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 CALA2026032614842Cover · missing20C CEILING EXIT LIGHT PATH INDICATOR COVER MISSING. REPLACED 20C CEILING LIGHT PATH LENS OPS CHECK GOOD REF AMM 33-51-03 SDR UPDATE LOG GRIPE REPORTED BY FLIGHT CREW FOR MISSING EXIT PATH LIGHT COVER.SDR CALA2026032614841Retainer · out of adjustR2 DOOR SLIDE COVER BRAKET LOOSE ON RIGHT SIDE FOR GIRT BAR SPOKE WITH PILOT AND F/A. WRITEUP FOR R1 DOOR. AFT GIRT BAR RETENTION CLIP LOOSE. ADJUSTED AS REQUIRED REF AMM 25-66-01-200-802. TENSION OK AT THIS TIME. OK FOR SERVICE. INSPECTED R2 GIRT BAR RETENTIOSDR CALA2026032614840Door · out of rigF/A FOUND THAT DOOR 2L ARM/DISARM HANDLE MOVED OUT 1 INCH DURING FLIGHT.NO ECAM MESSAGE. ITEM LOCKED TO CONFIRM FINDINGS EMERGENCY ESCAPE SLIDE REF AMM 52-10-00-720-005-A. AT 2 LEFT AT APPROX 6 LBF RELEASE MECHANISM HANDLE BEGINS TO MOVE. UNLOCKED FOR UPDATINGSDR CALA2026032614839Sensor · faultedFL LEADING EGDE TRANSIT AT FLAPS 10 LOCKED FOR CONFIRMED FAULT, DECLARED EMERGENCY DEBRIEFED CREW CA STATED. SELECTED 10 FLAPS, AMBER TRANSIT LIGHT ON. FOLLOWED REF GUIDE SELECTED FLAPS 15, AMBER LIGHT REMAINED ON. AFTER LANDING DURING TAXI TRANSIT LIGHT WENTSDR DALA2026032602016Apu · odorRAN APU WITHOUT BLEED FOR 8 MINUTES BEFORE TURNING ON BLEED WHEN BLEED TURNED ON DIRTY SOCKS SMELL STARTED, RAN WITH BLEED FOR ABOUT 1 MINUTE AND THE SMELL GOT STRONGER, TURNED BLEED OFF SMELL WENT AWAY. FLIGHT ATTENDANTS DID NOT SMELL IT BUT BOARDING DOOR WASSDR MAS2026F00004Battery · firePASSENGER AT SEAT 3D PORTABLE CHARGER CAUGHT FIRE/ PERFORMED AMM CHECK FOR SMOKE/ ABNORMAL SMELL NFDN. A/C OUTLET ON 3D HAS SCORCH MARKS NEEDS AN INSPECTION/ PLACED ON MEL. HALON FIRE EXTINGUISHER FWD WAS USED. R&R FWD FIRE EXTINGUISHER. CONTAINMENT BAG ANSDR MASA2026032500011Battery · firePASS BATT CAUGHT FIRE AT 3D/EMER DECLASDR EVGR20260325001Actuator · jammedPITCH TRIM WHEEL COULD ONLY BE MOVED WITHIN A VERY SMALL RANGE. MAINTENANCE INVESTIGATED AND FOUND THAT THE LH PITCH TRIM ACTUATOR WAS BOUND UP AND WOULD NOT ROTATE. THE ACTUATOR WAS REMOVED AND DISASSEMBLED IAW THE KODIAK 100 AMM CH. 2731.5.10 AND DAHER FIELSDR DALA2026032502001Light · damagedEMERGENCY LIGHT DAMAGED AT SEAT 19FED. R & R SEAT MOUNTED EMERGENCY LIGHT AT SEAT 19DEF PER AMM 33- 51. OPS CHK GOOD. (7214340)SDR MASA20260325032Seat Track · corrodedDURING HEQAVY CHECK INSPECTIONS ON FWD FUSELAGE FLOOR STRUCTURE, CORROSION FOUND ON RH INBD SEAT TRACK BETWEEN FR 12-18. RH INBD SEAT TRACK HAS BEEN REPLACED IAW ERJ-175 SRM 51-43-03, 51-41.01 AND 51-43-02 REV 53.SDR 2026FA0000214Bushing Sleeve · migratedFOUND BRONZE PARTICLES IN FULL FLOW FILTER AT INSPECTION. TRACED TO MIGRATING CONNECTING ROD BUSHINGS ON ALL 4 RODSSDR FDEA202603250371Tire · damagedNR 7 TIRE ARRIVED WITH THROWN TREAD. REMOVED AND REPLACED THE NR 7 MLG WHEEL ASSY REF ABOVE. ACFT OK FOR CONTINUED SERVICE.SDR AALA202603253511Light · inoperativeAIRCRAFT IN BASE MAINTENANCE: L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED L1 DOOR EXTERIOR EMERGENCY LIGHT. PER AMM 33-51-04. OPS CHECK GOOD.SDR WX0A2026032532766Power Supply · no test(AIRCRAFT NOT GROUNDED) ALL 4 EPSU BATTERIES FAILED CAPACITANCE TEST/ REMOVED ALL 4 EPSU BATTERIES (FIN 10WL, 11WL, 12WL, 13WL) REF. AMM 33-51-38-000-002-A & INSTALLED SERVICEABLE BATTERIES REF. AMM 33-51-38-400-002-A"SDR KCSA2026032512Escape Reel · unserviceableNR 1 EMERGENCY DESCENT DEVICE DEPLOYED. R & R EMERGENCY DESCENT DEVICE IAW AMM 25-61-01. NO DEFECTS NOTED. CHECKS GOOD. NR 2 EMERGENCY DESCENT DEVICE DEPLOYED. R&R EMERGENCY DESCENT DEVICE IAW AMM 25-61-01. NO DEFECTS NOTED. CHECKS GOOD. NR 3 EMERGENCY DESDR ABXA20260325132Circuit Card · defectiveDURING TAXI OUT, AFTER ENG START CHECKLIST R STRUT DCT LEAK & L STRUT DCT LEAK EICAS MESSAGE. MAINTENANCE REMOVED AND REPLACED DUCT LEAK DETECT CARD IAW B767 AMM 26-10-01. OPS CHECK GOOD. A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.SDR UIEA2026031100080Floorbeam · corrodedMAIN DECK CARGO UPON REMOVAL OF FLOOR PANEL FLOOR BEAM AT STATION 2220 LBL 82 FOUND CORRODED. CORRODED FLOOR BEAM AT STATION 2220 LBL 82, REPAIR CARRIED OUT AS PER SRM 53-00-51-2R-3 REPAIR 3 REV 106. NO FURTHER DEFECTS NOTED. PN BAC1505-101049.SDR UIEA2026031100081Lever · crackedMAIN DECK CARGO DOOR L5 FUSELAGE DOOR FRAME CUTOUT JUST OUTBOARD OF HOLD/OPEN RELEASED LEVER FOUND CRACK. CRACK ON MAIN DECK CARGO DOOR L5 FUSELAGE DOOR FRAME CUTOUT OUTBOARD OF HOLD/OPEN RELEASED LEVER, REPAIR CARRIED OUT AS PER B747-400F SRM 53-60-15-2R-7 RSDR UIEA2026031100082Not Reported · not reportedWHILE ACCOMPLISH EO #4453C592, FOUND STEP 1 TBD BY EO REV 1 AND REQUIRE TO CONTACT MANUFACTURER TO APPROVE THE EXISTING REPAIR AND PROVIDE THE CAT B FAA 8100-9. REPAIR CARRIED OUT IAW EN #3137-26 REV 1. NO FURTHER DEFECTS NOTED.SDR UIEA2026031100085Splice · corrodedMAIN EE CTR SPLICE STRAP AT STATION 400 RBL 63 FOUND WITH SURFACE CORROSION.(<P>MAIN EE CTR SPLICE STRAP AT STATION 400 RBL 63 WORK ACCOMPLISHED IAW EN# 3155-26 REV 0. NO FURTHER DEFECTS NOTED. PN 65B07936-358SDR UIEA2026031100086Frame · crackedDURING HFEC OPEN HOLE INSPECTION AT NON STRETCHED UPPER DECK TENSION TIE AND FRAMES, STATION 820 LHS FOUND 01 EA HOLE CRACKED AT AROUND 6 O'CLOCK POSITION AS MARKED.(<P>REPAIR CARRIED OUT ON CRACKED TENSION TIE AT STATION 820 IAW B747-400F SRM 53-20-302R REPAISDR UIEA2026031100087Frame · crackedDURING HFEC OPEN HOLE INSPECTION AT NON STRETCHED UPPER DECK TENSION TIE AND FRAMES, STA 820 RHS. FOUND 02 EA HOLES CRACKED AT 11 O'CLOCK AND 6 O'CLOCK POSITION RESPECTIVELY, VIEW LOOKING FORWARD AS MARKED.(<P>REPAIR CARRIED OUT ON CRACKED TENSION TIE AT STA SDR UIEA2026031100088Frame · crackedDURING HFEC OPEN HOLE INSPECTION AT NON STRETCHED UPPER DECK TENSION TIE AND FRAMES, STA 860 RHS FOUND 01 EA HOLE CRACKED AT AROUND 11 O'CLOCK POSITION VIEW LOOKING FORWARD AS MARKED. REPAIR CARRIED OUT ON CRACKED TENSION TIE AT 860 RT IAW B747-400F SRM 53-20SDR UIEA2026031800096Frame · crackedDURING HFEC OPEN HOLE INSPECTION AT NON STRETCHED UPPER DECK TENSION TIE AND FRAMES STA 760 LHS FOUND 01 EA HOLE CRACKED ON STEEL PLATE AS MARKED.(<P>NON STRETCHED UPPER DECK TENSION TIE AND FRAMES STA 760 LHS WORK ACCOMPLISHED IAW EN#3186-26 REV 0. NO FURTHESDR UIEA2026031800097Skin · dentedLOWER FUSELAGE SKIN STA 517 S36R FOUND DENT. LOWER FUSELAGE SKIN STA 517 S36R WORK ACCOMPLISHED IAW EN 3188-26 REV 0. NO FURTHER DEFECTS NOTED.SDR UIEA2026031800098Skin · dentedDENT AT LOWER HALF OF FUSELAGE EXTERNAL SKIN AT STA 463 S33L - S34L. DENT AT LOWER HALF OF FUSELAGE EXTERNAL SKIN AT BS 463 S33L - S34L WORK ACCOMPLISHED IAW EN #3167-26 REV 0. NO FURTHER DEFECTS NOTED.SDR UIEA2026031800099Skin · dentedDENT ON FUSELAGE EXTERNAL SKIN AT STA 2595 S25R - S26R.(<P>DENT AT OF FUSELAGE EXTERNAL SKIN AT STA 2595 S25R - S26R, WORK ACCOMPLISHED IAW EN #3185-26 REV 0. NO FURTHER DEFECTS NOTED. PN 65B02698-18.SDR UIEA2026031800100Spar Web · corrodedRIGHT WING GEAR W/W CENTER WING REAR SPAR WEB JETTISION PUMP CUTOUT FOUND CORROSION. RT WING GEAR W/W CENTER WING REAR SPAR WEB JETTISION PUMP CUTOUT WORK ACCOMPLISHED IAW EN #3157-26 REV 0. PN 111U1007-11. NO FURTHER DEFECTS NOTED.SDR UIEA2026031800101Spar Web · corrodedLH WING GEAR W/W CENTER WING REAR SPAR WEB JETTISON PUMP CUTOUT FOUND CORROSION.(<P>LH WING GEAR W/W CENTER WING REAR SPAR WEB JETTISON PUMP CUTOUT WORK ACCOMPLISHED IAW EN 3156-26 REV 0. NO FURTHER DEFECTS NOTED. PN 111U1007-11.</P>)SDR UIEA2026031800102Structure · corrodedDURING HFEC INSPECTION AT LOWER FUSELAGE AREA 2, FOUND CORROSION INDICATION AT STA 1718 - STA 1740 S45L. LOWER FUSELAGE AREA 2 STA 1718 - STA 1740 S45L WORK ACCOMPLISHED IAW EN #3190-26 REV 0. NO FURTHER DEFECTS NOTED.SDR 2026FA0000213Compressor · damagedENGINE WAS RETURNED TO OUR REPAIR STATION FOR UNSCHEDULED REPAIR. FLIGHT CREW REPORTED HEARING AN “ABNORMAL NOISE” DURING FLIGHT; HOWEVER, ALL ENGINE PARAMETERS WERE REPORTED TO REMAIN WITHIN NORMAL LIMITS. POST-FLIGHT INSPECTION REVEALED MISSING AIRCRAFT INSDR SCNA20260325143Light · inoperativeRIGHT OVERWING EMERGENCY LIGHT AFT IS INOPERATIVE. R & R RT AFT OVERWING EMERGENCY LIGHT IAW AMM 33-51-04 OPS CHECK GOOD AT THIS MOMENT,SDR SCNA20260325142Warning Message · illuminatedON FLAP EXTENSION. GOT A FLAP DISAGREE <1 HANDLE AT 5. REMOVED AND REPLACED FLAP POSITION INDICATOR REF. AMM 27-58-02, OPS CHECK GOOD. REMOVED AND REPLACED FLAP POSITION TRANSMITTER PER AMM 27-58-02 OPS CHECK GOOD.SDR 2026FA0000212Engine · making metalDURING THE ENGINE OVERHAUL, UNDER THE DISASSEMBLY PROCESS, WE FOUND A MOUNTED EXTERNAL SPIN-ON OIL FILTER. HOWEVER, THE ENGINE STILL RETAINED ITS ORIGINAL INTERNAL MESH OIL FILTER. THE ORIGINAL FILTER CONTAINED A SIGNIFICANT AMOUNT OF OIL SLUDGE, DEPOSITS, ANDSDR SWIA2026032477423Bulkhead · corrodedCORROSION FOUND ON BS 280 BULKHEAD AT STR 26L UNDER CRAWL WAY SUPPORT ANGLE. REMOVED CORROSION ON THE BS 280 BULKHEAD IAW SRM 51-21-06-001-001-A01,COMPLIED WITH ALL STEPS 1-9 OF REO 670-53-11-2298, REV -.SDR 9SZA202609100148Terminal · looseENGINE FIRE CAUTION LIGHT INTERMITTENT. FIRE DETECTORS PASSED BENCH TEST PROCEDURES IAW MM. WITH EXCESSIVE VIBRATION AND MOVEMENT, ENG FIRE CAUTION LIGHT INTERMITENT ILLUMINATION.SDR 9SZA202607100147Terminal · looseENGINE FIRE CAUTION LIGHT INTERMITTENT. FIRE DETECTORS PASSED BENCH TEST PROCEDURES IAW MM. WITH EXCESSIVE VIBRATION AND MOVEMENT, ENG FIRE CAUTION LIGHT INTERMITENT ILLUMINATION.SDR SWIA2026032476345Skin · gougedLEFT AILERON LEADING EDGE GOUGED AND CHAFED IN MULTIPLE LOCATIONS. REPLACED THE LH AILERON LEADING EDGE SKIN IAW DWG CC670-13000, REV-D, SRM 51-42-06, SRM 51-42-21, AND SRM 51-42-22. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SWIA2026032476342Skin · gougedRIGHT AILERON LEADING EDGE GOUGED AND CHAFED IN MULTIPLE LOCATIONS. REPLACED RT AILERON LEADING EDGE SKIN IAW DWG 601R13031, REV-K , SRM 51-42-06 AND SRM 51-42-13. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR IPXA2026052858550Skin · damagedMAJOR REPAIR, OVERSIZE RIVET HOLES, IN SLAT INSERT FITTING AND SLAT LEADING EDGE RIB ATTACH FASTENERS NR 9 SLAT ALL STEPS OF EO-96917-REQ7 C/W.SDR REXA2026050700511Crossbeam · crackedAFTER RH CROSSBEAM REMOVAL, CRACK ON ANGLE RBL26.00 & LBL26.00 FS280.00 WAS FOUND AT FWD FACE OF THE BULKHEAD FS280.00, BELOW FLOOR ANGLE RBL26.00 & LBL26.00 FS280.00 AT FWD FACE OF THE BULKHEAD FS280.00, BELOW FLOOR WERE REPLACED PER CRJ900 SRM 51-42-06-001-SDR REXA2026050700510Crossbeam · crackedAFTER RH CROSSBEAM REMOVAL, CRACK ON ANGLE RBL26.00 & LBL26.00 FS280.00 WAS FOUND AT FWD FACE OF THE BULKHEAD FS280.00, BELOW FLOOR ANGLE RBL26.00 & LBL26.00 FS280.00 AT FWD FACE OF THE BULKHEAD FS280.00, BELOW FLOOR WERE REPLACED PER CRJ900 SRM 51-42-06-001-SDR SWAA2026050482884Floorbeam · corrodedCORROSION FLOORBEAM LOCATED BS 947.5 AND RBL23 WL208.1 AFT GALLEY AND LAV. PERFORMED REPAIR ON FLOORBEAM LOCATED STA947.5 AND RBL23 WL208.1 AFT GALLEY AND LAV IAW EA 26-153-00958.SDR SWAA2026050482883Floor Support · corrodedCORROSION FLOOR SUPPORT BTW BS947.5 TO BS967 ; LBL16 AND WL208.1 AT AFT GALLEY AREA. REPLACED INTERCOSTAL AND FASTENERS LOC. FLOOR STRUCTURE BTW BS947.5 TO BS967 ; LBL16 AND WL208.1 AT AFT GALLEY AREA IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND SDR SWAA2026050495352Floor Support · corrodedCORROSION FLOOR SUPPORT BTW BS947.5 TO BS967 ; LBL16 AND WL208.1. REPLACED INTERCOSTAL AND FASTENERS LOC. FLOOR STRUCTURE BTW BS947.5 TO BS967 ; LBL16 AND WL208.1 AT AFT GALLEY AREA IAW B737-800 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 147A565SDR SWAA2026050482887Floor Support · corrodedCORROSION INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA947.5 TO STA967 AND RBL50 WL208.1 AT AFT GALLEY AREA. REPLACED INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA947.5 TO STA967 AND RBL50 WL208.1 AT AFT GALLEY AREA IAW B737-800 SRM 51-40-02; SRM 51-10-02SDR SWAA2026050482582Scuff Plate · crackedCRACK SERVICE DOOR SCUFF PLATE AT FWD AREA GALLEY. REPAIRED THE CENTER SCUFF PLATE AT FWD SERVICE DOOR IAW SRM 53-10-15-2R-2; REPAIR 2; PARAGRAPH 4. B; FIGURE 203. REFER TO BAC 5975.SDR SWAA2026050482886Floorbeam · corrodedCORRODED FLOORBEAM LOCATED BS 947.5 AND LBL51 WL208.1 AFT GALLEY AND LAV CHORD PERFORMED REPAIR ON FLOORBEAM LOCATED STA947.5 BTW BL0 TO LBL 60 WL208.1 AFT GALLEY AREA IAW SRM 53-70-51-2R-5, REPAIR 5, PARAGRAPH 4, AND EA 26-153-00929-WIP5.SDR SWAA2026050482792Light · deterioratedDETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ALONG PASSENGER CABIN (1KT) REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ALONG PASSENGER CABIN IAW AMM 33-51-15-400-802; INSTALLATION WILL BE DOCUMENTED ON TTG8Q003LL23 AND TTG8Q003LMTPSDR AALA202605011964Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT #1 DOORSTOP FITTING AT FR 68 AND S22L. REPAIRED FRAME PER EA 374075.