Service difficulty reports

1,771,154 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 SWIA2026060377054Bulkhead Web · corrodedBS 280 BULKHEAD LEFT UPPER WEB CORRODED, INBD SIDE AT WL 79.50. REMOVED AND INSTALLED A -1 L/H LOWER WEB, -3 BUTTSTRAP -5, AND -7 SHIM ON BS 280 BULKHEAD IAW SRM 53-11-10-201-004-A01.Jun 3, 2026 · N792SK · Cndair CL6002C11 · Fuselage Main, BulkheadSDR SWIA2026060377053Plate · crackedFORWARD BAGGAGE BAY LEFT SIDE NP PLATE CRACKED ON BS 613 FRAME. INSTALLED A NEW FABRICATED NP PLATE OF FWD BAGGAGE BAY ON FRAME BS 613, IAW DWG SH670-33600, REV AD, AND SRM 51-42-06-001-001-A01.Jun 3, 2026 · N792SK · Cndair CL6002C11 · Fuselage Main, StructureSDR SWIA2026060377052Fitting · corrodedPASSENGER DOOR SURROUND CLOSING FITTING, STGR 18L, BS 314, CORRODED. INSTALLED A NEW PASSENGER DOOR LOWER CLOSING FITTING IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-31810 REV AE.Jun 3, 2026 · N792SK · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWIA2026060377049Floorbeam · corrodedBS 280 FLOORBEAM CORRODED. REMOVED AND INSTALLED A NEW BS 280 FLOORBEAM IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, REVISION 38, & DWG CC670-34010, REV -K.Jun 3, 2026 · N792SK · Cndair CL6002C11 · Fuselage Main, Floor BeamSDR SWIA2026060377046Crossbeam · crackedBS 280 CROSSBEAM RBL 9 OTBD ANGLE CRACKED. REMOVED AND INSTALLED A NEW BS 280 CROSSBEAM RBL 9 OTBD ANGLE IAW SRM 51-42-21-001-001-A01, REVISION 38, & DWG NO CC670-34010, REV K.Jun 3, 2026 · N792SK · Cndair CL6002C11 · Fuselage Main, StructureSDR SWIA2026060377039Floorbeam · crackedBS 280 CROSSBEAM LBL 9 OTBD ANGLE CRACKED. REMOVED & INSTALLED NEW BS 280 CROSSBEAM LBL 9 OTBD ANGLE IAW SRM 51-42-21-001-001-A01, REVISION 38, & DWG CC670-34010, REV K. CW SKYWEST TASKCARD 51-900-1002-SKY.Jun 3, 2026 · N792SK · Cndair CL6002C11 · Fuselage Main, Floor BeamSDR SWIA2026060377033Fitting · corrodedPASSENGER DOOR SURROUND CLOSING FITTING, STR 18L, BS 342 CORRODED. INSTALLED NEW PASSENGER DOOR LOWER CLOSING FITTING, STR 18L, BS 342 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-31810, REV AE C/W TASK CARD 51-900-1002-SKY.Jun 3, 2026 · N792SK · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWIA2026060377029Bulkhead Web · corrodedBS 280 BULKHEAD RIGHT UPPER WEB CORRODED INBOARD SIDE AT WL 79.50. REMOVED & WET INSTALLED ALL REPAIR PARTS -2 LOWER WEB, -4 BUTT STRAP, -6 AND -8 SHIM IAW SRM 53-11-10-201-004-A01. COMPLIED WITH SKYCARD 51-900-1002-SKY.Jun 3, 2026 · N792SK · Cndair CL6002C11 · Fuselage Main, BulkheadSDR SWIA2026060376913Lug · gougedRWS 178 AFT INBD AND OTBD FLAP HINGE BOX LUG FITTING GOUGED. REPAIRED GOUGED DAMAGES IAW REO 601R-57-21-4108, REV -. COMPLIED WITH SKY CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR.Jun 3, 2026 · N936EV · Cndair CL6002B19 · AileronsSDR SWIA2026060376808Lintel · gougedAFT BAGGAGE BAY LINTEL AFT SIDE STARTING TO GOUGE BY DOOR CABLE. INSTALLED -1 REPAIR ANGLE IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01, COMPLYING WITH ALL STEPS OF REO 670-53-61-2735, REV -, COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY, SEE Jun 3, 2026 · N719SK · Cndair CL6002C10 · Cargo/Baggage DoorsSDR REXA2026080401443Door Frame · corrodedSECONDARY NRC FROM NRC 290: CORROSION ON INNER CHORD (3EAS) BTW FS1000 TO FS1047 AT AFT BAGGAGE DOOR SURROUND STRUCTURE LOWER SIDE. CORROSION ON INNER CHORD (2EAS) BTW FS1000 TO FS1047 AT AFT BAGGAGE DOOR SURROUND STRUCTURE LOWER SIDE WAS REMOVED PER CRJ/900 SJun 3, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026080401442Angle · corrodedSECONDARY NRC FROM NRC 00099 AND 00100: AFTER REMOVAL, CORROSION ON ANGLE SUPPORTS (2EA) OF ACCESS PANELS 542AZ AND 642AZ. CORROSION ON ANGLE SUPPORTS (2EA) OF ACCESS PANELS 542AZ AND 642AZ WAS REMOVED PER SRM 51-21-06-001-001-A01 AND ANGLE SUPPORT (1EA) OF ACJun 3, 2026 · N146PQ · Cndair CL6002D24 · Wing Miscellaneous StructureSDR IXXA2026072701Angle · crackedVERTICAL ANGLE ON FRONT SIDE OF FRAME 1085 RBL 26 IS CRACKEDJun 3, 2026 · N379AZ · Boeing 767323 · Fuselage Miscellaneous StructureSDR R61A2026072200200Seal Rest · corrodedDURING HEAVY CHECK FWD CARGO DOOR CUTOUT FWD LOWER SEAL REST FOUND WITH CORROSION. REMOVED AND REPLACED SEAL REST IAW EMB 170/175 SRM 51-41-01Jun 3, 2026 · N213JQ · Emb ERJ170100LR · Fuselage Main, StructureSDR REXA2026070701015Hinge · corrodedCORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER. DUE TO EXCESSIVE CORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER WERE REPLACED IAW SRM 51-10-06-001-001-A01 AND SRM 51-41-02-001-001-A01.Jun 3, 2026 · N927XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR IPXA2026070679800Skin · dentedDENT ON LEADING EDGE SLAT #7. VIEW ATTACHMENTS. WILL REQUIRE LINE MX 8 HOURS EXTEND AND LOTO L/E SLATS. S/M SHOP 40 HOURS TO REPAIR PER SRM 57-43-01-2R-2 RP. 2 THIS IS PRIMARY STRUCTURE MAJOR REPAIR. HANGAR NOT REQUIRED WITH GOOD WEATHER AND MATERIALS IN STOCKJun 3, 2026 · N310UP · Boeing 76734AF · Leading Edge DevicesSDR SWAA2026070608959Support Angle · crackedCRACKED SUPPORT ANGLE, BS 380 - 400, RBL 10, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A5400, SHEET 139, SHEET 184, REV -.Jun 3, 2026 · N8641B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026070608961Support Angle · crackedCRACKED SUPPORT ANGLE BTW BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, AND DWG 143A5400, SHEET 182, SHEET 184, REV-.Jun 3, 2026 · N8641B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026070608960Support Angle · crackedCRACKED SUPPORT ANGLE BTWN BS 380 - 400, LBL 51, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A5400, SHEET 139, REV-.Jun 3, 2026 · N8641B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026070609082Support Angle · crackedCRACKED SUPPORT ANGLE, BS 867, STRINGER 26L IN THE CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, & SRM 51-10-02, ITEM 9.Jun 3, 2026 · N8641B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR REXA2026070301014Hinge · corrodedCORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER. DUE TO EXCESSIVE CORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER WERE REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01 AND SRM 51-41-02-001-001-A01Jun 3, 2026 · N927XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026070301013Hinge · corrodedCORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER. DUE TO EXCESSIVE CORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER WERE REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01 AND SRM 51-41-02-001-001-A01Jun 3, 2026 · N927XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026070301012Hinge · corrodedCORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER. DUE TO EXCESSIVE CORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER WERE REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01 AND SRM 51-41-02-001-001-A01Jun 3, 2026 · N927XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026070301004Acoustic Panel · crackedCRACK ON ACOUSTIC PANEL AFTER REMOVAL OF ZEE STIFFENER AT LH UPPER TRANSCOWL ACOUSTIC PANEL AT LT UPPER TRANSCOWL WAS REPAIRED PER EA NO CRJ954-22246 REV IR.Jun 3, 2026 · N927XJ · Cndair CL6002D24 · Engine Thrust ReverserSDR HNAA2026070300571Floorbeam · corrodedWARDROBE FLOORBEAM ANGLE AT FRAME 18 HAS CORROSION. REMOVED AND REPLACED WARDROBE FLOORBEAM ANGLE AT FRAME 18 IAW EMB 145 SRM 51-40-02.Jun 3, 2026 · N923AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR SWAA2026070209081Web · crackedCRACKED WEB LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT. REPLACED WEB LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9 AND DWG 147A7500, SHEET 37, REV-.Jun 3, 2026 · N8641B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR DALA2026062503775Door · missingTOILET SERVICE DOOR MISSING. INSTALLED NEW LAV SERVICE DOOR PER B737 AMM 52-49. (LOG 8051507 - AIRCRAFT WAS GROUNDED).Jun 3, 2026 · N3736C · Boeing 737832 · Fluid Service DoorsSDR SWAA2026062409094Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING. REPLACED FASTENERS AND CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING IAW SRM 51-40-02 AND DWG 115A2713 SHEET 3, REV A.Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing Main, Frame StructureSDR SWAA2026062409092Plate · crackedCRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS272 AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS ON TRAILING EDGE LOCATED ORSS 272 AT RT WING IAW SRM 51-40-02.Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing Main, Frame StructureSDR SWAA2026062409093Plate · crackedCRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT RT WING IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A2001; SHEET: 1; REV B.Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing Main, Frame StructureSDR SWAA2026062408976Fitting · damagedELONGATED HOLE ON FITTING TRAILING EDGE LOCATED ORSS256 AT LT WING. REPLACED FITTING LOCATED ON TRAILING EDGE ORSS 256 AT LT WING IAW SRM 51-40-02-0G-0, SRM 51-10-02 ITEM 9, DWG 115A5300 SHEET 17, REV- .Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing Main, Frame StructureSDR SWAA2026062409091Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS272 AT LT WING. REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED ORSS272 AT LT WING IAW SRM 51-40-02 AND DWG 115A2714; SHEET 6; REV: -. DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM 57-51-02-1A-1 ALLOWABLE DAMAGE 1Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing Main, Frame StructureSDR SWAA2026062408975Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561CB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561CB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-9, REPAIR 9.Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing, Plate/SkinSDR SWAA2026062408977Access Panel · damagedELONGATED HOLES ON FITTING ACCESS PANEL 651GB AT RT WING. REPLACED FITTING ACCESS PANEL 651GB AT RT WING IAW SRM 51-40-02, SRM 51-10-02 ITEM 9, AND DWG 115A2714 SHEET 6 REV -.Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing, Plate/SkinSDR SWAA2026062408974Access Panel · damagedELONGATED HOLES ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-9 REPAIR 9.Jun 3, 2026 · N7876A · Boeing 7377Q8 · Wing, Plate/SkinSDR SWAA2026062309065Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 219 AT LT WING. REPLACED CORRUGATED PLATE LOC. ON TRAILING EDGE IRSS 219 AT LT WING IAW SRM 51-40-02-0G-0 AND 51-10-02-0G-0, ITEM 9.Jun 3, 2026 · N476WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2026062309073Plate · crackedCRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 250 AT LT WING. PERFORMED VISUAL INSPECTION IAW SRM 51-10-04-0G-0 ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 250 AT LT WING AND NOT FOUND CRACK ONLY BROKEN FASTENER HEAD (2/EA) REMOVED AND INSTALLED FASJun 3, 2026 · N476WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2026062308953Angle · crackedCRACKED ANGLE TRAILING EDGE LOCATED ORSS 271 RT WING. REPLACED ANGLE T/E LOCATED ORSS 271 RT WING IAW SRM 51-40-02-0G-0, DWG 115A2930, SHEET 6, REV-.Jun 3, 2026 · N476WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2026062308954Fastener · brokenCRACKED CORRUGATED PLATE T/E LOCATED ORSS 261 AT RT WING. PERFORMED VISUAL INSPECTION IAW SRM 51-10-04 ON CORRUGATED PLATE T/E LOCATED ORSS 261 AT RT WING AND NOT FOUND CRACK ONLY BROKEN FASTENER HEAD (1 E/A). REMOVED AND INSTALLED FASTENER IAW SRM 51-40-02, Jun 3, 2026 · N476WN · Boeing 7377H4 · Wing Main, Frame StructureSDR IPXA2026061694292Angle · crackedLEFT WING, FIXED L/E, INBD SIDE, INTERNAL STRUCTURE, JUST NEXT TO KRUEGER FLAP COMPARMENT, ANGLE WITH A CRACK 1/2 LONG. REMOVED ANGLE WITH CRACK IAW SRM 51-40-21. INSTALLED ANGLE IN LT WING, FIXED L/E, INBD SIDE, INTERNAL STRUCTURE IAW SRM 51-40-21.Jun 3, 2026 · N161UP · Airbus A300F4622R · Wing, Attach FittingsSDR IPXA2026062395002Wire · brokenCREW DOOR CUTOUT, HINGE BONDING WIRE BROKEN. INSTALLED TERMINAL LUG AT BONDING JUMPER CREW DOOR IAW ESPM 20-56-22-03 AND INSTALLED BONDING JUMPER IAW AMM 20-28-11/001. BONDING TESTED GOOD.Jun 3, 2026 · N161UP · Airbus A300F4622R · Door System WiringSDR SIMA20260603002Seat Track · corrodedFWD GALLEY RT CENTER FLOOR BEAM CORRODED BETWEEN FR 13-15. (LVL1 CORROSION)(MAJOR REPAIR) ACCOMPLISHED A PERMANENT REPAIR ON FWD GALLEY RH CENTER FLOORBEAM BETWEEN FR 14-15 IAW ERS-EJ-53MR-5456. FR 13-14 WAS FOUND TO BE WITHIN LIMITS IAW SRM 53-10-10AD01.Jun 3, 2026 · N209NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026062208737Web · crackedCRACKED DOUBLER WEB LOCATED ON BS 663.75 VAPOR BARRIER AREA BTW RBL 6.15 AND RBL 31.83. REPLACED WEB LOCATED ON BS 663.75 VAPOR BARRIER AREA BTW RBL 6.15 AND RBL 31.83 IAW SRM 51-40-02; SRM 51-10-02, AND DWG 111A1001 SHEET 504, REV -.Jun 3, 2026 · N951WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026062208736Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 193B (LEFT SIDE) BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193B (LEFT SIDE) BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-10 REPAIR 10.Jun 3, 2026 · N951WN · Boeing 7377H4 · Aerodynamic FairingsSDR IPXA2026062294734Roller Guide · damagedCREW DOOR CUTOUT, LOWER FWD ROLLER GUIDE DAMAGED. INSTALLED ROLLER GUIDE ON CREW DOOR CUTOUT, LOWER FWD IAW AMM 52-10-31.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026062294928Roller · damagedCREW DOOR, FWD LOWER ROLLER DAMAGED. REMOVED AND REPLACED AT CREW DOOR, FWD LOWER ROLLER IAW AMM 52-11-21/401.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026062295167Roller · damagedCREW DOOR, AFT LOWER ROLLER DAMAGED. REMOVED AND REPLACED AT CREW DOOR, AFT LOWER ROLLER IAW AMM 52-11-21/401.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026062295164Bracket · damagedCREW DOOR, AFT LOWER ROLLER BRACKET DAMAGED. REMOVED AND REPLACED AT CREW DOOR, AFT LOWER ROLLER BRACKET IAW AMM 52-11-21/401.Jun 3, 2026 · N161UP · Airbus A300F4622R · Passenger/Crew DoorsSDR SWAA2026061708719Wire · brokenRIGHT SIDEWALL PANEL 232ZLW AT STA 616 HAS BROKEN EXIT LIGHT WIRE RT SIDEWALL PANEL 232ZLW AT BS 616. REMOVED, REPLACED AND PERFORMED GOOD OPS CHECK OF THE EXIT LIGHT ASSEMLY AT RT SIDEWALL PANEL 232ZLW AT BS 616 IAW AMM 33-51-01-960-802.Jun 3, 2026 · N8312C · Boeing 7378H4 · Light System WiringSDR IPXA2026061794650Door Frame · gougedCREW DOOR CUTOUT, UPPER FWD CORNER HAS A GOUGE. REMOVED MINOR GOUGE AT CREW DOOR CUTOUT, UPPER FWD CORNER IAW 51-10-10-101 AND ORIGINAL THIKNESS 0.265" MATERIAL LOST 0.003" REMAINING MATERIAL 0.262" FOUND WITH IN LIMITS IAW SRM 51-73-11-001. RESTORE SURFACE PRJun 3, 2026 · N161UP · Airbus A300F4622R · Fuselage Main, Structure