Service difficulty reports
1,770,704 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 SWAA2026092868281Floor Panel · pulledFLOOR PANEL 241JF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED A NEW FLOOR PANEL 241JF IAW SRM 53-00-50-2R-0 AND DWG 146A5810-453.SDR SWAA2026092887107Floor Panel · pulledFLOOR PANEL 241SF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241SF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1,SDR SWAA2026092827889Floor Panel · pulledFLOOR PANEL 242GF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACED THE FLOOR PANEL IAW SRM 53-00-50-2R-0-B00275.SDR SWAA2026092832479Attach Angle · crackedCRACK FOUND AT BS 692.75, RBL 0.2, WL 207, UNDER 241AF FLOOR PANEL. REMOVED AND REPLACED THE FLOORBEAM ATTACH ANGLE IAW SRM 51-40-02, & DWG 273A9111, REV -.SDR SWAA2026092891995Floor Panel · pulledFLOOR PANEL 241HF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 AND BOEING DWG 146A5810.SDR SWAA2026092851806Floor Panel · pulledFLOOR PANEL 241RF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE FLOOR PANEL 241RF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR SWAA2026092804217Floor Panel · pulledFLOOR PANEL 241GF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE FLOOR PANEL 241GF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR SWAA2026092844663Floor Panel · pulledFLOOR PANEL 231NF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE FLOOR PANEL 231NF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR SWAA2026092847690Sidewall Support · corroded18 AREAS OF CORROSION FOUND ON FLOOR TO SIDEWALL SUPPORT FROM BS 480 - 500D+15, WL 156, TASK CARD WILL BE ACCOMPLISHED ON CUSTOMER CARD TTG8Q01DUKN2.SDR SWAA2026092813479Floor Panel · pulledFLOOR PANEL 231GF UPPER SKIN HAD AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE, THE FLOOR PANEL 231GF WAS REPLACED IAW SRM 51-10-02-0G-0, PAR 9.A (1).SDR SWAA2026092823015Floor Panel · pulledFLOOR PANEL 241PF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2026092823001Floor Panel · pulledFLOOR PANEL 232JF UPPER SKIN HAD AREAS OF PULLED STRANDS. FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0, AND DWG 143A5810.SDR SWAA2026092862914Floor Panel · damagedAFT FLOOR PANEL 242D UPPER SKIN ALONG THE OTBD EDGE HAD AN AREA OF EXPOSED HONEYCOMB CORE. THE AFT FLOOR PANEL 242D WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2026092806679Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAD AREAS OF PULLED STRANDS. THE FLOOR PANEL 241DF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2026092890908Scuff Plate · crackedACD AFT CORNER SCUFF PLATE IS CRACKED REPAIRED ACD AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1AND TREATED AND PRIMER IAW SRM 51-20-01-0G-0 FOR CHEMICAL CONVERSION COATING AND AMM 51-21-72-370-804 FOR PRIMER. (THE INSTALLATION PROCCES WILL BE ATTENDED ON TASK SDR SWAA2026092880434Floor Panel · pulledFLOOR PANEL 231FF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2026092828963Stringer Clip · crackedBS 727E, STR 6R STRINGER CLIP CRACKED, REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1112 REV -.SDR SWAA2026092804978Floor Panel · pulledFLOOR PANEL 232CF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE FLOOR PANEL 232CF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR SWAA2026092812829Stringer Clip · crackedFOUND A CRACKED STRINGER CLIP AT STA 727B, STGR 8 LH. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1102 REV -.SDR SWAA2026092863655Floor Panel · pulledFLOOR PANEL 231DF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE FLOOR PANEL 231DF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR SWAA2026092831840Floor Panel · pulledFLOOR PANEL 232FF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED BY FABRICATING NEW PANEL IAW SRM 53-00-50-2R-0-B00275.SDR SWAA2026092861519Stringer Clip · crackedFOUND A CRACKED STRINGER CLIP AT STA 727C, STGR 5 LH. REMOVED AND REPLACED STRINGER CLIP AT BS 727C STR-5L IAW SRM 51-40-02-0G-0 AND DWG#146A1103 REV: -.SDR SWAA2026092888536Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED NEW FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810-127.SDR SWAA2026092847554Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED DAMAGED UPPER SKIN ON FLOOR PANEL 231ZF IAW SRM 53-00-50-2R-1.SDR SWAA2026092491395Access Panel · delaminatedDELAMINATED EXTERNAL SKIN ACCESS PANEL 191CL. REPAIRED EXTERNAL SKIN ACCESS PANEL 191CL IAW SRM 51-70-04-2R-1 REPAIR 1.SDR SWAA2026092433515Frame · crackedCRACKED FRAME, BS 312, BTWN STR 5L - 6L. REPAIRED THE FRAME IAW M-22-153-01244.SDR SWAA2026092343474Shear Angle · crackedCRACKED SHEAR ANGLE, BS 658 - BS638, LBL 40.875. FABRICATED & REPLACED THE SHEAR ANGLE & FASTENERS IAW SRM 51-10-02, ITEM 9, & DWG 110A0220, SHEET 2, REV-.SDR 2026FA0000754Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.SDR AALA202609189657Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD FLAP INTERCONNECTING HINGE FITTING BEARING HAS EXCESSIVE PLAY - REPLACED INTERCONNECTING HINGE FITTING PER SRM 51-42-11SDR SWAA2026091754439Attach Angle · crackedRIGHT BS 663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL 10, WL167.68, BS 663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL 11, WL 167.68, CRACK FOUND TO BE OUT OF LIMITS AS PER SRM 57-10-10-1A-2. REPAIRED THE UPPER ATTACH ANGLE ON VAPOR BARRIER IASDR SWAA2026091689932Seat Track · corrodedCORROSION ON SEAT TRACK (TOP SURFACE) LOCATED BS 639 PLUS 23 INCH RBL 45.50 AT PASSENGER CABIN REFER TO FAULT TTG8Q01DUFY3 WHERE 26-153-02366-WIP1 WAS ADDED AS A SUBTASK.SDR SWAA2026091672764Seat Track · corrodedCORROSION ON SEAT TRACK (TOP SURFACE) LOCATED BS 639 PLUS 12 INCH RBL 45.50 AT PASSENGER . REPAIRED SEAT TRACK BTW BSTA 639 & BSTA 706 AT RBL 45.50 AT PASSENGER CABIN IAW EA 26-153-02366 AND EA 26-153-02366-WIP1.SDR SWAA2026091689594Seat Track · corrodedCORROSION ON SEAT TRACK (TOP AND BOTTOM SURFACE) LOCATED BTW BS 685 TO BS 706 RBL 45.50 AT PASSENGER CABIN.SDR SWAA2026091621561Skin · corrodedCORROSION EXTERNAL SKIN WATER SERVICE CUT OUT BTW BS 907 TO BS 927 AND BTW STRG 26R TO STRG 27R AT LOWER FUSELAGE. REPAIRED EXTERNAL SKIN WATER SERVICE CUT OUT BTW BS 907 TO BS 927 AND BTW STRG 26R TO STRG 27R AT LOWER FUSELAGE IAW EA 26-153-02413 SUMMARY EA SDR SWAA2026091613651Seat Track · corrodedCORROSION ON SEAT TRACK (TOP SURFACE) LOCATED BTW BS 663 TO BS 685 RBL 45.50 AT PASSENGER CABIN 2026-505409 REFER TO FAULT TTG8Q01DUFY3 WHERE 26-153-02366-WIP1 WAS ADDED AS A SUBTASK..SDR SWAA2026091478011Crossbeam · crackedCRACKED BRAKE PANEL, BS 540, BTWN BL 0 - RBL 24.75. REPLACED THE BRAKE PANEL IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DWG 143A0060, SHEET 64, REV-.SDR SWAA2026091457583Crossbeam · crackedCRACKED FLOOR CROSSBEAM, BS 540 BTWN BL 0 - RBL 24. REPLACED THE FLOOR CROSSBEAM IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, AND DWG: 143A0060, SHEET 36, REV A.SDR SWAA2026091413486Stringer · deformedSTRINGER 24R, BS 380+11.5, STRINGER IS DEFORMED. DAMAGE MEASUREMENT ENTRY ACCOMPLISHED INTERIM REPAIR FOR FERRY FLIGHT PER EA 26-153-02269. REF: TTG8Q01DU003 REFER TO TTG8Q01DX8JC FOR STRINGER 24R REPLACEMENT.SDR SWAA2026091457114Crossbeam · crackedCRACK FLOOR STRUCTURE SUPPORT BREAK ASSY LOCATED BS 540 BTW BL0 TO LBL 24. REPLACED IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, AND DWG 143A0060, SHEET 36, REV A.SDR CALA2026091419397Threshold Web · damagedELONGATED HOLES ON WEB IN FWD CARGO DOOR CUTOUT, LOWER FRAME, AFTER CORNER STA 450 APPROX (REF AAR NR 1000088040). REMOVED AND REPLACED WEB ON FWD CARGO DOOR CUTOUT, LOWER FRAME BTW STA 440 TO 492.4 IAW B737-700 SRM 51-40-02-0G-0, 51-40-05-0G-0, 51-40-08-0G-0,SDR SWAA2026091100263Angle · crackedCRACK ON ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN. REPLACED ANGLE AND FASTENERS IAW SRM 51-40-02 AND DWG 273A9110, SHEET 6, REV A.SDR SWAA2026091156959Strap · crackedCRACK INDICATION FOUND ON BS 639, LBL 45.57 STUB BEAM STRAPS AREA (AFT FASTENER HOLE) AT PASSENGER CABIN. REPLACED THE STRAPS, STUB BEAM STRAPS IAW SRM 51-10-02, ITEM 9, & DWG 144A1715, SHEET 9, REV A.SDR SWAA2026090819724Angle · crackedCRACKED TRAILING EDGE ANGLE LOCATED ORSS 270, RT WING. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 115A2930, SHEET 8, REV -.SDR R61A2026090700251Skin · crackedDURING HEAVY CHECK RUDDER ASSEMBLY SKIN CRACK FOUND ON RT L/E BY HINGE 2. RUDDER ASSEMBLY WAS REPAIRED IAW EMB ETD 2026-170-014644SDR SWAA2026090457748Handle · unsecureR2 DOOR ASSIST HANDLE NEEDS TO BE SECURED. SECURED R2 DOOR ASSIST HANDLE IAW AMM 25-21-25-420-801.SDR SWAA2026090432072Handle · unsecureL1 DOOR ASSIST HANDLE NEEDS SECURED. SECURED THE L1 DOOR ASSIST HANDLE IAW AMM 25-21-25-420-801.SDR DALA2026090104938Light · detachedEMERGENCY LIGHT AT 3C IS COMING OUT. REMOVED AND REPLACED SEAT SHROUD AND EMERGENCVY PATH LIGHT ASSY IAW CMM25-29-58. (9566679) AIRCRAFT WAS GROUNDEDSDR AALA202608314168Support Angle · crackedAIRCRAFT IN BASE MAINTENANCE: VAPOR BARRIER SUPPORT ANGLE CRACKED AT AC BAY FWD OF STA 663, RBL 9" FROM CENTER OF KEEL BEAM. MAINTENANCE PERFORMED DOUBLER REPAIR OF SUPPORT ANGLE IAW EA 378309 AND DRAWING DBF 2211.SDR SWIA2026082176992Skin · dentedMULTIPLE DENTS AND ONE CREASE ON FUSELAGE BELLY, FWD OF AFT EQUIPMENT BAY DOOR. REPAIRED MULTIPLE DENTS AND THE CREASE ON THE FUSELAGE FWD OF THE AFT EQUIPMENT BAY DOOR IAW REO 601R-53-61-8627, REV -.SDR IPXA2026082995025Blowout Door · chafedCHAFED SKIN OF NR 1 ENG RT THRUST REVERSER LOWER BLOWOUT DOOR INNER L/E AREA. INSTALLED NEW BLOWOUT DOOR IAW SRM 51-40-02-0G, REV 132, & AIPC 78-31-51-03, REV 40, IPC 78-32-22, REV 96, & AMM 78-31-19-402-008, REV 149.