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 SWAA2026041677808Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026041677665Floorbeam · corrodedCORRODED FLOORBEAM, BS 986, RBL 44, WL 208.1. PERFORMED A PERMANENT REPAIR TO THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.SDR SWAA2026041677654Floorbeam · corrodedCORRODED FLOORBEAM, BS 344, LBL 7, WL 208.1. REPAIRED THE FLOORBEAM IAW EA 26-153-00771. 26-153-00771-WIP1, 26-153-00771-WIP2, AND 26-153-00771-WIP3.SDR SWIA2026030875685Seat Track · corrodedFORWARD FUSELAGE WET AREA RH TRACK AT FRAME 17 AT Y+10IN HAS CORROSION. REMOVED AND REPLACED FWD FUSELAGE WET AREA RH TRACK AR FR 16 PN 170-03263-001 PO# 339110 IAW EMB 175 SRM 51-40-08. PART DOES NOT AFFECT WEIGHT AND BALANCE. NO FURTHER ACTION REQUIREDSDR SWIA2026030875684Seat Track · corrodedFORWARD FUSELAGE WET AREA L/H TRACK AT FRAME 16 Y-10IN HAS CORROSION AROUND RIVET. REMOVED AND REPLACED FWD FUSELAGE WET AREA LH TRACK AR FR 16 PN 170-03264-001 PO# 329698 IAW EMB 175 SRM 51-40-08. PART DOES NOT AFFECT WEIGHT AND BALANCE. NO FURTHER ACTION RSDR SWAA2026040777642Stiffener · crackedNR 2 ENG OTBD FAN COWL CRACKED STIFFENER AFT OF OIL SERVICE PANEL 424AR. REMOVED AND REPLACED FAN COWL; CORRECTING FAULT ON SEPARATE CARD. REF TTG8Q00S5GXC FOR DETAILS.SDR R61A2026040500084Shear Tie · corrodedDURING HEAVY CHECK AFT CARGO FRAME 77 BETWEEN STR 29 L - STR 28 L SHEAR CLIP FOUND WITH CORROSION. REMOVED AND REPLACED SHEAR CLIP IAW SRM 51-41-01 AND 51-41-02.SDR R61A2026040500083Support · corrodedDURING HEAVY CHECK AFT CARGO FRAME 77 BETWEEN STGR 29 L - 29 R SUPPORT BAG FOUND WITH CORROSION. REMOVED AND REPLACED SUPPORT BAG IAW EMB 170/175 SRM 51-41-01 AND 51-41-02SDR R61A2026040500082Shear Tie · corrodedDURING HEAVY CHECK AFT CARGO FRAME 76 BETWEEN STR 22 L - 21 L SHEAR CLIP FOUND WITH CORROSION. REMOVED AND REPLACED SHEAR CLIP IAW SRM 51-41-01 AND 51-41-02SDR R61A2026040500081Seal Rest · corrodedDURING HEAVY CHECK AFT CARGO DOOR CUTOUT LOWER AFT SEAL REST FOUND CORRODED. REMOVED AND REPLACED SEAL REST IAW EMB 170/175 AMM 20-10-01SDR R61A2026040500080Seal Rest · corrodedDURING HEAVY CHECK AFT CARGO DOOR CUTOUT LOWER FWD SEAL REST FOUND WITH CORROSION. REMOVED AND REPLACED SEAL REST IAW EMB 170/175 AMM20-10-01SDR R61A2026040500079Seal Rest · corrodedDURING HEAVY CHECK FWD CARGO DOOR CUTOUT LOWER FWD SEAL REST FOUND WITH CORROSION. REMOVED AND REPLACED SEAL REST IAW AMM 20-10-01SDR R61A2026040500078Shear Panel · corrodedDURING HEAVY CHECK CF III MID SHEAR PANEL BETWEEN FR 87 - FR 88 RBL 10 - LBL 10 FOUND CORODED. REMOVED AND REPLACED SHEAR PANEL IAW EMB 170/175 SRM 51-42-01SDR R61A2026040500077Plate · corrodedDURING HEAVY CHECK CF III GUSSET PLATE AT FR 90 RBL 24 FOUND CORRODED. REMOVED AND REPLACED GUSSET PLATE IAW EMB 170/175 SRM 51-42-01SDR R61A2026040500076Shear Panel · corrodedDURING HEAVY CHECK CF III R/H SHEAR PANEL BETWEEN FR 87 - FR 88 RBL 12 - RBL 41 FOUND CORRODED. REMOVED AND REPLACED SHEAR PANEL IAW EMB 170/175 SRM 51-42-01SDR R61A2026040500075Floor Panel · corrodedDURING HEAVY CHECK CF III R/H FLOOR PANEL BETWEEN FR 88 - FR 90 RBL 40 FOUND CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PANEL IAW EMB 170/175 SRM 51-42-01 AND 51-43-01SDR R61A2026040500074Floor Panel · corrodedDURING HEAVY CHECK CF III R/H FLOOR SUPPORT PANEL AT FR 84 BETWEEN RBL 35 - RBL45 FOUND CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PANEL IAW EMB 170/175 SRM 51-41-02SDR R61A2026040500073Stringer · corrodedDURING HEAVY CHECK AFT CARGO STRINGER 29R BETWEEN FR 74 TO FR 82 FOUND WITH SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED STRINGER IAW EMB 170/175 SRM 51-01-01 ,51-41-02 AND 51-43-04SDR SWIA2026030875623Seat Track · corrodedFORWARD WET AREA LT SEAT TRACK CORRODED AROUND THE FORWARD END OF THE MILLED SEAT TRACK AREA BETWEEN FR19-20. PERFORMED REPAIR OF FORWARD WET AREA LT TRACK BEAM BETWEEN FR19-20. REF ETD2026-170-004518 REV.A.SDR SWIA2026030875622Floorbeam · corrodedAFT WET AREA FLOORBEAM CORRODED FR86. REMOVED AND REPLACED AFT WET AREA FLOORBEAM IAW SRM 51-40-08.SDR SWIA2026030875621Seat Track · corrodedFORWARD WET AREA RT TRACK BEAM CORRODED AROUND SCREW HOLE AND FASTENERS AT FR 17. REPAIRED FORWARD WET AREA R/H TRACK BEAM AT FR 17, REF SRM 53-10-10/REPAIR 01P.SDR AALA202603313364Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL AT BS 540 AND LBL 24. REPLACED TRANSITION PANEL PER 51-00-05-01.SDR AALA202603318767Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 500B AND BS 500I AT RBL 24. REPAIRED TRANSITION PANEL PER SRM 51-40-02.SDR SWAA2026033077860Stringer · crackedBS 1016 AFT PRESSURE BULKHEAD, STRINGER 13R CRACKED AT RBL 3.45. REPAIRED IAW EA 26-153-00643.SDR SWAA2026033077527Web · corrodedACB DOOR SURROUND STRUCTURE CORRODED ON THE LOWER INTERCOSTAL WEB, BS 791, RBL 25, WL 159. REMOVED AND REPLACED THE INTERCOSTAL WEB IAW SRM 51-40-02, & DWG 146A8320, REV D.SDR AALA202603272383Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT BS 948 AND LBL 54. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR AALA202603269151Bolt · crackedAIRCRAFT WAS GROUNDED: FORWARD SEVICE DOOR OPERATING MECHANISM SUPPORT BOX FORWARD LOWER BOLT STRUCTURE CRACKED. INSTALLED REPAIRED R1 DOOR, PER 52-41-00. RESET STOP CLEARANCES AND SAFETYED, PER AMM 52-41-00. OPS CHECK GOOD.SDR AALA202603250730Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 68 AND FR 70 AND S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.SDR AALA202603254821Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 68 AND FR 70 AND S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.SDR AALA202603252150Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND AFT CABIN FLOOR SHEAR PLATE AT FR 69 AND S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.SDR AALA202603258400Channel · crackedAIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER J-CHANNEL RIGHT HAND RELIEF CUTOUT IS CRACKED, LOCATED ABOVE THE FRONT SPAR TERMINAL FITTING RIGHT HAND LUG. REMOVED AND REPLACED VERTICAL STABILIZER J-CHANNEL RIGHT HAND RELIEF CUTOUT. PER SRM 51-40-01-0G.SDR IPXA2026032076722Retainer · brokenBROKEN RETAINER, RT WING L/G W/W OUTBD DOOR FWD AND AFT SEAL AREA, QTY:2EA INSTALL NEW RETAINERS I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO.65B10907 SH11 REV.-.SDR IPXA2026032076687Retainer · crackedCRACKED RETAINER, LT WLG W/W OUTBD DOOR AFT SEAL .INSTALL NEW RETAINER I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO.65B10907 SH11 REV.-.SDR SWAA2026032377777Cover · crackedCRACKED GAP COVER, EXTERNAL SKIN BS 291.5, BTWN STR 8R -10R, REPLACED THE GAP COVER IAW SRM 51-40-02, & DWG 141A8350, SHEET 16, REV -.SDR IPXA2026032176637Bracket · crackedCRACK-BRACKET, R/H BODY L/G W/W FLUID TRANSFER ALTERNATE BRAKE SUPPORT BRACKET, STA 1394 (REPLACE) INSTALLED FABRICATED BRACKET I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO 257U2231 SH1 REV.ASDR IPXA2026031675369Skin · crackedCRACK - SKIN , LOWER FACE OF L/H WING T/E INBD MID FLAP T/E UPPER FIXED PNL , WBL 438. (REPAIR) I.A.W AMM 27-51-03-404-008 REV.115 INSTALL THE PIN BETWEEN NO.5 SWING ARM AND SPINDLE.SDR IPXA2026032075538Latch · deformedDEFORMED SKIN , R1 ENGINGE THRUST REVERSER COWL BLOWOUT DOOR INBD EDGE ADJACENT NR 1 LATCH. INSTALL NEW DOOR I.A.W SRM 51-40-02-0G REV.106 AND IPC 78-31-19-02 REV.60.SDR IPXA2026031977449Bracket · crackedCRACK-BRACKET, NO.2 ENG R/H T/R COWL LOWER LATCH HANDLE (REPLACE) I.A.W. AMM 78-31-02-004-001-J00 REV:116 AND AMM 78-31-02-404-007-J00 REV:116, REPLACED THE BRACKET.SDR CALA2026031914679Wire Harness · damagedSTS MSG DOOR AFT CARGO IND WITH MSG 52 11570. REQST MEL APPROVAL. OK TO DEFER AFT CARGO DOOR INDICATION INOP ACP'ED DDG AS MEL REQ'ED. PLACED ITEM ON MEL. DM REF. MX FAULT MSG 52-11570 FIM 52-37 TASK 807. CONFIRMED FAULT CODE 52-11570. PERFORMED FIM 52-37 TASKSDR AALA202603182148Shield · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHIELD BETWEEN BS 420 AND BS 440 AT S25R. REPLACED SHIELD PER AARD 51-00-05-01.SDR AALA202603188513Support Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY SERVICE DOOR THRESHOLD SUPPORT ANGLE BETWEEN BS 309 AND BS 324 AT RBL 62. REPLACED ANGLE PER SRM 51-40-01-0G.SDR IPXA2026031705369Skin · crackedCRACKED SKIN, LOWER FACE OF LT WING T/E INBD MID FLAP T/E UPPER FIXED PANEL , WBL 438. RII COMPLETED FOR THE PIN BETWEEN NR 5 SWING ARM AND SPINDLE OK TO INSTALL.SDR IPXA2026031775549Skin · crackedCRACKED PANEL, RT BODY MLG WW INNER LONGERON BOX AREA ,BS 1372. REPAIRED THE DAMAGE IAW EO-96831,REQ1, REV 1, AND EGAT EI F2026A53M-503, REV 1.SDR IPXA2026031675363Skin · crackedRIGHT WING INBOARD MID FLAP , T/E LOWER SURFACE CRACK. (REPAIR) 3 BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG.SDR AALA202603173338Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 500 AND BS 500A AT S24R. REPLACED TRANSITION PANEL PER SRM 51-40-02.SDR CALA2026031714624Lock · brokenFOUND BROKEN FOWARD NLG LINK LOCK BRACKET. REMOVED LOCK LINK IAW AMM 32-33-51-000-801. COMPLETED INSTALL OF NOSE GEAR MECHANISM UP TO STEP 5.)K NEXT IS LOCK SENSORS. REF AMM 32-33-51-400-801. INSPECTED INSTALL OF NOSE GEAR LOCK MECHANISM UP TO STEP 3.F.(5)SDR CALA2026031714618Window Frame · crackedFLIGHT DECK, WINDSHIELD CTR POST, LOWER NODE, INBD HOLE BOTH LT & RT SIDE HAS CRACK INDICATION AT LOWER SURFACE. LT SIDE: 40% S.H. 6 OCLOCK POS. AT .050 LONG. RT SIDE: 80% S.H. 6 OCLOCK POS. AT 100 LONG. ACCOMPLISHED INTERIM REPAIR AT LT & RT WINDSHIELD FRAMESDR AALA202603167506Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.SDR AALA202603165013Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.SDR VNAA202603140006Skin · scratchedRIGHT FUSELAGE SKIN SCRATCHED. WITHIN 661 FLIGHT HOURS FROM REVISION REQUEST, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IAW APPROVED PROCEDURES OR REPLACE PART. ENGINEERING COMMENTS: SUBMIT AN RFTS WITH UPDATED DAMAGE REPORT.