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 IXXA202607109058Life Vest · tornRIGHT SUPERNUMERARY SEAT LIFE VEST BAG TORN OPEN. PLACED ON DEFERRAL 74891 MINIMUM EQUIPMENT LIST CATEGORY D PER ATI-25-25-03-01. DUE 06 NOVEMBER 2026SDR IXXA202607109057Life Vest · missingFIRST OBSERVER SEAT LIFE VEST MISSING. PLACED ON DEFERRAL 74890 MINIMUM EQUIPMENT LIST CATEGORY A PER ATI-25-11-02-01. INSTALLED FIRST OBSERVER SEAT LIFE VEST IN ACCORDANCE WITH AMM 25-62-00.SDR AALA202607106270Elec Connector · no testAIRCRAFT WAS NOT GROUNDED: ON PS CHECK FOUND SEAT 4D EMERGENCY LIGHT AFT SIDE INOP. MAINTENANCE FOUND CONNECTOR LOOSE AT SEAT 4D RE SECURED CONNECTION FOR SEAT 4D AFT EMERGENCY PROXIMETY LIGHT IAW AMM 33-51-05.SDR AALA202607108945Power Supply · faultedAIRCRAFT WAS NOT GROUNDED: DURING EMERGENCY LIGHT TEST PER PS CK FOUND POWER SUPPLY M33424 AT 1L OVERDOOR PANEL FAULTY. MAINTENANCE REPLACED POWER SUPPLY M33424 AT 1L OVERDOOR PANEL IAW AMM 33-51-06.SDR AALA202607107336Flashlight · inoperativeAIRCRAFT WAS NOT GROUNDED: FED FLIGHT ATTENDANT STATION FLASHLIGHT BLINKING RED. MAINTENANCE REPLACED FWD OUTBOARD F/A FLASHLIGHT. OPS CK OK.SDR AALA202607104228Light · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT SIGN BY FWD FLIGHT ATTENDANT SEAT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT FWD FLIGHT ATTENDANT SEAT IAW AMM 33-51-02.SDR DALA2026071004047Retainer · wornSHIP 9576 WEAR ON INTERNAL/EXTERNAL PAN AND SEAL RETAINERS AT FWD LOWER CORNER OF AFT CARGO DOOR, CORRECTIVE ACTION: COMPLIED WITH ER/A 633377-14. (1690771) (AIRCRAFT GROUNDED).SDR SIMA202607109001Light · inoperativeAFT SERVICE DOOR LOWER EMERGENCY EXIT LIGHT INOPERATIVE. R & R NR 4 ELPU IAW AMM 33-50-01. OPC GOOD.SDR SIMA202607109002Light · fadedFRONT RIGHT CABIN EMERGENCY PHOTOLUMINESCENT STRIP FADED DOES NOT ILLUMINATE. DEFERRED PER MEL 33-32 AUTH 070527-C. PENDING CORRECTIVE ACTIONSDR CALA2026071017669Bracket · corrodedCORRODED BRACKET AT BS 500H AND NEAR STR 23L. REMOVED AND REPLACED BRACKET AT BS 500H AND NEAR STR 23L. IAW SRM 53-00-07-1A-1, SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, AND AIPC 38-31-51-17.SDR CALA2026071017667Floor Support · corrodedPOSSIBLE CORROSION ON FLOOR SUPPORT BTW STA 312 TO 328 LBL 11. REMOVED AND LOCATED, DRILLED AND INTALLED NEW INTERCOSTAL ON FLOOR SUPPORT BTW STA 312 TO 328 LBL 11. IAW SRM 51-40-02-0G-0, SRM 51-40-08-0G-0, AMM 51-21-41-370-802 AND AMM 51-21-72-370-804.SDR CALA2026071017665Intercostal · corrodedPOSSIBLE CORROSION ON INTERCOSTAL BTW BS 312 TO 328, LBL 45. REMOVED AND LOCATED, DRILLED, AND INTALLED NEW INTERCOSTAL ON FLOOR SUPPORT BTW BS 312 - 328, LBL 45. IAW SRM 51-40-02-0G-0, SRM 51-40-08-0G-0, AMM 51-21-41-370-802, & AMM 51-21-72-370-804.SDR CALA2026071017663Intercostal · corrodedAFT WET AREA INTERCOSTAL BETWEEN STA 947.5 AND 967 AT RBL 51.5 WITH POSSIBLE CORROSION. COMPLETED INSTALL INTERCOSTAL OM STA 947.5 AT RBL 51.5 ALL WORK DONE ON WC# 3502888-1000-0040 ATTACHED REFERENCE.(SDR CALA2026071017661Support · corrodedAFT WET AREA Z SUPPORT P/N 147A5710-1 WITH POSSIBLE CORROSION AT BS 1006 BETWEEN LBL 32 AND LBL 42. LOCATED, DRILLED, COUNTRSINK AND INSTALLED ZEE SUPPORT ON AFT WET AREA BS 986.5 TO 1006, LBL 32 AND 42 IAW SRM-51-40-05-0G-0,-0, SRM-51-40-08-0G-0, SRM-51-40SDR CALA2026071017658Control Panel · faultedAUTO THROTTLE FAIL AUTO PILOT WILL NOT MODE CONTROL HOT TO TOUCH INTERVIEWED CREW. AUTOPILOT KICKED OFF & MODE CONTROL PANEL WAS VERY HOT TO TOUCH. BURNED 1ST OFFICER'S THUMB. ALSO NOTED FAINT BURNING ODOR WHEN ENTERING COCKPIT. REPLACED MODE CONTROL PANELSDR CALA2026071017656Support Bracket · damagedWINDOW HEAT FWD LT SIDE. SPARKS WERE SEEN IN COCKPIT FOR 10 SECS ONCE IT HAPPENED. REMOVED GLARESHIELD, FOUND WIRES ARCING OFF FRAME. CAPT WINDOW HEAT POWER WIRE APPEARS TO HAVE BEEN PINCHED BETWEEN WINDOW & GLARE SHIELD BRACKET. WIRE INSULATION MELTED OFF.SDR CALA2026071017654Door Sill · corrodedAFT CARGO DOOR LOWER SILL HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED LOWER ENTRY DOOR SILL WEB AFT CARGO FROM RT SIDE BS 794 TO 847 IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, & 51-40-08-0G-0.SDR FDEA202607090881Floor Panel · damagedFIBERS BROKEN AT FLOOR PANEL 241KFF OF MAIN DECK CARGO COMPARTMENT FLOOR PANEL 241KFF OF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50- 2R PAR. 4-B FIG. 201 SHEET 2 REV. 94 DEC. 15/2025SDR FDEA202607090880Floor Panel · puncturedPUNCTURE AT FLOOR PANEL 241EFF OF MAIN DECK CARGO COMPARTMENT FLOOR PANEL 241EFF OF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50- 2R PAR. 4-B FIG. 201 SHEET 2 REV. 94 DEC. 15/2025SDR FDEA202607090879Floor Panel · damagedBROKEN FIBERS AT FLOOR PANEL 251KFF OF MAIN DECK CARGO COMPARTMENT FLOOR PANEL 251KFF OF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50- 2R PAR. 4-B FIG. 201 SHEET 2 REV. 94 DEC. 15/2025SDR FDEA202607090878Floor Panel · puncturedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 232MFF HAS PUNCTURE DAMAGE. JM25 REPAIRED FLOOR PANEL 232MFF (P/N:143T5876-128) AT APPROXIMATELY AT STA 654 22 THRU 654 88 BETWEEN RBL-55 AND RBL 77. USING B767 SRM 53-00-50-2R FIG. 201. REPAIR 1. SH 1. THIS IS A MAJSDR FDEA202607090877Light · damagedL1 DOOR EMERGENCY SLIDE LIGHT WILL NOT TEST. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT, IAW AMMM 33-51-06-2-1. LIGHT TESTED GOOD.SDR FDEA202607090876Floor Panel · puncturedFIVE PUNCTURES ON FLOOR PANEL 231AFF AT MDCC. THE FLOOR PANEL 231AFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2, PAR 4.B, FIG 201, SHEET 2, REV 94. DEC 15/2025.SDR FDEA202607090875Floor Panel · puncturedMAIN DECK CARGO COMPARTMENT, 232NFF HAS PUNCTURE DAMAGE.JM24. REPAIRD FLOOR PANEL 232NFF, RBL77-TO RBL 88 BS 654.22 TO 676 IAW SRM 53-00-50-2R, FIG 201, REPAIR 1, SHEET 2. MAJOR REPAIR. THIS FLOOR PANEL WAS REPAIRED ON AIRCRAFT.SDR FDEA202607090874Floor Panel · puncturedTHREE PUNCTURES ON FLOOR PANEL 232NFF AT MDCC FLOOR PANEL 232 NFF AT MDC WAS REPAIRED IAW SRM 53-00-50-2R, PAR. 4-B, FIG. 201, SHEET 2, REV 94 DEC 15/2025SDR FDEA202607090873Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231LFF AT MDCC FLOOR PANEL 231 LFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202607090872Floor Panel · dentedDENT WITH DELAMINATION ON FLOOR PANEL 242CFF AT MDCC FLOOR PANEL 242CFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201, SHEET 2, REV 94, DEC 15/2025.SDR FDEA202607090871Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231KFF AT MDCC FLOOR PANEL 231KFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV. 94 DEC 15/2025SDR FDEA202607090870Floor Panel · dentedDENT WITH DELAMINATION ON FLOOR PANEL 231LFF AT MDCC FLOOR PANEL 231LFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4-B FIG 201 SHEET 2 REV. 94 DEC 15/2025SDR DXTA2026071008770Light Sys · malfunctionedEMERGENCY LIGHTS REMAIN ILLUMINATED WITH THE EMERGENCY LIGHTS SWITCH IN THE ARM POSITION. THE FIRST TIME AFTER OPENING THE MAIN CABIN DOOR THEY EXTINGUISHED AND OPERATED NORMALLY. THE SECOND TIME THEY WOULD NOT EXTINGUISH UNTIL EMERGENCY LIGHTS SWITCH WAS PLACSDR O9IA202607090145Warning Message · false activationNUMEROUS IN FLIGHT L OR R BLEED LEAK CAS MESSAGES OVER THE PAST TWO YEARS. NOT ABLE TO REPRODUCE THEM ON THE GROUND OR DURING MAINT CHECK FLIGHTS. EVEN GETTING THIS WITH THE THROTTLES PULLED BACK AND NOT WHEN THERE IS POWER APPLIED. WE DO NOT FIND LEAKS DURINGSDR O9IA2026070900146Warning Message · false activationNUMEROUS IN FLIGHT L OR R BLEED LEAK CAS MESSAGES OVER THE PAST TWO YEARS. NOT ABLE TO REPRODUCE THEM ON THE GROUND OR DURING MAINT CHECK FLIGHTS. EVEN GETTING THIS WITH THE THROTTLES PULLED BACK AND NOT WHEN THERE IS POWER APPLIED. WE DO NOT FIND LEAKS DURISDR DALA2026070904034Skin · crackedCRACKS ON INTERNAL SKIN BTW STA Y= 760/770 AND BTW STA X= -45/-60 APPROX AT RT MLG DOOR, COMPLIED WITH ER/A 634942-14. (1689728) (AIRCRAFT GROUNDED).SDR IPXA2026070971659Controller · failedEMERGENCY DECLARED AT CRUISE 340, NR 2 A/C PACK FAILED, RAN ECAM NR 1 A/C PACK ALSO FAILED. INITIATED DESCENT TO 10,000 FT, DURING DESCENT BOTH PACKS INTERMITTENTLY WOULD OPERATE THEN FAIL. AT 10,000 FT, BOTH PACKS ARE OPERATING. REPLACED CONTROLLER 37HSDR QR9R2026070900001Sensor · fluctuatesGEN NR 1 FAILED DURING REFUEL, GENERATOR AMP NOT WITHIN FIVE. ERRATIC AMP FLUCTUATIONS DURING MTF OF 15 TO 20 AMP DIFFERENCE BETWEEN #1 AND #2 WITH #1 BEING THE FAULT SIDE. #2 WAS STABLE DURING FLIGHT AND VOLTAGE ON BOTH WERE 28.6 STEADY. REMOVED AND REPLACED SDR 37CA2026070900144Skid · corrodedCORROSION WAS IDENTIFIED IN THE SKID TUBE BUSHING AREA WHERE SKID SHOE THROUGH BOLTS ATTACH.SDR 37CA202607090143Skid · corrodedCORROSION WAS IDENTIFIED IN THE SKID TUBE BUSHING AREA WHERE SKID SHOE THROUGH BOLTS ATTACH.SDR ABXA20260709312Fire Warning · false activationCARGO FIRE B8 LIGHT ILLUMINATED ON CENTER CONSOLE. PERFORMED BITE PROCEDURE FOR THE CARGO COMPARTMENT SMOKE DETECTION SYSTEM. IAW IAI FIM 26-14-00. OPS CHECK GOOD. LIGHT IS CLEARED. A/C RETURNED TO SERVICE.SDR FDEA202607090869Skin · dentedWHILE ACCOMPLISHING CURRENT HEAVY MAINTENANCE CHECK AT IND, TECHNICIANS FOUND DENT AND GOUGE DAMAGE ON THE FUSELAGE SKIN AND ACCESS DOOR DOUBLER AT STA 308 NEAR RBL 10 AT THE E&E DOOR CUTOUT (SKIN) & 141T3222-1 (ACCESS DOOR DOUBLER)). THE DENT WAS MEASURED ASDR FDEA202607090868Skin · crackedWHILE ACCOMPLISHING CURRENT HEAVY MAINTENANCE CHECK AT IND, TECHNICIANS FOUND DENT AND GOUGE DAMAGE ON THE FUSELAGE SKIN AND ACCESS DOOR DOUBLER AT STA 308 NEAR RBL 10 AT THE E&E DOOR CUTOUT (P/N 141T3221-7 (SKIN) & 141T3222-1 (ACCESS DOOR DOUBLER)). THE DSDR DALA2026070904019Bottle · low pressureL3 DOOR ASSIST BOTTLE HAD LOW PRESSURE. REPLACED DIAPHRAGM AND SERVICED BOTTLE IAW AMM 52-15. (1689640) AIRCRAFT WAS GROUNDED.SDR 2026FA0000575Wire Harness · chafedDUAL ECU FAILURE ON LH ENGINE. EMERGENCY LANDING INTO KBMI. THE DOWNLOAD SHOWED, "PRESSURE CONTROL VALVE POWER FAILURE." WHEN GAINING ACCESS TO THE PRESSURE CONTROL VALVE, THE ENGINE CONTROL HARNESS WAS FOUND TO BE CHAFFING ON THE CYLINDER HEAD AND THE FUELSDR SWAA2026102887010Girt Bar · wornGIRT WORN REMOVED/REPLACED GIRT ASSY REF CMM 25-60-37.SDR SWAA2026102888082Girt Bar · wornGIRT WORN R&R GIRT ASSY PER CMM 25-60-37SDR SWIA2026070877622Retainer · crackedUPON REMOVAL OF PAX DOOR, AFT SUPPORT ANGLE FOUND CRACKED ON LOWER CORNER SEAL RETAINER. REPLACED AFT LOWER CORNER SEAL RETAINER WITH NEW IAW SRM 51-42-06-001-001-A01 AND DWG 601R31871, REV D. COMPLIED WITH 51-900-1002-SKY. LEAK CHECKED GOOD.SDR VNAA202610060033Hinge Fitting · mechanic errorMAINTENANCE ERROR: AFTER REMOVAL OF RH AILERON TOOL MARK ON R5 OF CENTER HINGE FITTING OF OUTB AILERON PCU. R5 OF CENTER HINGE FITTING OF OUTB AILERON PCU WAS REPAIRED PER REO 690-57-61-543 REV - -SDR VNAA202610060030Aileron · corrodedREF TO TRFKE00GTBX6. AFTER REMOVAL OF BEARING AND BUSHING ON RH AILERON CORROSION ON LUGS BORES: R2, R3, R4 AND R6 WAS FOUND AT CENTER HINGE FITTING AND UPPER/LOWER HOLES OF OUTB HINGE FITTING. LUGS BORES R4, R6 AT CENTER HINGE FITTING AND UPPER HOLE OF OUTB SDR 2026FA0000785Turbine Wheel · meltedTHE MENTIONED PART WAS SEND AS PIECE PART FROM THE CUSTOMER (DELTA) TO MTU BB FOR OVERHAUL. DURING THE INCOMING INSPECTION OF THE COMPONENT AN UNUSUAL FINDING WAS DETECTED IN THE AREA OF THE FIR-TREE PRESSURE FACE,- DEPOSITED MATERIAL/METAL EXHIBITING A MELTESDR IPXA2026082962661Plate · damagedNR 2 PYLON, LT SIDE, FROM FR 5 TO FR 7, METALLIC PLATE WITH TOOL DAMAGE, MULTIPLE RIVETS DAMAGE AND HOLES WITH EVIDENCE OF BE ELONGATED. INSTALLED NEW SPRING AND NEW EXTRUSION ON NR 2 PYLON INBD SIDE FROM FR 5 TO FR 7 IAW SRM 51-40-21-001 AND 54-56-10-001.SDR IPXA2026082562757Rub Strip · gougedNR 2 ENG, LT T/R, AFT RUB STRIP WITH MULTIPLE GOUGE. INSTALLED RUB STRIP P/N::221-6583-501/502 AT NR 2 ENG LT,T/R, AFT RUB STRIP IAW SRM 51-40-21-001 AND PART MARKED IAW GMM09-08.