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 WX0A2026030232744Unknown · odor(AIRCRAFT NOT GROUNDED) DESCENDING THROUGH 8,000 TO 4,000 FEET STRONG DIRTY SOCK SMELL NOTED IN FLIGHT DECK, FWD CABIN, AND AFT CABIN. PERFORMED TC A32X-21-000-001 (W/O: 545051, TASKCARD: NR-00001). TASK CARD 21-000-002 COMPLIED (W/O: 544173, TASKCARD: NR-00SDR YENA2026030200246Unknown · odorFLT #405 EWR-FLL. "ON DESCENT @ APPROX 10,000 FT ENGINES AT IDLE, APU OFF MAGIC MARKER ODOR IN FLIGHT DECK, DIMINISHED WITH PACK 1 OFF PER PROCEDURE RETURNED W/ PACK ON .;COMPLIED WITH INFORMATION NOTICE 2017-T015, STEP 1, ISOLATED FAULT TO TYPE 10 MISCELLANEOSDR YENA2026030200245Manifold · leakingFLT# 1584 MCO-JFK."GREEN HYD RESERVOIR QUANTITY LOW DURING CRUIS ON ECAM.; FOUND 1113GM GREEN PTU MANIFOLD LEAKING. REMOVED PTU MANIFOLD ASSY IAW AMM 29-11-15. REF L/P 4452864 ITEM 2 FOR INSTALLATION."SDR ASAA2026030164639Switch · no discrepancyFA REPORTS L1 DOOR YELLOW DOOR RELEASE SWITCH STICKS, HARD TO RELEASE TO CLOSE THE DOOR. GROUNDED - YES. CHECK L1 DOOR HOLD OPEN LOCK (YELLOW) OPEREATION, NO DEFECT NOTED REF. AMM 52-11-00/201.SDR SWIA2026030175392Bleed Air Sys · faultedBLEED 2 FAIL ON DEPARTURE CLIMB PASSING APPROX 7,000. CYCLED BLEED 2 PER QRH PROCEDURE AND BLEED 2 FAIL RETURNED. (FLIGHT 3845) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31807705. TROUBLESHOT THE BLEED 2 FAIL MESSAGE IAW FIM 36-11-00. FOUND FAULT CODE SDR SWAA2026030275725Girt Bar · detachedFWD SVC DOOR SLIDE SHROUD; GIRT BAR CLIP PULLED FROM RIVET. PERFORMED MT 725-61-06-FS TO FACILITATE FASTENER REPLACEMENT ON FWD GIRT BAR CLIP PER SRM 51-40-02. SLIDE REINSTALLED; CHECKS GOOD.SDR VNAA2026030213202Manifold · unserviceableSTEERING INOP CAUTION MSG IN FLIGHT. / REMOVED AND REPLACED OF THE STEERING MANIFOLD IAW AMM 32-51-50-000/400-801-A01. PERFORMED BLEEDING OF HYDRAULIC SYSTEM NO 3 IAW AMM 29-10-00-870-802-A01. PERFORMED OPERATIONAL TEST OF THE NOSE WHEEL STEERING IAW AMM 32-51SDR DALA2026030201414Warning Message · false activationFCNT/DE- DUE TO TRAILING EDGE FLAP DISAGREE FROM FLAP HANDLE OVERSHOOT. T/S PER FIM WITH NO FAULTS.SDR DALA2026030201411Warning Message · false activationFCNT/DE- DUE TO TRAILING EDGE FLAP DISAGREE. T/S PER FIM. RAN FLAPS WITH NO TROUBLE FOUND. PERFORMED FLAP LUBE WORKCARDS.SDR DALA2026030201410Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE BTW STA 1600- 1640 RBL22 AND RBL44 AT PASSENGER CABIN (W4). : CORROSION LEVEL 2. SEAT TRACK FLANGE BTW STA 1600-1640 RBL22 AND RBL44 AT PASSENGER CABIN WERE REPLACED AND INSTALLED PER DWG 146N5126 REV: - AND B757-300 SRM 51-40-02SDR F3LA202603020375Power Supply · no testDURING HEAVY CHECK EPSU TEST FAILED DUE TO POSITION 10WL UNIT FAILURE. REMOVED AND REPLACED EPSU UNIT AT POSITION 10WL IN REF TO AMM 33-51-38-000/400-001-A. EPSU SYSTEM TEST OK./END/SDR AALA202603021278Power Supply · faultedAIRCRAFT WAS GROUNDED: DURING POST SLIDE INSTALL TEST FWD LEFT EPSU AND MID CABIN LEFT EPSU FAIL OPS TEST. MAINTENANCE REPLACED MID LEFT EPSU IAW AMM 33-51-38.SDR QMLA2026030220014Vent · obstructedFLIGHT LEG RETURNING TO BASE FROM PATIENT DROP OFF THE CREW MEMBER IN THE BACK SAID THEY COULD SMELL FUEL. I COULD NOT AND HE STATED THAT HE HAD THE WINDOW OPEN. WHEN I ASKED HIM TO CLOSE THE WINDOW I COULD THEN SMELL THE FUEL UP IN FRONT OF THE CABIN. REMOSDR FDEA202603010302Wedge · wornWEAR IN WEDGE TRAILING EDGE LOWER SURFACE AT 33.75 INCHES OF INBD END ON SLAT NR 4, LT WING. WEAR IN WEDGE T/E LOWER SURFACE AT 33.75 INCHES OF INBD EDGE WAS REPAIRED IAW SRM 51-70-10-2R, REP 4, FIG 202, REV 94 & SRM 57-43-02-2R, FIG 201, REP 1, SHEET 1, REV SDR FDEA202603010301Wedge · wornWEAR IN WEDGE TRAILING EDGE LOWER SURFACE AT 30" OF INBD END ON SLAT NR 5, LT WING. LT WING, SLAT NR 5 TRAILING EDGE WEDGE LOWER SURFACE AT 30" OF INBD END EDGE WAS REPAIRED IAW SRM 51-70-10-2R, REP 4, FIG 202, SHEET B, REV 94 AND SRM 57-43-02-2R, FIG 201, RESDR FDEA202603010300Safety Wire · wrong partREF F.E.A. G-2560-F0386282 REV "C" PART 1. FOUND INCORRECT SAFETY WIRE INSTALLED ON L-1 DOOR SLIDE PACK RELEASE CABLE. AMM: 25-66-01-4 EA: 9-2560-T0386431 REF ABOVE AMM, E.A. AND WRI 25-60/7794, REPLACED SAFETY WIRE ON L1 DOOR SLIDE PACK RELEASE MECHASDR FDEA202603010299Rib · crackedRIGHT WING CENTER FLAP RIBS UPR FLANGE FOUND 3EA CRACKS AT RIB25 BETWEEN STGR2.7 AND REAR SPAR, RIB26 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 3EA CRACKS OF RIB25 AND 26 BETWEEN STGR2SDR FDEA202603010298Rib · crackedRT WING CENTER FLAP RIBS UPR FLANGE FOUND 3EA CRACKS AT RIB18 BETWEEN STGR2.7 AND REAR SPAR, RIB19 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 3EA CRACKS OF RIB18 AND 19 BETWEEN STGR2.7 SDR FDEA202603010297Rib · crackedRT WING CENTER FLAP RIBS UPR FLANGE FOUND 7EA CRACKS AT RIB11 BETWEEN S2.6 AND REAR SPAR, RIB12 BETWEEN STGR2.7 & REAR SPAR, RIB13 BETWEEN S2.6 AND S2.8 COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 7EA CRACKS OF RIB11SDR FDEA202603010296Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB15 BETWEEN STGR2.5 AND FRONT SPAR COMPLIED WITH EA 6-5750-T0386614 INSPECTED THE LH WING CENTER FLAP RIB UPR FLANGE OF RIB15 BETWEEN STGR2.5 AND FRONT SPAR AND REPAIRED THE BOTTOM SKIN POCKET CUT OUTSDR FDEA202603010295Rib · crackedLH WING CENTER FLAP RIBS UPR FLANGE FOUND 6EA CRACKS AT RIB16 BETWEEN STGR2.7 AND STGR2.8, RIB17 BETWEEN STGR2.8 AND REAR SPAR, RIB18 BETWEEN STGR2.8 AND REAR SPAR, RIB19 BETWEEN STGR2.7 AND REAR SPAR, RIB20 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6SDR FDEA202603010294Rib · crackedLH WING CENTER FLAP RIBS UPR FLANGE FOUND 5EA CRACKS AT RIB25 BETWEEN STGR2.7 AND REAR SPAR, RIB26 BETWEEN STGR2.7 AND REAR SPAR, RIB27 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0386614 REPAIRED THE LH WING CENTER FLAP RIB UPR FLANGES 5EA CRSDR FDEA202603010293Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB11 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0386614 REPAIRED THE LH WING CENTER FLAP RIB UPR FLANGE 1EA CRACK OF RIB11 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - LH SDR MASA2026030100007Battery · inoperativeEMERGENCY LIGHT, LT BATTERY FAULTED. R & R THE EMERGENCY LIGHT POWER SUPPLY.SDR UIEA2026030100070A/C Pack · odorDESCENDING THROUGH 10500 FEET, STRONG OIL TYPE SMELL IN BLEED AIR AIR CONDITIONING SYSTEM, STRONGER IN COCKPIT(<P>T/S OIL SMELL IN CABIN IAW B777 FIM 21-00 TASK 808, NO SMOKE OR OIL SMELL FOUND. PERFORMED HIGH POWER RUNS FOR BOTH ENGINES IAW B777 AMM 71-00-00,SDR ABXA20260301080Door · defectiveAT 3000 AGL DURING THE AFTER-TAKEOFF CHECKLIST, THE GEAR LEVER WAS MOVED TO THE OFF POSITION, DURING WHICH THE RT MLG EXTENDED, & GEAR DISAGREE LIGHT ILLUMINATED GEAR EXTENDED NORMALLY WILL PLACE GEAR ON MEL 32-30-1.MTX DEFERRED LANDING GEAR RETRACTION SYSTEMSDR COEA2026072329803Spar · corrodedWO 273091 NR 600013 HEAVY CHECK COE/MAJOR REPAIR: R/H WING REAR SPAR STRIP SLAT UPPER SURFACE BETWEEN RIBS 6-9 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS-00026285-01 ISSUE B, DATED 7/17/2026.SDR COEA2026072225803Strip · corrodedLEFT WING, REAR SPAR STRIP SLAT UPPER SURFACE BETWEEN RIBS 10-13 HAS LEVEL 2 CORROSION AROUND MULTIPLE FASTENER HOLES. CORRECTIVE ACTION: REPAIR PER SRAS-00026288-01 ISSUE A, DATED 6/8/2026.SDR COEA2026072218803Seat Track · corrodedRT SEAT TRACK HAS LEVEL 2 CORROSION. REPAIRED PER SRM 536300-01-A01, 51-25-02, 51-25-04 REV. 121.SDR SWIA2026022876125Intercostal · chafedLEFT OVERWING EMERGENCY EXIT CUTOUT SURROUND INTERCOSTAL CHAFED BETWEEN FS439 TO FS449.85, STGR 9L AND STGR 10L. REMOVED AND REPLACED INTERCOSTAL LOCATED AT LH OVERWING EE CUTOUT SURROUND BETWEEN FS439-449.85 STGR9L AND 10L IAW SRM 51-42-06.SDR SWIA2026022876014Window Post · crackedFOUND CRACK ON FO SIDE WINDSHIELD/WINDOW SIDE POST. CRACK STARTS AT UPPER MOST BARREL NUT HOLE AND EXTENDS ALL THE WAY THROUGH TO THE FWD EDGE. CRACK IS 0.50'' LONG. PER REO 670-53-11-2276 THE SUBJECT CONDITION IS ACCEPTABLE FOR ONE FERRY FLIGHT ONLY(THREE LESDR IPXA2026042451858Sidewall Panel · damagedLOWER FWD CARGO PIT SLOPING SIDE WALL PANEL ON LH SIDE P1 STATION 500. HAS SCRIVET HOLES PULLED THROUGH. .I.A.W AMM25-52-01-004-044 REV50 AND I.A.W AMM25-52-01-404-054 REV50 REPLACE SIDEWALL PANEL WITH NEW PARTS.SDR SWIA2026022875959Angle · corrodedMCD SILL ANGLE (2) CONNECTOR BRACKETS HAVE SURFACE CORROSION. REMOVED AND REPLACED 2 CORRODED CONNECTOR BRACKETS ON MCD SILL ANGLE IN REFERENCE TO SRM 51-42-06. DISPLACED AND RE-CONNECTED PAX DOOR WIRE HARNESS IN REFERENCE TO AMM 52-11-00. COMPLIED WITH TASKSDR SWIA2026022875958Retainer · gougedCARGO DOOR UPPER AFT SEAL RETAINER GOUGED. REMOVED AND REPLACED CARGO DOOR UPPER AFT SEAL RETAINER WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SWIA2026022875953Slat Track · wornLEFT SLAT TRACK 1-1 HAS WORN SPOT ON UPPER SIDE. BLENDED WORN AT LH SLAT TRACK 1-1 ON UPPER SIDE IAW SRM 51-12-00-001-001-A01, FOUND TO BE OUT OF LIMITS IAW SRM 57-41-25-001-001-A01 AND REMOVED AND REPLACED LT SLAT TRACK 1-1 ON JOB HN00298053.SDR SWIA2026022875952Slat Track · wornLEFT SLAT TRACK 1-1 HAS WORN SPOT ON LOWER SIDE. BLENDED WORN AT LH SLAT TRACK 1-1 ON LOWER SIDE IAW SRM 51-12-00-001-001-A01 FOUND TO BE OUT OF LIMITS IAW SRM 57-41-25-001-001-A01, AND REMOVED AND REPLACED LT SLAT TRACK 1-1 IAW AMM 27-81-41-400-801-A01 AND SDR SWIA2026022875938Slat Track · wornLEFT SLAT TRACK 3-3 HAS WORN SPOT ON LOWER SIDE. BLENDED WORN AT LT SLAT TRACK 3-3 ON LOWER SIDE IAW SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-57-42-2405, REV -.SDR SWIA2026022875937Slat Track · wornLEFT SLAT TRACK 2-1 HAS WORN SPOT ON LOWER SIDE. LIGHTLY BLENDED 2 EACH SPOTS ON LT SLAT TRACK 2-1 LOWER SIDE IAW SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-57-42-2400 REV-.SDR SWIA2026022875936Slat Track · wornLEFT SLAT TRACK 2-2 HAS WORN SPOT ON INBD SIDE. BLENDED WORN AT LT SLAT TRACK 2-2 ON INBD SIDE IAW SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-57-42-2399, REV -. CHECKS GOOD.SDR SWIA2026022875935Slat Track · wornLEFT SLAT TRACK 2-2 HAS WORN SPOT ON OTBD SIDE. BLENDED WORN AT LT SLAT TRACK 2-2 ON OTBD SIDE IAW SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-57-42-2399, REV -.SDR SWIA2026022875934Slat Track · wornRIGHT SLAT TRACK 2-2 HAS WORN SPOT ON OTBD SIDE. BLENDED WORN AREA OF RH SLAT TRACK 2-2 ON OUTBOARD FORWARD EDGE AND 3EA WORN AREAS ON AFT FACE OF RH SLAT TRACK 2-2 IAW SRM 51-12-00-001-001-A01. FOUND TO BE WITHIN LIMITS REF REO 670-57-42-2401, REV --, COMPSDR SWIA2026022875933Slat Track · wornRIGHT SLAT TRACK 1-1 HAS WORN SPOT ON LOWER SIDE. BLENDED 4 EACH SPOTS RH SLAT TRACK 1-1 LOWER SIDE IAW SRM 51-12-00-001-001-A01, COMPLIED WITH ALL STEPS OF REO 670-57-42-2383 REV-.SDR SWIA2026022875932Slat Track · wornRIGHT SLAT TRACK 2-3 HAS WORN SPOT ON LOWER SIDE. BLENDED WORN AT RT SLAT TRACK 2-3 ON LOWER SIDE IAW SRM 51-12-00-001-001-A01. PERFORMED REPAIRS IAW REO 670-57-42-2384 REV-. CHECKED GOOD.SDR SWIA2026022875931Slat Track · wornRIGHT SLAT TRACK 3-2 HAS WORN SPOT ON LOWER SIDE. BLENDED WORN AT RT SLAT TRACK 3-2 ON LOWER SIDE IAW SRM 51-12-00-001-001-A01. PERFORMED REPAIRS IAW REO 670-57-42-2398, REV --,CHECKED GOOD.SDR SWIA2026022875930Slat Track · wornRIGHT SLAT TRACK 3-1 HAS WORN SPOT ON LOWER SIDE. BLENDED WORN AT RT SLAT TRACK 3-1 ON LOWER SIDE. IAW SRM 51-12-00-001-001-A01. PERFORMED REPAIRS IAW REO 670-57-42-2393, REV -A CHECKED GOOD.SDR VNAA202604110003Skin · damagedLIGHTNING STRIKES (2EAS) BTW FS=260.00 TO FS=280.00 AND SGTR 20L AT FUSELAGE SKIN. LIGHTNING STRIKES (2EAS) BTW FS=260.00 TO FS=280.00 AND SGTR 20L AT FUSELAJE SKIN. WAS REPAIRED PER REO 690-53-11-2168 REV. - -SDR VNAA202604110002Skin · damagedLIGHTNING STRIKES (1EA) BTW FS=295.00 TO FS=310.00 AND BTW SGTR 7L TO SGTR 8L AT FUSELAJE SKIN. LIGHTNING STRIKES (1EA) BTW FS=295.00 TO FS=310.00 AND BTW SGTR 7L TO SGTR 8L AT FUSELAJE SKIN WAS REPAIRED PER REO: 690-53-21-2115, REV: - -SDR VNAA202604110001Skin · dentedDENTS (2 EAS) ON EXTERNAL FUSELAGE SKIN BTW FS 1031-1051 AND STGRS 26R-24R. DENTS ON EXTERNAL FUSELAGE SKIN BTW FS 1031-1051 AND STGRS 26R-24R WAS REPAIRED PER REO 690-53-61-1750 REV -SDR SWAA2026033175363Access Panel · crackedCRACKED ACCESS PANEL 324AR ON THE VERTICAL STAB. REPLACED THE ACCESS PANEL 324AR IAW SRM 51-40-02-0G, SRM 51-10-02-0G-0, & DWG 172A6123, SHEET 1, REV A.SDR SWAA2026033075399Cover · detachedFWD ENTRY DOOR SLIDE COVER DETACHED FROM FRAME. REPAIRED THE SLIDE COVER IAW AMM 25-66-01-340-001.