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 VNAA2026031310001Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM SDR 9WGA2026031345201Skin · crackedWHILE PERFORMING WO 15947, SSID TASK, 4A-5318203-01-WG, INSPECTION FUSELAGE SKIN LONGITUDINAL LAP SPLICES, FOUND 3/4" CRACK STATION 2300, S-46L. PERFORMED LAP SPLICE OVERLAPPING SKIN EXTERNAL REPAIR I/A/W SRM 53-00-01-2R-10, ASSIGNED REP-44-452-159.SDR SWAA2026031267264Access Panel · crackedCRACKED ACCESS PANEL 192F LOWER FUSELAGE. REPLACED ACCESS PANEL IAW AMM 34-32-11-400-802.SDR SWAA2026031267449Skin · delaminatedDELAMINATED OTBD LT WING AFT FLAP. PERFORMED INTERIM REPAIR AT OTBD AFT FLAP, LT WING IAW SRM 57-53-01-2R-16, REPAIR 16, & THE REPAIR REQUIRED TAP TEST INSPECTION EVERY 6;875 CYCLES OR 30 MONTHS. WHICHEVER COMES FIRST.SDR ASAA2026020364808Transition Panel · corrodedAFT PIT LH SIDEPLATE (TRANSITION PANEL) IS CORRODED MULTIPLE SPOTS STA 727-807. GROUNDED - YES. REMOVED CORROSION, DUE TO 100% MAT LOSS, FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-00-53-1A-2 FABRICATED, LOCATED, DRILLED & INSTALLED NEW TRANSITION PANEL SISDR SWAA2026031167430Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED. AFT CARGO BAY FWD CORNER SCUFF PLATE REPAIRED IAW SRM 53-60-15-2R-1.SDR SWAA2026031067085Doubler · corrodedLAV SERVICE DOOR HAS CORROSION ON EXTERIOR SURFACE ON PREVIOUS REPAIR DOUBLER. REMOVED AND REPLACED LAV SERVICE DOOR IAW AMM 52-49-07-000-801; AMM 52-49-07-400-801. BOND CHECK GOOD. BONDING METER: ATS312 11/2026. OPS CHECK GOOD.SDR SWAA2026031067429Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. AFT CARGO BAY AFT CORNER SCUFF PLATE REPAIRED IAW SRM 53-60-15-2R-1.SDR SWAA2026031067437Bear Strap · crackedCRACK NOTED ON R1 DOOR BEAR STRAP AROUND FASTENER, L: 0.3, BS 291.5+4, BETWEEN S8R - 9R, WL 265. REPAIRED IAW SRM 53-10-01-2R-6, AND EA M-25-153-01539.SDR SWAA2026030967382Support · corrodedCORRODED SUPPORT ZEE, BS 500 - 500E, LBL 22, WL 156. THE DAMAGE WAS REPAIRED IAW SRM 53-00-53-2R-5, REPAIR 5, AND EA M-22-153-01550.SDR SWAA2026030967251Support · corrodedCORRODED SUPPORT ZEE, BS 500E - 500I, LBL22, WL 156. 6. REPAIRED THE SUPPORT ZEE IAW SRM 53-00-53-2R-5.SDR SWAA2026030967241Support Angle · crackedCRACKED SUPPORT ANGLE, BS 380 - 400, RBL 10. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G, & DWG 143A5400, SHEET 182, REV-.SDR SWAA2026030967245Angle · crackedCRACKED ANGLE, BS 500H, STR 26L. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A7505, SHEET 137, REV-.SDR SWAA2026030967246Angle · crackedCRACKED ANGLE, BS 500F, STR 26R. REPLACED THE ANGLE IAW SRM 51-10-02, AND DWG 143A7505, SHEET 137, REV -.SDR SWAA2026030967247Angle · crackedCRACKED ANGLE, BS 500G, STR 26R. REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, & DRAWING 143A7505, SHEET 137, REV -.SDR SWAA2026030967248Angle · crackedCRACKED ANGLE, BS 500G, STR 26RL REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A7505, SHEET 137, REV -.SDR SWAA2026030967379Angle · crackedCRACKED ANGLE BS 500A, STR 26R. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, & DWG 143A7505, SHEET 137, REV -.SDR SWAA2026030967244Angle · crackedCRACKED ANGLE, BS 500H, S26L, REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A7505, SHEET 137, REV -.SDR SWAA2026030967381Angle · crackedCRACK GUSSET ANGLE, BS 500I, STR 21L. REPLACED THE GUSSET ANGLE IAW SRM 51-40-02-0G, AND DWG 143A7902. SHEET 256, REV B.SDR SWAA2026030967385Angle · crackedCRACKED GUSSET ANGLE, BS 500I, STR 19R. REPLACED THE GUSSET ANGLE IAW SRM 51-40-02, & DWG 143A7902, SHEET 256, REV B.SDR SWAA2026030967384Angle · crackedCRACKED ANGLE TRAILING EDGE MLG BAY AT LT WING. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, AND DWG 115A2510, SHEET 12, REV-.SDR SWAA2026030967242Support Angle · crackedCRACKED SUPPORT ANGLE LOCATED BETWEEN BS380 - 400, LBL 13. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G AND DRAWING 143A5400, SHEET 182, REV -.SDR SWAA2026030967243Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BETWEEN BS 380 - 400 AND LBL52. REPLACED SUPPORT ANGLE LOCATED BETWEEN BS 380 - 400 AND LBL52 IAW SRM 51-40-02-0G, AND DRAWING 143A5400, SHEET 182, REV -.SDR SWAA2026030667252Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231PF AT PASSENGER CABIN 2026-93281<[01] TOOL USED: CALIPER P/N: 500-752-20. S/N: B21038258; DUE DATE: 06-NOV-26.;[02] TOOL USED: HOT BONDER P/N HCS9200B-AV S/N 18185733 DUE DATE 17-JUL-26;[03] TOOL USED: SCALE P/N: CR5200 S/N: 83425145SDR SWAA2026030667383Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS500A TO BS500E; RBL22 AND WL156 AT FWD CARGO COMPARTMENT 2026-93282<[01] TOOL USED ON Ï¿½TEM 4: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 250592609; DUE DATE: 03-OCT-26<BR><BR>TOOL USED ON Ï¿½TEM 5: ULTRASONIC ESDR SWAA2026030667249Tie Clip · crackedCRACK ON TIE CLIP FLOOR STRUCTURE LOCATED BETWEEN BS500I AND STR26R AT FWD CARGO COMPARTMENT 2026-93269<[01] REPLACED TIE CLIP FLOOR STRUCTURE LOCATED BETWEEN BS500I AND STR26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G-0 AND DWG 143A1234 SHEET: 14 SDR SWAA2026030667250Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS500E TO BS500I; RBL22 AND WL156 AT FWD CARGO COMPARTMENT 2026-93268<[01] TOOL USED ON Ï¿½TEM 4: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 250592609; DUE DATE: 03-OCT-26<BR><BR>TOOL USED ON Ï¿½TEM 5: ULTRASONIC ESDR SWAA2026030667380Web · crackedCRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500A TO BS500B AND STR26R FWD CARGO COMPARTMENT 2026-93285<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS500A TO BS500B AND STR26R FWD CARGO COMPARTMENT I.A.W B737-800 SRM 51-40-02; SRM 51-10-02 ITEM SDR SWAA2026030667253Lanyard · wornWORN EMERGENCY EXIT HATCH LIFE LINE RH SIDE AT PASSENGER CABIN 2026-93265<[01] REPLACED EMERGENCY EXIT HATCH LIFE LINE RH SIDE AT PASSENGER CABIN I.A.W. B737-800 AMM 25-61-10-400-802;[02] TASK COMPLETED AND CERTIFIED.SDR AALA202603069418Flange · corrodedAIRCRAFT IN BASE MAINTENANCE: APU AIR INLET DUCT FLANGE CORRODED. REMOVED CORRODED SPLICE PLATES FROM INLET DIFFUSER DUCT AND INSTALLED NEW SPLICE PLATES. PER AMM 49-15-15.SDR SWAA2026030567342Frame · crackedCRACKED FRAME, BS 312, STRINGERS 5L - 6L, LBL 33. PERFORMED A TRIM OUT OF FRAME IAW EA M-22-153-01244, REV B.SDR AALA202603058900Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING OUTBOARD FLAP AFT SECTION DELAMINATED ON LOWER SKIN INBOARD END RIGHT HAND WING. REPAIRED BY REMOVING LOWER SKIN AND REPLACING WITH A NEW LOWER SKIN. PER AA APPROVED BOEING CMM 57-53-08, BCSRPPM 1.2.10, AND BCSRPPMSDR SWAA2026030367347Frame · crackedCRACKED FRAME, BS 400, S8 - 9L. REPAIRED THE FRAME IAW EA 26-153-00377. ;SDR SWAA2026030367348Frame · crackedCRACKED FRAME, BS 440, S8 - 9L. REPAIRED THE FRAME IAW EA 26-153-00370.SDR SWAA2026030367350Bolt · deterioratedDETERIORATED HARDWARE ON THE GIRT BAR FLOOR BRACKETS. REPLACED THE HARDWARE ON THE GIRT BAR FLOOR BRACKETS FOR SERVICE DOOR IAW AMM 25-66-02-400-801.SDR SWAA2026030367351Bolt · deterioratedDETERIORATED HARDWARE ON GIRT BAR FLOOR BRACKETS. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS IAW AMM 25-66-02-400-801.SDR SWAA2026030367356Support Angle · crackedCRACKED SUPPORT ANGLE, BS 867, STRINGERS 2R - 3R. REPLACED SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 146A7901, SHEET 66, REV A.SDR SWAA2026030267355Frame · crackedCRACKED FRAME, BS 380, BTW S7L - 8L. PERFORMED A REPAIR OF THE FRAME IAW EA 26-153-00379. MAJOR REPAIR WORK PERFORMED.SDR SWAA2026030267357Frame · crackedCRACK ON FRAME LOCATED BS867 AND BTW STR8R TO STR9R AT PASSENGER CABIN. PERFORMED RAPAIR AT FRAME LOCATED BS867 AND BTW STR8R TO STR9R AT PASSENGER CABIN IAW EA 26-153-00378, 26-153-00378-WIP1, AND 26-153-00378-WIP2.SDR SWIA2026022705384Stringer · fomREMOVED STRINGER 2L FORWARD (REFERENCE SRM 53-21-03 ITEM 6) TO FOM. (C-CHECK RO 02/25/2026)INSTALLED STR 2L FORWARD (REFERENCE SRM 53-21-03 ITEM 6) WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLETED M-337. REFERENCE CP# 316SDR SWIA202602275365Frame · damagedREMOVED SUB-FRAME, FS 317 REFERENCE SRM 53-21-23 ITEM 34. INSTALLED SUB-FRAME BS 317 IAW SRM 51-42-06 AND SRM 51-42-21.SDR SWIA2026020375360Fitting · fomREMOVED PAX DOOR FWD LATCH BACKUP FITTING LINTEL IAW DWG SH670-31270 TO FOM. INSTALLED PAX DOOR FWD LATCH BACKUP FITTING LINTEL IAW DWG SH670-31270 WITH REFERENCE TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1002-SKY.SDR SWAA2026022670876Panel · damagedPASSENGER CABIN CEILING BULL NOSE COVE PANEL IS DAMAGED, OR PRIOR REPAIRS ARE PEELING OFF AT 6/7 ABC AND 17/18 ABC. REMOVED AND REPLACED THE BULL NOSE PANELS AT POSITION 6/7 ABC AND 17/18ABC PER AMM 33-51-01. INSPECTED IAW AMM 33-51-01-960-802-NG.SDR AALA202602266625Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT BS 663.5, FROM RBL 9 TO RBL 35. REPLACED ANGLE AARD 51-00-05-1 AND EA 372421.SDR ASAA2026020364521Shield · corrodedAFT DOOR CUT OUT, FWD RH SHIELD IS CORRODED. GROUNDED - YES. REMOVED CORROSION, MAX MAT LOSS .027, FOUND TO BE OUT OF LIMITS, REMOVED & REPLACED IAW B737-900ER SRM 53-60-15-1A-1, SRM 51-40-05 & SRM 51-40-02W= 1.5" O= .050 R= .027 L= 3.0" D= .023.SDR ASAA2026020364520Transition Panel · corrodedAFT CARGO RT SIDEPLATE (TRANSITION PANEL) IS CORRODED MULTIPLE SPOTS STA 727-787. GROUNDED - YES. REMOVED CORROSION, DUE TO 100% MAT LASS, FOUND TO BE OUT OF LIMITS IAW B737-900ER SRM 53-00-53-1A-2, FABRICATED, LOCATED, DRILLED & INSTALLED NEW TRANSITION PANELSDR SWIA2026020375353Skin · damagedFWD FUSELAGE EXTERNAL SKIN HAS EVIDENCE OF LIGHTNING STRIKE AT FR 2 STGR 20L. REPAIRED LIGHTNING STRIKE DAMAGE AT FRAME 2, BETWEEN STRINGERS 23L-24L BY DRILLING THE FUSELAGE EXTERNAL SKIN TO SIZE AND INSTALLING A FREEZE PLUG REF ETD2026-170-002533 REV. B.SDR AALA202602245369Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT STA 987, RBL 47. REPAIRED CHORD PER SRM 53-70-51-2R-6 ALTERNATIVE 4.SDR AALA202602247171Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD AT BS 986, LBL 47. REPAIRED CHORD PER SRM 53-70-51-2R-6 ALTERNATIVE 4.SDR KCSA2026020308Fitting · damagedL1 DOOR WAS VERY DIFFICULT TO OPEN. HANDLE WILL STOP HALF WAY UP. TRANSFERRED TO DMI 100305587 IAW B777 KA MELB 25-10 52-11-01-01B, CAT C, DUE 02-13-26, (M) PROCEDURE C/W. INSTALLED PLACARD. 100305786: REF DMI 100305587 L1 DOOR INOP. PERFORMED ENTRY DOOR