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 IPXA2026021260798Handle · brokenENTRY DOOR OUTR HANDLE SHUTTER BROKEN REMOVED AND REPLACED L1 DOOR SHUTTER HANDLE IAW AIRBUS CMM 52-11-11. OPS CHECK GOOD.SDR DALA2026021201020Indicator · malfunctionedCAPTAIN`S AIRSPEED INDICATOR FLAG IN VIEW. REPLACED CAPT AIRSPEED INDICATOR.SDR DALA2026021201018Spring · inoperativeIN REF AMDS 2560-01492-02010, STEP 2B, LEAF SPRING DID NOT HOLD THE AFT GIRT BAR SLIDER AT L2 DOOR. THE TWO SPRINGS ON THE AFT GIRT BAR SLIDER WERE REPLACED & GIRT BAR INSPECTION WAS PERFORMED IAW CMM 25-66-14, AND AMDS 2560-01492-0201. (1447157)SDR DALA2026021201017Snubber · out of limitsCOMPRESSOR INDICATOR EXTENSION OUT OF LIMITS AT ROTARY SNUBBER OF R4 DOOR. THE R4 DOOR WAS REMOVED & INSTALLED IAW AMM 52-11-01, ROTARY SNUBBER WAS REPLACED IAW AMM 52-11-09. AND AMM 52-11-10. (1446927)SDR DALA2026021201016Strap · crackedCRACKED PREVIOUS REPAIR OF STABILIZER STRAP BTW BS 365 - 377, LBL. 25, LT OTBD NLG WW AREA. STABILIZER STRAP WAS REPAIRED IAW SRM 53-00-51-2R-12 PAR.4, SRM 51-40-02-0G, PARA 7 D, SRM 51-20-05-0G, DAL P.S. 900-2, NO 09, & DWG 51-0039, REV C. (1446242)SDR FDEA202602110181Floor Panel · dentedMAIN DECK, AT APROX. BS 870, FLOOR PANEL 241FFF, SURFACE SKIN DENTED. REPAIRED THE TOP SKIN OF THE FLOOR PANEL IAW SRM 53-00-50-2R 4.B. INSTALLATION OF FLOOR PANEL 241FFF WILL BE ACCOMPLISHED ON WO 91257, SEQ 149. MAJOR REPAIR.SDR FDEA202602110180Floor Panel · dentedMAIN DECK, AT APROX. BS 820, FLOOR PANEL 241AFF DENTED. REPAIRED TOP SKIN OF MAIN DECK FLOOR PANEL IAW SRM 53-00-50-2R 4.B. INSTALLATION OF THE FLOOR PANEL 241AFF WILL BE ACCOMPLISHED ON WO 91257, SEQ 149. MAJOR REPAIR.SDR FDEA202602110179Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 241QFF OF MDC. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 93, AUG 15, 2025.SDR FDEA202602110178Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 241MFF OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 93, AUG 15, 2025.SDR FDEA202602110177Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 241WFF OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 93, AUG 15, 2025.SDR FDEA202602110176Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 242SFF OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 93, AUG /15, 2025.SDR CALA2026021213743Release Mech · damagedFOUND BOTH LEFT FWD, & AFT EMERGENCY OVERWING EXITS SLIDE RELEASE MECHANISMS DAMAGED IAW AMM 52-21-11. R & R BOTH LT FWD AND AFT EMERGENCY OVERWING EXITS SLIDE RELEASE MECHANISMS IAW AMM 52-21-11.SDR CALA2026021213742Slide Raft · expiredL2 DOOR SLIDE EXPIRED 02/01/26, REQUIRES REPLACEMENT. R & R L2 SLIDE RAFT IAW AMM 25-62-44-400-007-A.SDR CALA2026021213740Girt Bar · looseGIRT BAR AT R1 DOOR IS LOOSE, SECURED THE R1 GIRT BAR. OK TO CONTINUE. IAW AMM 25-66-01.SDR CALA2026021213739Indicator · out of alignmentR1 DOOR SLIDE LIGHT NOT ILLUMINATING WITH DOOR CLOSED, & ARMED MANUALLY. ALIGNED INDICATOR UNIT TO RESET CONTACT POSITIONS, INDICATOR NOW ILLUMINATES NORMALLY WITH THE ACTUATION OF THE ARM/DISARM LEVER, NO DAMAGE FOUND AT THIS TIME.SDR CALA2026021213737Battery Pack · inoperativeEMERGENCY SIDEWALL LIGHT AT 2R AFT DOOR INOPERATIVE. CONFIRMED. R & R THE BATTERY PACK IAW 33-51-06-960-802, CHKD OK.SDR CALA2026021213736Light · damagedEMERGENCY LIGHT, OPS TESTED WITH THE TEST SWITCH PROCEDURE. ROW 1 FWD EMERGENCY LIGHT IS RECESSED INTO SEAT SHROUD. REPLACED THE EMERGENCY LIGHT ASSY, OPS CHKD GOOD IAW AMM 33-51-11-003-032.SDR CALA2026021213735Battery Pack · inoperativeEMERGENCY CELLING LIGHT AT THE L3 DOOR INOPERATIVE, CONFIRMED. R & R THE PACK BATTERY IAW 33-51-06-960-802, CHKD OK.SDR CALA2026021213734Lamp · inoperativeAN EMERGENCY LIGHT OPS TEST WITH THE TEST SWITCH PROCEDURE, FLT DECK EMERGENCY LIGHT INOPERATIVE, REPLACED THE LAMPS, OPS CHKD GOOD IAW AMM 33-51-09-033-001.SDR CALA2026021213724Attach Angle · crackedFOUND A CRACK ON THE FWD CARGO ATTACH ANGLE AT S26L, BS 500I BULKHEAD AFT FACE. REMOVED AND REPLACED THE CARGO ATTACH ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A9873.SDR CALA2026021213723Floorbeam · corrodedFOUND CORROSION ON THE FLOORBEAM AT BS 333.40, BL 0, SEE BAM N/R 003182031 FOR WORK PERFORMED.SDR CALA2026021213722Elec Connector · disconnectedL2 DOOR EMERGENCY LIGHT DID NOT TEST, FOUND CONNECTOR 7245VC DISCONNECTED ENTIRELY IAW AIPC 24-92-04-46M, ITEMS 10, AND 20, AWM 33-51-03 PAGE 8, AND ESPM 20-44-29-01. RECONNECTED & OPS CHECKED PERFORMED IAW AMM 31-51-00-710-007-A. OPS CHKD NORMAL.SDR 2026F00010Avionics Unit · degradedDURING THE DOCKING PHASE OF FLIGHT, THE FRONT LEFT HAND BOOM ARM ON AIRCRAFT P2-ZIP-642 FRACTURED UPON IMPACT WITH THE DOCK, RESULTING IN AN AUTO-DOCK IN A DEGRADED HOVER MODE. THE AIRCRAFT RECOVERED WITHOUT FURTHER INCIDENT. REVIEW OF FLIGHT TELEMETRY IDENTISDR SWAA2026021169785Unknown · odorVERY STRONG BURNING METAL ODOR IN THE AFT GALLEY, NO SMOKE. COFFEE POT WAS NOT ON. ODOR CAME ON STRONG & THEN DECREASED. PERFORMED AN INSPECTION IAW AMM 05-51-56, AND FIM 21-00-806. NO DEFECT OR ODOR NOTED. SUSPECT FLIGHT PATH OVER KNOW EVERGLADES FIRE TO SDR SWAA2026021169686Nut · looseFWD SERVICE DOOR ASSIST HANDLE LOOSE. R & R THE LOWER NUT ON THE ASSIST HANDLE IAW AMM 52-41-31-400-802-NG.SDR SWAA2026021169698Retainer · looseFWD ENTRY DOOR SLIDE GIRT BAR, AFT CLIP LOOSE. SECURED THE GIRT BAR AFT CLIP IAW SRM 51-40-02.SDR FDEA202602110175Lamp · inoperativeNO SLIDE LIGHT ON L1 DOOR DURING ARMING PROCEDURE. RELAMPED SLIDE INDICATION ON L1 DOOR OPS CK GOOD PER FIM 25-66-11 FT 802. ACFT OK FOR SERVICESDR FDEA202602110174Bulb · dimDURING MX PRE-FLIGHT FOUND R1 EMERGENCY EXIT SIGN DIM. REMOVED AND REPLACED 5 FAULTY BULBS AT THE R1 EMERGENCY EXIT SIGN IAW AMM 33-51-01-2 . OPS CHECK GOOD. ACFT OK FOR SERVICE.SDR FDEA202602110173Bulb · inoperativeDURING PRE-FLIGHT CHECK, FOUND CENTER OVERHEAD EMERGENCY EXIT IDENTIFIER SIGN DIM. AMM 33-51-01-2 FOUND CENTER OVERHEAD EMERGENCY EXIT SIGN HAS 14 FAULTY BULBS. REMOVED AND REPLACED 14 FAULTY BULBS AS PER ABOVE REF. OPS CHECK GOOD.SDR FDEA202602110172Bulb · inoperativeDURING PRE-FLIGHT FOUND L1 OVERHEAD EMERGENCY EXIT SIGN SLIGHTLY DIM. AMM 33-51-01-2 FOUND L1 OVERHEAD EMERGENCY EXIT SIGN HAS 5 FAULTY BULBS. REMOVED AND REPLACED 5 FAULTY BULBS AS PER ABOVE REF. OPS CHECKED GOOD.SDR FDEA202602110171Flex Line · leakingON APPROACH EXTENDING MLG & FLAPS TO 20, LT HYD QTY EICAS & COMPLETE LOSS OF LT SYS HYD FLUID. MAINTAINED CONFIGURATION & COMPLETED LT HYD QTY QRH PROCEDURE PRIOR TO LANDING. EMERGENCY DECLARED AMM 12-12-01, AMM 29-11-17-4 , FOUND FLEX LINE CONNECTED TO SWISDR 2026F00009Slide · unwanted deployDURING MAINTENANCE ACTIVITY, RH OVERWING SLIDE WAS INADVERTENTLY DEPLOYED. SLIDE DEPLOYED NORMALLY BUT DEFLATED COMPLETELY WITHIN 5 MINUTES OF DEPLOYMENT. UNIT WAS MANUFACTURED ON NOV 2017 AND HAD BEEN OVERHAULED ON 02/11/2023 BY MEL AVIATION UNDER WO 454-923/SDR AALA202602113670Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: RIGHT AFT PASSENGER / CREW DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.SDR YENA2026021100167Unknown · odorFLT 2220 (8613), LHR - JFK. F/A REPORTED DIRTY SOCK ODOR ON DESCENT IN REAR GALLEY. COMPLIED WITH INFORMATION NOTICE 2017-T015, STEP 1. ISOLATED FAULT TO TYPE 10. HIGH COFFEE BURNING SCENT IN THE AFT GALLEY. COFFEEMAKERS & HOT PLATE CLEANED. ALSO PERFORMEDSDR QXEA2026021100030Throttle · malfunctionedFLIGHT 2460. ON FINAL AT 2000 FT AIRCRAFT WENT INTO GO AROUND MODE UNCOMMANDED. LANDED UNEVENTFULLY. REMOVED FROM SERVICE. REMOVED AND REPLACED THRUST CONTROL QUADRANT WITH NEW PART FROM STOCK IAW AMM 76-11-01-000-801-A, 76-11-01-400-801-A. OPS CHECK GOOD. A/CSDR DALA2026021100963Oil System · leakingRETURNED TO SEA DUE TO STRONG OIL ODOR IN THE CABIN AND FLIGHT DECK. TROUBLESHOT LT & RT ENGINES, PERFORMED OIL DECONTAMINATION, FOUND OIL LEAKING FROM APU GEN HOUSING, DEFERRED APU PER MEL 49-11-01. (8445066)SDR DALA2026083104895Plug · corrodedCORROSION ON FASTENER HOLE C1 OF RT WINGLET ADAPTER PLUG. REPAIRED PER PRI/ER/A 632062-14 (1445360)(AIRCRFT GROUNDED)SDR REXA2026080301414Track · corrodedCORROSION ON RAILS ON FWD CARGO COMPARTMENT 10E/AÏ¿½S RAILS (2EAS P/N: DSY7058-5) WERE REPLACED AND VERIFIED PER CRJ-700 IPC: 52-51-02-01 ITEM: 250, RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21615 REV. IR., RAILS (2EAS P/N: DSY7058-SDR REXA2026080301413Track · corrodedCORROSION ON RAILS ON FWD CARGO COMPARTMENT 10E/AÏ¿½S RAILS (2EAS P/N: DSY7058-5) WERE REPLACED AND VERIFIED PER CRJ-700 IPC: 52-51-02-01 ITEM: 250, RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21615 REV. IR., RAILS (2EAS P/N: DSY7058-SDR REXA2026080301412Track · corrodedCORROSION ON RAILS ON FWD CARGO COMPARTMENT 10E/AÏ¿½S RAILS (2EAS P/N: DSY7058-5) WERE REPLACED AND VERIFIED PER CRJ-700 IPC: 52-51-02-01 ITEM: 250, RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21615 REV. IR., RAILS (2EAS P/N: DSY7058-SDR REXA2026080301411Hinge · corrodedCORROSION ON HINGE FWD/MID/AFT (3EAS), ALSO DEGRADED PAINT OF STEP PLATE AT AFT CARGO COMPARTMENT HINGE MID (P/N: MM670-35623-003) OF STEP PLATE AT AFT CARGO COMPARTMENT WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01, HINGE FWD (P/N: MM670-35622-003) WAS FSDR REXA2026080301410Hinge · corrodedCORROSION ON HINGE FWD/MID/AFT (3EAS), ALSO DEGRADED PAINT OF STEP PLATE AT AFT CARGO COMPARTMENT HINGE MID (P/N: MM670-35623-003) OF STEP PLATE AT AFT CARGO COMPARTMENT WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01, HINGE FWD (P/N: MM670-35622-003) WAS FSDR REXA2026080301409Hinge · corrodedCORROSION ON HINGE FWD/MID/AFT (3EAS), ALSO DEGRADED PAINT OF STEP PLATE AT AFT CARGO COMPARTMENT HINGE MID (P/N: MM670-35623-003) OF STEP PLATE AT AFT CARGO COMPARTMENT WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01, HINGE FWD (P/N: MM670-35622-003) WAS FSDR REXA2026080301404Seal Rest · corrodedINITIAL INSPECTION: CORROSION ON AFT BAGGAGE BAY DOOR SEAL REST BTW FS1000.00 TO FS1047.00 AND LBL 43 APROX. CORROSION ON AFT BAGGAGE BAY DOOR SEAL REST BTW FS1000.00 TO FS1047.00 AND LBL 43 APROX WAS EVALUATED OUT LIMITS PER CRJ700 SRM 53-61-23-101-001-A01 THSDR REXA2026080301387Plate · crackedCRACK ON SUPPORT PANEL OF RH SIDE CONSOLE AT FLIGHT COMPARTMENT. SUPPORT PANEL OF RH SIDE CONSOLE AT FLIGHT COMPARTMENT WAS REPAIRED PER EA CRJ725-21690 REV. IRSDR DXTA2026021306860Fairing · damagedHIT A HERD OF DEER JUST PRIOR TO V1, AIRCRAFT NEEDS INSPECTION FOR ANY DAMAGE. BELLY FAIRING FRAME 6 AND BELLY FAIRING C CHANNEL. DAMAGE TO THE LT MLG DOOR. THE DOOR ROD IS BENT. THE RIVETS ATTACHING THE FWD HINGE PLATE ASSEMBLY FOR THE LT GEAR DOOR TO THE AISDR SWIA2026021076078Stringer · corrodedCORROSION FOUND ON STR 18R FROM FS 477 - FS 629. REPAIRED STR 18R FROM FS477 TO FS 629 REF DWG# SH690-33101 REV:M AND SRM 51-42-06-001-001-A01; 53-00-03-201-001-A02 REV:38 DATE: JUL 25/2020. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY AND FORM M-33SDR SWAA2026021305581Battery · inoperativeCREW REPORTS AFT OUTBOARD EMERGENCY FLASHLIGHT INOP<[01] OK TO CONTINUE PER MEL 25-64-02A SP1B. REMOVED AND REPLACED FLASHLIGHT AND BATTERY IAW AMM 25-64-00-900-805 REMOVED AND REPLACED FLASHLIGHT AND BATTERY IAW B737-MAX AMM 25-64-00-900-805-MAX<BR>PO# 114SDR AALA202604241668Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N2 FR 36. CRACK L= 0.530 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOOR BEAM Y765 VERTICAL STRINGER #2 AT FR 36 SDR AALA202604226871Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N3 FR 36. CRACK L= 0.550 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM Y254 VERTICAL STRINGER #3 AT FR 36 IAW