THE SUPPORT ANGLE IAW SRM 57-10-10-2R-5, REPAIR 5, AND DWG 111A100, SHEET 226, REV A.SDR ASAA2026081468793Floorbeam · corrodedUPON REMOVAL OF DAMAGED LAV MOUNT FITTINGS FOUND CORROSION ON BS 947 FLOORBEAM UPPER CAP AT ALL 4 LAV MOUNT FITTING LOCATIONS. GROUNDED - YES. REPAIRED FLOORBEAM 947.5 LBL-59-RBL-59 IAW SRM 53-70-51-2R-5 REPAIR 5, EA 900ER-53EA-30665.SDR ASAA2026081468792Sill Drain · corrodedR2 MOPSILL HAS MULTIPLE AREAS OF CORROSION. GROUNDED - YES. REMOVED & REPLACED R2 MOP SILL CHORD IAW BOEING SRM 51-40-02.SDR IPXA2026091780741Frame · damagedRIGHT WING FR 47 UPPER RADIUS BRACKET HAS ELONGATED HOLES. INSTALLATION OF SPLICE AND SPAR CONTROLLED IN THE EO-18290-JIC004.SDR REXA2026092101869Seat Track · corrodedCORROSION ON RT SIDE SEAT RAIL (1E/A) FROM BS 907 - 969 IN THE PAX CABIN. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49.SDR REXA2026092101868Seat Track · corrodedCORROSION ON THE RT SIDE SEAT TRACK, BS 661+101 - 847+14. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49SDR REXA2026092101867Seat Track · corrodedCORROSION ON RT SIDE SEAT TRACK, BS 379 - 482. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49.SDR REXA2026092101866Seat Track · corrodedCORROSION ON LT SIDE SEAT TRACK, BS 744 - 761. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49SDR REXA2026092101865Seat Track · corrodedCORROSION ON RT SEAT TRACK, RBL 9 BTWN BS 349 - 677. THE SEAT TRACKS WAS REPLACED IAW AMM 53-00-49.SDR REXA2026092101863Seat Track · corrodedCORROSION ON FLOOR SEAT TRACK FROM BS 374 TO 409, LBL 9 AT PAX CABIN. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49SDR AALA202609187342Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT MAIN LANDING GEAR DOOR FORWARD FITTING CRACKED - REPLACED FITTING PER CMM 52-81-18SDR AYPA20260917001Fire Detector · false activationDURING CRUISE FLIGHT, A MOMENTARY INSTANCE OF THE #1 ENG FIRE WARNING SYSTEM ILLUMINATED. NO SECONDARY OR CONFIRMING INDICATIONS. NO TRAILING SMOKE WAS OBSERVED.SDR SCNA20260916396Speed Brake · faultedSPEED BRAKE NOT ENGAGING ON LANDING. PERFORMED BITE TEST OF AACU PER B737 FIM TASK 32-42 TASK 801. FAULT CLEARED. RETESTED NO FAULTS. A/C OK FOR SVC AT THIS TIME.SDR ASAA2026081468665Mount · corrodedUPON REMOVAL OF DAMAGED LAV MOUNT FITTINGS FOUND LAV SUPPORT RBL 20 BETWEEN STA 947 AND 967 TO BE CORRODED WHERE MOUNT SITS. GROUNDED - YES. REMOVED CORROSION & FOUND OUT OF LIMITS IAW BOEING 737-900ER SRM 53-70-51-1A-1. REMOVED & REPLACED LAV MOUNT SUPPORT INSDR ASAA2026081468664Mount · corrodedUPON REMOVAL OF DAMAGED LAV MOUNT FITTINGS FOUND INTERCOSTAL RBL50 BETWEEN STA 927 AND 947 TO BE CORRODED WHERE MOUNT SITS. GROUNDED - YES. REMOVED CORROSION & FOUND OUT OF LIMITS IAW BOEING 737-900ER SRM 53-70-51-1A-1. REMOVED & REPLACED LAV MOUNT SUPPORT INTSDR ASAA2026081468663Mount · corrodedUPON REMOVAL OF DAMAGED LAV MOUNT FITTINGS FOUND LAV SUPPORT LBL 50 BETWEEN BS 947 & 967 TO BE CORRODED WHERE MOUNT ATTACHES. GROUNDED - YES. REMOVED CORROSION & FOUND OUT OF LIMITS IAW BOEING 737-900ER SRM 53-70-51-1A-1. REMOVED & REPLACED LAV MOUNT SUPPORT ISDR ASAA2026081468609Mount · corrodedUPON REMOVAL OF DAMAGED LAV MOUNT FITTINGS FOUND LAV SUPPORT RBL50 BETWEEN STA 947 AND 967 TO BE CORRODED WHERE MOUNT ATTACHES. GROUNDED - YES. REMOVED CORROSION & FOUND OUT OF LIMITS IAW BOEING 737-900ER SRM 53-70-51-1A-1 REMOVED & REPLACED LAV MOUNT SUPPORT SDR IPXA2026090991849Floor Panel · damagedMAJOR REPAIR. MCD FLOOR PANEL 242DN IS BROKEN. FLOOR PANEL 242DN IS FABRICATED IAW SREO-16407-REQ001 (APPX B) A300 MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATION.SDR IPXA2026090987132Floor Panel · brokenMAJOR REPAIR. MCD FLOOR PANEL 231WG IS BROKEN. THE FLOOR PANEL 231WG WAS FABRICATED IAW SREO-16407-REQ001 (APPX B) A300 MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATION.SDR IPXA2026090987296Floor Panel · brokenMAJOR REPAIR. MCD FLOOR PANEL 231VG IS BROKEN. PANEL 231VG IS FABRICATED IAW SREO-16407-REQ001 (APPX B) MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATION.SDR SWAA2026090862594Pressure Deck · corrodedCORROSION AT HORIZONTAL PRESSURE DECK WEB BS 663 +4" RBL 67, WL 203. CORROSION AT HORIZONTAL PRESSURE DECK WEB STA 663 +4" RBL67 WL 203. IAW EA 26-153-02215 THE DAMAGE IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERSDR SWIA2026081477106Seat Track · corrodedCORROSION ON FWD WET AREA R/H SEAT TRACK BETWEEN FR12-21 IN 9 LOCATIONS AS MARKED. REMOVED AND REPLACED R/H SEAT TRACK BETWEEN FR12-21, REF SRM 51-40-08.SEE CONTINUATION CARD FOR ADDITIONAL WORK PERFORMED. NO CHANGE TO WEIGHT AND BALANCE.SDR IPXA2026090494048Support Fitting · crackedHORIZONTAL STAB, R/H LOWER APRON ATTACH AREA, #10 BRACKET, WITH CRACK. REMOVED #10 BRACKET, HORIZONTAL STAB, R/H LOWER IAW A300-600 SRM 51-40-21-001. REPLACED APRON FITTING SUPPORT P/N A5517160320251 AT R/H LOWER APRON ATTACH AREA, #10 BRACKET IAW SRM 51-40SDR SWAA2026090715135Plate · crackedBEHIND THE 551EB PANEL THERE IS A WIGGLE PLATE CRACKED BEHIND THE 551EB PANEL THERE IS A WIGGLET CRACKED. REMOVED AND REPLACED FOR NEW WIGGLE PLATE IAW SRM 51-40-02-0G AND DWG BOEING 115A2001 REV A.SDR AALA202609058224Link · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FLAP TRACK POSITION 2 INBOARD LINK - MAINTENANCE REPLACED LINK PER AIRBUS DRAWING D57556566SDR AALA202609052251Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 3 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609058400Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 5 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609052288Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STAB ELEVATOR POSITION 5 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609050642Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STAB ELEVATOR NR 2 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42