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 DALA2026061603602Battery · inoperativeM1673 BATTERY INOPERATIVE. R & R M1673 BATTERY PER B737 AMM 33-51. OPS CHECK GOOD. (LOG 8366906 - AIRCRAFT WAS GROUNDED).SDR HNAA2026061600501Dau · faultedNR 2 BLEED VALVE CLOSED AFTER TAKEOFF, MSG CLEARED AFTER LANDING. R & R DAU NR 1 & 2 IAW AMM 31-41-01-04. INSPECTED FUEL QTY INDICATION HARNESS IAW AMM 28-41-00. NO DEFECTS NOTED. PERFORMED EICAS OPS CHECK IAW AMM 31-41-00. OPS CHECK GOOD. PERFORMED AIR BLEEDSDR IXXA20260613051Cradle · brokenCENTER AISLE STAND EMERGENCY FLASHLIGHT HOLDER BOTTOM BROKEN. PLACED ON DEFERRAL 74109 MINIMUM EQUIPMENT LIST CATEGORY C PER ATI-25-63-04-01. DUE 23 JUNE 2026. REMOVED AND REPLACED CENTER AISLE STAND EMERGENCY FLASHLIGHT HOLDER IN ACCORDANCE WITH B767 SRM 51-4SDR DXTA2026061608432Pcb · faultyAMBER CAS MESSAGE CABIN DOOR OPEN AND ASSOCIATED CHECK DOORS CAME ON AT CRUISE 39000. RAN QRH AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CED MONITOR PCB NC105, REF MM 24-60-40. PERFORMED SUCCESSFUL CABIN DOOR LATCHING/LOCKING SYSTEM AND CABIN DOOR WARSDR DXTA2026061608430Seal · leakingMAIN DOOR WAS MAKING A LOUD NOISES ON APPROACH INTO MORRISTOWN. PASSENGERS AND FLIGHT ATTENDANT NOTICE IT. NO NOISE ON TAKEOFF. REMOVED MAIN CABIN ENTRY DOOR SEAL & INSTALLED NEW MAIN CABIN ENTRY DOOR SEAL IAW CL350 52-11-28. ALL OPS AND LEAK CHECKS GOOD.SDR I5PA2026061375703Gcu · inoperativeRIGHT BUSS TIE TRIPS WHEN POWER TRANSFERED. R & R RT GCU IAW AMM, OPS CHECKED NORMAL.SDR IPXA2026061551590Pawl · inoperativeYELLOW ARM HANDLE ON ENTRY DOOR DOES NOT WORK. REPLACED PAWL MECHANISM ON CREW ENTRY DOOR IAW AMM 52-11-26. OPS CHECKED OK.SDR FDEA202606130735Fseu · faultedEMERGENCY DECLARED FOR TE FLAP ASYM DISCREPANCY. AMM: 27-51-01-4 LAST FLIGHT FAULT: 27-51102. PERFORMED L, C, R FSPM BITE IAW 767 FIM 27-58 FAULT TREE 804, TESTS OK. PERFORMED GVI AND RIG CHECK WITH RIG PIN OF NR 1 AND 8 FLAP POSITION TRANSMITTER IAW AMM 27SDR FDEA202606130732Transponder · failedTRANSPONDER WAS SMOKING AND SHOWED FAILED. VERIFIED AND CONFIRMED THAT THE ATC PANEL FAILED AND THE SMOKING WAS CONFINED TO THE PANEL ITSELF. VERIFIED NO ASSOCIATED CIRCUIT BREAKERS POPPED. WIRING AND ELCTRICAL CONNECTORS THE ATC PANEL VISUALLY INSPECTEDSDR 3J7R0615202600001Lamp · failedEXTERIOR WINDOW EMERGENCY EXTT LAMP WILL NOT ILLUMINATE.SINGLE LAMP IS AFT OF THE EMER WINDOW EXITSDR DALA2026061503578Bottle · low pressureL3 DOOR ASSIST LOW. CORRECTIVE ACTION: SERVICED DOOR ASSIST BOTTLE PER A330 AMM 52-15. (8747146) AIRCRAFT WAS GROUNDED.SDR DALA2026061503576Wire · disconnectedSEAT 35AB EMERGENCY LIGHT INOP. RECONNECTED WIRE PER A330 AMM 33-51. OK FOR SERVICE. (8320947) AIRCRAFT WAS GROUNDED.SDR AALA202606150492Circuit Breaker · pulledAIRCRAFT WAS GROUNDED: ALL THREE LAVS ON AIRCRAFT WILL NOT FLUSH. VACUUM BLOWER PREVIOUSLY REPLACED ON JUN 14. REPORTED NO HELP. PIREP VACUUM TOILET SYSTEM NOT WORKING ABOVE 16000 FT. TROUBLESHOOTING FOUND C/B C11 ON P-91 PANEL OPEN AND COLLARED. PER TROUBLSDR AALA202606152795Elec Connector · inoperativeAIRCRAFT IN BASE MAINTENANCE: PAX OXY SYS DROP TEST FOUND SEAT 5 DH OXY CONTAINER DOOR ACTUATOR NOT ACTIVATED. PAX OXY SYSTEM ELECTRICAL CONNECTOR DM33232B REPLACED AND PAX OXY SYSTEM DROP TEST RESULT NORMAL, SEAT 5DH OXY CONTAINER DOOR OPENED IAW AMM 35-21-0SDR AALA202606156465Transmitter · inoperativeAIRCRAFT WAS GROUNDED: FLAPS WOULD NOT EXTEND PAST 1 WITH HANDLE IN 5,10,15 POSITION. DID ALTERNATE FLAP EXTENSION TO GET FLAPS TO 15 FOR NORMAL LANDING. EMERGENCY WAS DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LH FLAP POSITION TRANSMITTER IAW SDR AALA202606156232Flashlight · not seatedAIRCRAFT WAS NOT GROUNDED: L1 FORWARD ENTRY FLIGHT ATTENDANT FLASHLIGHT INOP. MAINTENANCE RESEATED FLASHLIGHT PER AMM 25-64-00.SDR AALA202606150439Potable Water · emptyAIRCRAFT WAS GROUNDED: FA NOTIFIED FLIGHT DECK THEY HAD ZERO POTABLE WATER UPON REACHING CRUISE. I HAD THEM TRY TO FLUSH TOILETS AND USE SINK, STILL ZERO WATER AVAILABLE. ALSO ZERO WATER AVAILABLE IN EITHER GALLEY. DECESION MADE TO RETURN TO CLT EMERGENCY DECLSDR DALA2026061503572Floor Support · corroded(UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON FLOOR STRINGERS (ATTACH POINTS) 2.9, 7.55,RBL AND BTW BS 1320 TO BS 1340 OF FLOOR STRUCTURE AT AFT CARGO COMPARTMENT, AREA IT IS OUT LIMITS PER SRM 53-00-53-1A PROCEDURE 1, DETAIL III, NOTE C (DETAIL VII); AND B75SDR SIMA20260613001Flap System · malfunctionedFLAP FAIL ON APPROACH TO LANDING, WHEN SELECTING FLAPS 2. FINAL SETTING ACHIEVED WAS SLATS 3 FLAP 1 (EMERG DECLARED) FLAP FAIL ON APPROACH TO LANDING. FAULT CODE 27512014ACE . FOUND LH L4 FLAP ACTUATOR TRIP INDICATOR TRIPPED. COMPLIED WITH ETN-EJ-27-012. PERFOSDR DXTA2026061508426Warning Message · false activationDURING TAXI OUT WE RECEIVED A VENTRAL RUDDER FAIL CAS FOLLOWED BY AP FAIL AND YD FAIL. WHEN WE STOPPED TAXIING, ALL MESSAGES DISAPPEARED. WHEN WE STARTED TO TAXI AGAIN, THEY IMMEDIATELY CAME BACK. CORRECTIVE ACTION: POWERED ON AND NO CAS MESSAGE PRESENTED. PERSDR DXTA2026061508434Light · malfunctionedEMER LIGHTS BY THE EMERGENCY EXIT AND EXTERIOR ARE INOP. EMER LIGHTS BY THE MAIN CABIN DOOR ARE STILL WORKING PROPERLY. ARRIVED AT AIRCRAFT, PERFORMED OPS CHECK OF EXTERIOR AND INTERIOR EMER LIGHTS. OPS CHECK GOOD. STARTED APU AND CHARGE THE EMERGENCY BATTERSDR CALA2026061517095Support Bracket · crackedDURING OK TO INSTALL R2 DOOR OPENING MECHANISM ACCESS DOOR 232AR, FOUND UPPER SUPPORT BRACKET CRACKED REMOVED, FABRICATED, INSTALLED 143N8313-63 IAW REF DWG 143N8313- 63 AND SRM 51-40-05, 51-40-0 2-0G.SDR CALA2026061517075Engine · bird ingestionENG NR 2 SHOWS SIGN OF BIRD STRIKE. COMPLETED BIRD STRIKE INSP IAW AMM REF 05-51-14-200-803-A AND 72-00-00-210-807-A. NO BIRD STRIKE DAMAGE. NO PILOT REPORTS OF SMELL OR STALLS. DEBRIS CLEANED. READY FOR SERVICES.SDR SCNA20260615247Bracket · corrodedAFTER REMOVAL FLOOR MOUNTED ESCAPE SLIDE BRACKETS, BRACKETS (8 EAS) WAS FOUND WITH CORROSION. REPLACED AND VERIFIED PER B737-800 AIPC 25-66-02-01 AND B737-800 AIPC 25-66-02-02SDR DALA2026061503568Pump · failedDUE TO GREEN HYDRAULIC SYSTEM AIR PRESSURE LOW ECAM MSG. REPLACED NR 1 AND NR 2 GREEN SYSTEM EDP'S AND SEALS AND FLUSHED HYDRAULIC SYSTEM. ALSO REPLACED GREEN AIR PRESSURIZATION UNIT. OK FOR SERVICE. (8317802)SDR AALA202606153948Power Supply · inoperativeAIRCRAFT IN BASE MAINTENANCE: AFT EXTERIOR EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY PER AMM 33-51-06.SDR AALA202606159599Power Supply · inoperativeAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND OVERWING EMERGENCY EXIT SIGN LIGHTS ARE INOPERATIVE. REPLACED POWER SUPPLY PER AMM 33-51-06.SDR DALA2026061503564Computer · faultedBOTH ENGINES RUNNING, REJECTED TAKEOFF DUE TO ELAC 1 PITCH FAULT MESSAGE AT 10 KNOTS. DUE TO HISTORY - APPLING ELAC 1 TO MEL & PLAC PER A319/320/321 MEL 27-93-01. M PROC C/W, MCC NOTIFIED. (LP: 8778668, AIRCRAFT WAS GROUNDED)SDR 2026FA0000517Bearing · improper partENGINE REMOVED FOR INSPECTION DUE TO LOW OIL PRESSURE. ON DISASSEMBLY DISCOVERED .020 UNDERSIZE CRANKSHAFT RUNNING IN .010 BEARINGS.SDR DALA2026061403561Oil System · leakingDIVERTED DUE TO RIGHT ENGINE OIL LOSS. CREW SHUT ENGINE DOWN AND DECLARED EMERGENCY. REPLACED NR 2 ENGINE. (LP 8052232 - AIRCRAFT WAS GROUNDED)SDR SWIA2026061277632Floorbeam · crackedCRACK FOUND ON THE RT SIDE INBD COCKPIT FLOORBEAM UNDER ACCESS PANEL 132AR. REMOVED THE DAMAGE FROM COCKPIT FLOORBEAM RBL 12. COMPLIED WITH ALL STEPS OF REO 690-53-11-2214, REV-, COMPILED WITH 51-900-1002-SKY.SDR 2026FA0000729Stiffener · crackedL/H WING FWD LWR I/B SKIN, TOP AFT STIFFENER CRACKED. REPLACED WITH NEWSDR 2026FA0000708Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITHNEWSDR SWIA2026061276983Skin · dentedTHERE IS A DENT ON THE PAX DOOR AT APPROX BS 333, STRINGER 7. FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICES AND/OR PROCEDURES. COMPLETED REPAIR WITH REO 601R-52-10-917.SDR SWIA2026061276979Skin · dentedADM# N982SW-9157THERE IS A DENT ON THE PAX DOOR AT APPROXIMATELY 15€Œ FWD OF TRAILING EDGE OF THE MCD AND 15€? DOWN FROM THE TOP EDGE OF THE MCD. COMPLETED REPAIR WITH REO: 601R-52-10-917SDR SWIA2026061276976Skin · dentedADM# N982SW-9158THERE IS A DENT ON THE PAX DOOR AT APPROXIMATELY 12€? AFT OF THE LEADING EDGE OF THE MCD AND 15€? DOWN FROM THE TOP EDGE OF THE MCD. COMPLETED REPAIR WITH REO: 601R-52-10-917SDR REXA2026082601735Fitting · wornINITIAL INSPECTION: WEAR ON LH/RH SIDE STAY FITTING IN MAIN WHEEL WELL AREA. LH/RH SIDE STAY FITTING IN MAIN WHEEL WELL AREA WERE BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE REPAIRED PER EA CRJ953-22582 REV IR AND EA CRJ953-22583 REV IRSDR REXA2026082601699Web · crackedCRACK ON FLOOR WEB RIGHT SIDE AT ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS 193.00. FLOOR WEB RIGHT SIDE (REPAIR DOUBLER) AT ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS 193.00 WAS REPLACED PER CRJ900 SRM 53-11-43-201-001-A01.SDR REXA2026082601661Support Bracket · crackedCRACK ON BRACKET SUPPORT OF JB6 AT FWD EQUIPMENT COMPARTMENT BRACKET SUPPORT OF JB6 AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01SDR REXA2026082601660Hinge · crackedFWD LAV SERVICE DOOR UPPER HINGE WONT LOCK AND CRACKED FWD LAV SERVICE DOOR UPPER HINGE WAS REPLACED PER CRJ 900 AMM 52-45-17 & SRM 51-42-21-001-001-A01SDR REXA2026082601654Drag Angle · crackedCRACKED AFT DRAG ANGLE AT LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. AFT DRAG ANGLE AT LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ900 SRMSDR REXA2026082601653Drag Angle · crackedCRACKED AFT DRAG ANGLE AT RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. AFT DRAG ANGLE AT RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ900 SRMSDR SWIA2026061276787Retainer · bentPAX DOOR BOTTOM RETAINER SEAL, IT IS BENT AND THE FASTENERS ARE CORRODED. REMOVED AND INSTALLED NEW PAX DOOR BOTTOM RETAINER SEAL IAW SRM 51-42-06-001-001-A01, & DWG 601R31702, REV N. PERFORMED PRESSURE LEAK CHECK OF PAX DOOR IAW AMM 52-00-00-790-801 A01. SDR REXA2026073001322Skin Splice · corrodedCORROSION ON INTERNAL SKIN SPLICE AT FS 280.00 TO FS 282.00 FROM STGR 24RH TO 26LH CORROSION ON INTERNAL SKIN SPLICE AT FS 280.00 TO FS 282.00 FROM STGR 24RH TO 26LH WAS REMOVED PER CRJ-900 SRM SRM 51-21-06-001-001-A01 EVALUATED BTW FS 280.00 TO FS 282.00 FROMSDR SWAA2026061511911Starter Gen · failedDURING PUSH, AFTER ENGINE START, AUDIBLE POP, POWER LOSS, & SMOKE ODOR IN COCKPIT & AFT GALLEY. CREW REPORTED ACFT WAS STILL ON APU GEN AT THE TIME OF POWER LOSS. INSPECTED APU GENERATOR AND FOUND DAMAGE & MELTED PLASTIC AT TERMINAL BOX. R & R APU STARTER SDR SWAA2026061511618Switch · faultySTAB OUT OF TRIM LIGHT ILLUMINATED ON DESCENT. RAN QRH AND STABLIZER DID NOT RESPOND TO ELECTRIC TRIM IMPUTS. RAN STAB TRIM INOP QRH. MANUAL STAB TRIM OPS NORMALLY. R & R STAB TRIM NOSE DOWN LIMIT SWITCH S145. COMPLETED STEPS (A) THRU (E)(1)(C) IAW AMM 27-41SDR SWAA2026061512469Trim Motor · faultySTAB OUT OF TRIM LIGHT ILLUMINATED ON DESCENT. RAN QRH & STABLIZER DID NOT RESPOND TO ELECTRIC TRIM IMPUTS. RAN STAB TRIM INOP QRH. MANUAL STAB TRIM OPS NORMALLY. R & R STAB TRIM NOSE DOWN LIMIT SWITCH S145. COMPLETED STEPS (A) THRU (E)(1)(C) IAW AMM 27-41SDR SWAA2026061511606Fuse · inoperativeFWD SLIDE EMERGENCY LIGHT NEAR L1 DOOR IS INOPERATIVE. R & R FWD SLIDE EMERGENCY LIGHT PACK ASSY FUSES IAW SWPM 20-91-00. WIRE W3142-01111-16 FOUND TO BE CHAFED. REPAIRED AND SPLICED WIRE BETWEEN CONNECTOR D0096P AND D11074 IAW WDM 33-51-12 AND SWPM 20-10-13.SDR SWAA2026061512470Wire · chafedFWD SLIDE EMERGENCY LIGHT NEAR L1 DOOR IS INOPERATIVE. R & R FWD SLIDE EMERGENCY LIGHT PACK ASSY FUSES IAW SWPM 20-91-00. WIRE W3142-01111-16, FOUND TO BE CHAFED. REPAIRED AND SPLICED WIRE BETWEEN CONNECTOR D0096P AND D11074 IAW WDM 33-51-12 AND SWPM 20-10-1SDR SWAA2026061511712Lamp · inoperativeAFT GALLEY OVERHEAD EMERG EXIT SIGN F/O SIDE 4 LOWER LIGHTS INOPERATIVE. RELAMPED IAW AMM 33-51-01 OPS CHECKED GOOD. ACFT OK FOR SERVICE.