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.

SDR JR2R20260221300Sill Drain · corrodedFWD WET AREA, LT MOP SILL AT LBL40 FR16 IS CORRODED. REPAIRED PER ETD.Feb 21, 2026 · N86312 · Emb ERJ170200LR · Fuselage Main, StructureSDR JR2R20260221296Doubler · corrodedFWD WET AREA, R/H FLOOR DOUBLER AT RBL40 BETWEEN FR12-FR14 IS CORRODED. REPAIRED PER ETD.Feb 21, 2026 · N86312 · Emb ERJ170200LR · Fuselage Main, StructureSDR JR2R20260221298Doubler · corrodedFWD WET AREA, RT BANJO DOUBLER AT RBL40 FR17 IS CORRODED AT FWD END. REPAIRED PER ETD.Feb 21, 2026 · N86312 · Emb ERJ170200LR · Fuselage Main, StructureSDR SWIA2026022076064Guide · chafedLH WING TE AT FSL168.63, THE ROLLER GUIDE FITTING FOR LH FLAP ROLLER CAM FITTING IS CHAFED (WEAR SIGN) REMOVE AND REPLACED WITH NEW ROLLER GUIDE FITTING. REF: CRJ-900-SRM-51-42-06-001-001-A01. COMPLIED WITH ALL STEPS ON TASK CARD 51-900-1002-SKY. SEE CONTINUFeb 20, 2026 · N899SK · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2026042800378Support Bracket · crackedCRACK ON CORNERS OF (BRACKET ASSY) MAIN BATTERY DIRECT BUS (JB6) AT FWD EQPT COMPT (BRACKET ASSY) MAIN BATTERY DIRECT BUS (JB6) AT FWD EQPT COMPT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01.Feb 20, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026042800377Bracket · corrodedCRACK ON UPPER STABILIZER BRACKET AT GALLEY SERVICE DOOR UPPER STABILIZER BRACKET AT GALLEY SERVICE DOOR WAS REPLACED PER CRJ 900 AMM 52-41-27Feb 20, 2026 · N297PQ · Cndair CL6002D24 · Service DoorsSDR IPXA2026031524636Adapter · corrodedMAJOR REPAIR. MAIN DECK-CLS ADAPTER FR30 YO IS CORRODED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96669-REQ1 AND VT-MAE EA 300-5314-27-A4358 REV. - .Feb 20, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031524630Adapter · corrodedMAJOR REPAIR. MAIN DECK-CLS ADAPTER FR32 YO IS CORRODED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96669-REQ1 AND VT-MAE EA 300-5314-27-A4358 REV. - .Feb 20, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031524730Adapter · corrodedMAJOR REPAIR. MAIN DECK-CLS ADAPTER FR36 YO IS CORRODED-109-124-VWV. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96669-REQ1 AND VT-MAE EA 300-5314-27-A4358 REV. - .Feb 20, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031524756Adapter · corrodedMAJOR REPAIR. MAIN DECK-CLS ADAPTER FR38 YO IS CORRODED-109-122-VWV ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96669-REQ1 AND VT-MAE EA 300-5314-27-A4358 REV. - .Feb 20, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031624780Adapter · corrodedMAJOR REPAIR. MAIN DECK-CLS ADAPTER FR38.1 YO IS CORRODED-109-120-VWV VERIFIED ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96669-REQ1 AND VT-MAE EA 300-5314-27-A4358 REV. - . AND UPS GMM 04.02.01.15 MAJOR REPAIRFeb 20, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031524510Adapter · corrodedMAJOR REPAIR, MAIN DECK CLS ADAPTER, FR 30, Y0 CORRODED. ACCOMPLISHED PERMANENT REPAIR IAW EO-96669-REQ1, AND EA 300-5314-27-A4358, REV -.Feb 20, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031524823Adapter · corrodedMAJOR REPAIR, MAIN DECK CLS ADAPTER FR 38.2, Y0 CORRODED. ACCOMPLISHED A PERMANENT REPAIR IAW EO-96669-REQ1, AND EA 300-5314-27-A4358, REV- .Feb 20, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031924843Adapter · corrodedMAJOR REPAIR, MAIN DECK CLS ADAPTER FR 55, Y0 RT IS CORRODED. ACCOMPLISHED PERMANENT REPAIR IAW EO-96670-REQ1, AND EA 300-5316-27-A4359, REV - .Feb 20, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031924827Adapter · corrodedMAJOR REPAIR, MAIN DECK CLS ADAPTER FR 55 Y0 CORRODED. ACCOMPLISHED PERMANENT REPAIR IAW EO-96670-REQ1, AND EA 300-5316-27-A4359, REV-A.Feb 20, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026033172773Panel · damagedELONGATED HOLE ON ACCESS PANEL 192HR, WING TO BODY FAIRING. REPAIRED THE ACCESS PANEL 192HR IAW SRM 51-70-04-2R-10, REPAIR 10.Feb 20, 2026 · N8633A · Boeing 7378H4 · Aerodynamic FairingsSDR SWAA2026033172464Seat Track · deterioratedDETERIORATED SEAT TRACK FITTING ON ROW 1(2EA) 11(1EA) 30(1EA) RT SIDE AT PASSENGER CABIN . REPLACED SEAT TRACK FITTING ON ROW 1(2EA) 11(1EA) 30(1EA) RT SIDE AT PASSENGER CABIN (4EA) IAW CMM-25-22-46 REV.9 PAGE 10220, FIGURE 25 ITEM 70 AND PAGE 7003 STEP 3.B.(Feb 20, 2026 · N8633A · Boeing 7378H4 · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031810473Floor Panel · gougedAPPROX. 1 INCH LINE GOUGE, DIRT/ DEBRIS ON AFT CARGO FLOOR PANEL TAGGED, FROM BS 1460 - 1500. BLENDED DAMAGE. ORIGINAL MATERIAL THICKNESS IS .071, MATERIAL REMOVED IS .021. FABRICATED, LOCATED, DRILLED AND COUNTERSUNK NEW FLOOR PANEL 161AF IAW SRM 51-40-05-Feb 20, 2026 · N422UP · Boeing 75724APF · Fuselage Floor PanelSDR AALA202603318560Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.Feb 20, 2026 · N980UY · Airbus A321231 · Fuselage Miscellaneous StructureSDR SWAA2026033072465Strip · corrodedCORRODED FLOOR AREA CAP STRIP, BS 947.5 IN THE AFT CARGO BAY. REPLACED THE CAP STRIP IAW SRM 51-10-02, ITEM 9.Feb 20, 2026 · N8633A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026033072483Fitting · deterioratedDETERIORATED GIRT BAR FITTINGS HARDWARE AT THE ENTRY AND SERVICE DOORS. REPLACED THE GIRT BAR FITTINGS HARDWARE IAW AMM 25-66-02-400-801, STEP 3.D (1) ITEM (H); (J), AND (K).Feb 20, 2026 · N8633A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026033072654Light · burnedBURNED OVERWING EXIT LIGHT RIGHT ROW 14. REPLACED OVERWING EXIT LIGHT RIGHT ROW 14 IAW AMM 33-21-00-960-805.Feb 20, 2026 · N8633A · Boeing 7378H4 · Emergency LightingSDR SWAA2026033072657Light · burnedBURNED OVERWING EXIT LIGHT LEFT ROW 14. REPLACED OVERWING EXIT LIGHT LEFT ROW 14 IAW AMM 33-21-00-960-805.Feb 20, 2026 · N8633A · Boeing 7378H4 · Emergency LightingSDR SWAA2026033072482Nut · deterioratedDETERIORATED AFT ENTRY DOORWAY LINER ASSIST HANDLE NUTS 2EA. REPLACED AFT ENTRY DOORWAY LINER ASSIST HANDLE NUTS 2EA IAW AMM 25-21-25-420-801, STEP 3.B. ITEM (5).Feb 20, 2026 · N8633A · Boeing 7378H4 · Passenger/Crew DoorsSDR A6WA202602208881Door · bindingLEFT OVERWING EXIT WILL NOT OPEN FREELY. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPS CHECK OF OVERWING EMGERGENCY EXIT IAW AMM 52-21-00. PERFORMED OPS CHECK OF OVERWING EMGERGENCY EXIT IAW AMM 52-21-00. DOOR OPENS AND CLOSES FREELY, COMPLIED WITH CM ACTFeb 20, 2026 · N463AW · Cndair CL6002B19 · Emergency ExitsSDR ASAA2026022065116Floorbeam · corrodedMAIN CABIN, AFT WET AREA, FLOORBEAM, BS 986.5 FOUND CORRODED AT MULTIPLE AREAS. GROUNDED - YES. REMOVED THE DAMAGE ON THE FLOORBEAM, BS 986, RBL 20 - LBL 20, FOUND TO BE IN LIMITS IAW SRM 53-70-51-1A-1, REPAIRED THE FLOORBEAM, BS 986.5, RBL20 - RBL30 &Feb 20, 2026 · N546AS · Boeing 737890 · Fuselage Main, Floor BeamSDR HNAA2026032600243Skin · crackedREAR FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACK AROUND RIVET AT FR 78 BETWEEN STGR 4L / 5L. PERFORMED CUTOUT OF CRACK AROUND RIVET ON REAR FUS EXTERNAL SKIN AT FR 78 AND BTW STR 4L-5L AND PERFORMED PERMANENT REPAIR OF SKIN AT FR 78 AND BTW STR 4L-5L IAW PIEDMOFeb 20, 2026 · N699AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SWAA2026032472671Angle · crackedCRACKED ANGLE, BS 500C, STRINGER 26L. REPLACED THE ANGLE, & FASTENERS IAW SRM 51-40-02, & DWG 143A7505, SHEET 84, REV -.Feb 20, 2026 · N920WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032472675Angle · crackedCRACKED ANGLE, BS 400, S26L. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 143A7505, SHEET 81, & 82, REV - .Feb 20, 2026 · N920WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032472673Gusset · crackedCRACKED GUSSET, BS 500D, STRINGER 19L. REPLACED THE GUSSET AND FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7902, SHEET, 209, REV - .Feb 20, 2026 · N920WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026032472672Gusset · crackedCRACKED GUSSET, BS 500D, STRINGER 19R. REPLACED THE GUSSET AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 143A7902, SHEET, 209, REV - .Feb 20, 2026 · N920WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR AALA202603244066Megaphone · crackedAIRCRAFT IN BASE MAINTENANCE: RED MEGAPHONE HAS CRACK. LOCATED IN FWD CREW REST LOWER EMERGENCY EQUIPMENT COMPARTMENT. MAINTENANCE REPLACED CRACKED MEGAPHONE WITH SERVICEABLE MEGAPHONE IAW AMM 25-64-02.Feb 20, 2026 · N772AN · Boeing 777223 · Emergency EquipmentSDR SWAA2026032372786Angle · corrodedCORRODED ANGLE, BS 947.5, STRINGERS 26R - 27R, WL 148.5. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, DWG 147A1047, SHEET 107, REV-, & DWG 147A7500, SHEET 25, REV-.Feb 20, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR AALA202603234945Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.Feb 20, 2026 · N980UY · Airbus A321231 · Fuselage Miscellaneous StructureSDR SWAA2026032072661Shield · corrodedCORROSION SHIELD WEB BTW STA 492.4 AND BTW STA 500A STR 26R AND WL 152 AT FWD CARGO BAY. REPLACED SHIELD WEB BTW STA 492.4 AND BTW STA 500A STR 26R AND WL 152 AT FWD CARGO BAY IAW SRM 51-10-02; SRM 51-40-02 AND DWG: 143A0080 SHEET: 39 REV -.Feb 20, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026032007903Wire · out of position***SUPPLEMENTAL SDR*** FAULT - AVI, Z800, CREW DOOR INNER SURFACE, BEHINDE ARM/DESARM HANDLE HAS ELECTRICAL WIRE TOUCHING W/ MECHANISM (SHAFT). DOT 103-36 (RED FLAG) SEPARATED AND SECURED ELECTRICAL WIRE BEHIND CREW DOOR INNER SURFACE, BEHIND ARM/DESARM HANDFeb 20, 2026 · N135UP · Airbus A300F4622R · Door System WiringSDR SWAA2026031972750Bracket · crackedCRACK TRAILING EDGE BRACKET, ORSS 270, LT WING. REPLACED THE BRACKET IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02-0G-0, & DWG 115A2030, SHEET 6, REV-.Feb 20, 2026 · N463WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2026031972753Bracket · crackedCRACK TRAILING EDGE BRACKET, ORSS 280 INTERNAL CAVITY AT RT WING. REPLACED THE BRACKET IAW SRM 51-10-02, PARA 9, SRM-51-40-02-0G-0, & DWG 115A2930, SHEET 6, REV-.Feb 20, 2026 · N463WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2026031972754Support Bracket · damagedELONGATED HOLE ON THE RT WING ACCESS PANEL 651GB SUPPORT BRACKET. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, SRM 51-40-02, & DWG 115A2714, SHEET 4, REV-.Feb 20, 2026 · N463WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2026031972755Access Panel · damagedELONGATED HOLE ON LT WING ACCESS PANEL 561AB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.Feb 20, 2026 · N463WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2026031972751Support Angle · crackedCRACKED TRAILING EDGE SUPPORT ANGLE, LT WING ORSS 269. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02-0G-0, PARAGRAPH 9.Feb 20, 2026 · N463WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR AALA202603182915Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON SKIN DOUBLER UNDER ETWLU ANTENA @ FR42-FR43, STR 1R TO STR 1L. MAINTENANCE REPLACED SKIN DOUBLER IAW SRM 51-42-11-801 AND DWG SI17-016-01 SHEET 9, DETAIL H.Feb 20, 2026 · N8027D · Airbus A319115 · Fuselage Main, Plate/SkinSDR ASAA2026022064885Skate Angle · crackedCENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE CRACKED AT BS.661.96 LBL+9. GROUNDED - YES. REPAIRED CENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE AT BS 661.96 LBL+9 IAW B737-900ER SRM 57-10-10-2R-5 REPAIR 5.Feb 20, 2026 · N281AK · Boeing 737990ER · Fuselage Miscellaneous StructureSDR ASAA2026022064884Skate Angle · crackedCENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE CRACKED AT BS.661.96 RBL +9. GROUNDED - YES. REPAIRED CENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE AT BS 661.96 RBL+9 IAW B737-900ER SRM 57-10-10-2R-5 REPAIR 5.Feb 20, 2026 · N281AK · Boeing 737990ER · Fuselage Miscellaneous StructureSDR AALA202603130605Skin · wornAIRCRAFT IN BASE MAINTENANCE: WEAR TO SLAT NUMBER 9 WEDGE LOWER SKIN. REPLACED SLAT WEDGE SKIN PER SRM 57-43-02-1A.Feb 20, 2026 · N772AN · Boeing 777223 · Leading Edge DevicesSDR REXA2026031300237Seal · leakingWHILE AT FL 310 I NOTICED L OIL LOW. BEGAN MONITORING OIL INIDCATIONS. EVENTUALLY RECEIVED A L ENG OIL PRESS WARNING MESSAGE. FOLLOWED CRJ 900 QRH 1-20 AND 1-22 AS DIRECTED. SHUTDOWN LEFT ENGINE IN FLIGHT AS DIRECTED BY QRH. REPLACEED OF LT ENGINE C SUMP INFeb 20, 2026 · N348PQ · Cndair CL6002D24 · Turbine Engine Oil SystemSDR CALA2026031314561Skin · corrodedFOUND CORROSION AFT OF AFT CARGO BAY SKIN PANEL AT LAV VENT DUCT BASE BETWEEN BS 907 & 927, S-21L & S-22L. FABRICATED AND INSTALLED REPAIR PARTS AT LT FUSELAGE SKIN BETWEEN BS 907 & 927 BETWEEN S-21L & S-22L IAW SRM 51-40-02-0G-0 AND SRM 53-70-01-2R-3.Feb 20, 2026 · N35236 · Boeing 737824 · Fuselage Main, Plate/SkinSDR IPXA2026030926467Floor Panel · damagedMAJOR REPAIR. MCD FLOOR PANEL 231MJ DAMAGED. FABRICATION IS COMPLETE ON PANEL 231MJ IAW SREO-16407-REQ001 ((APPX B).Feb 20, 2026 · N135UP · Airbus A300F4622R · Fuselage Floor PanelSDR SWAA2026031172744Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. FABRICATION OF NEW 231XF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.Feb 20, 2026 · N246LV · Boeing 7377H4 · Fuselage Floor PanelSDR IPXA2026030825078Longeron · damagedNR 2 ENG-PANEL RACK-485AL FWD O/B TOP LONGERON 1ST 2 HOLES HAVE WEAR -109-101-VWV. UPPER LONGERON REMOVED AND REPLACED IAW A300-600, SRM51-40-21-001, SRM 51-72-10-001.Feb 20, 2026 · N135UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame