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 SCNA20260616251Stringer Clip · crackedCRACK ON FRAME/STR CLIP ON STA 500H AND STGR 19RT AT FWD CARGO COMPARTMENT. CLIP FRAME/STGR ON STA 500H AND STR 19RT AT FWD CARGO COMPARTMENT WAS REPLACED IAW SRM 51-40-02-0G-0.May 6, 2026 · N827SY · Boeing 7378F2 · Fuselage Main, Attach FittingsSDR IPXA2026061253788Keelbeam · crackedMAJOR REPAIR, THE RT SIDE, BOTTOM FWD FASTENER HOLE BETWEEN FR13A & 14, IS IN AN OUT OF ROUND CONDITION AND IS GOUGED AROUND THE FASTENER HOLE ON THE BEAM FACE. ACCOMPLISHED THE REPAIR IAW EO-97712-REQ1 AND EA 300-5312-27-A4495, REV-, & GMM 04.02.May 6, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, KeelSDR IPXA2026061153760Keelbeam · crackedMAJOR REPAIR, THE LT SIDE, FWD BOTTOM KEELBEAM FASTENER HOLE BETWEEN FR13A & 14, HAS A CRACK IND. (1EA) BETWEEN THE 6 & 7 O'CLOCK POSITION. ACCOMPLISHED THE REPAIR PER EO-97711-REQ1 AND EA 300-5312-27-A4494, REV-, & GMM 04.02.May 6, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, KeelSDR IPXA2026052045853Strap · corrodedWHILE EVALUATING CORROSION AT APU INLET SURROUND STRUCTURE FOUND CORROSION AT APU AREA AFT STRAP AT STA 1825 BETWEEN STR 3R-6R. REPAIR ACCOMPLISHED PER B757-200PF SRM 53-80-15-2R-1 REPAIR 1.May 6, 2026 · N417UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026061051655Seat Track · contaminatedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SEAT TRACK ASSY HAS MULTIPLE NUT PLATE CORRODED APPROX BTW BS 1661 AND BS 1681, LBL 24.75, ACCOMPLISHED REPAIR PER B757-200PF SRM 53-00-52-2R-5 REPAIR 5 REVISION 124.May 6, 2026 · N417UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026051551707Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK ASSY HAS MULTIPLE NUT PLATE CORRODED APPROX BTW BS 1661 AND BS 1681, LBL 45.50, ACCOMPLISHED REPAIR PER B757-200PF SRM 53-00-52-2R-5 REPAIR 5 REVISION 124.May 6, 2026 · N417UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026061052459Frame · dentedAFT CARGO COMPARTMENT FRAME UPPER FLANGE HAS 2 EA DENT APPROX AT BS 1300, STGR 26L, ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97545-REQ1 AND VT-SAA EA 757-5360-01-B0743 REV IRMay 6, 2026 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2026060952752Angle · crackedRT AFT WTB LOWER PANEL LANDING SUPPORT ANGLE HAS A CRACK AT FASTENER. INSTALLED NEW PART SUPPORT ANGLE ON  RH AFT WTB LOWER PANEL LANDING IAW SRM 51-40-02-0G-0.May 6, 2026 · N417UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR VNAA202606120020Floor Support · crackedCRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE) BELOW WL 79.50. CRACKED ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENTMay 6, 2026 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASAA2026050666650Beam · crackedBEAM BELOW HANDLE BOX ON THE R1 DOOR IS CRACKED IN THE RADIUS NEXT TO MOUNT BOLTS MARKED WITH DOT. GROUNDED - YES. REMOVED AND INSTALLED NEW BEAM ON BELOW HANDLE BOX ON THE R1 DOOR IAW B737-800 SRM 51-40-02-0G-0.May 6, 2026 · N558AS · Boeing 737890 · Service DoorsSDR IPXA2026060551614Bracket · crackedCREW ENTRY DOOR SENSOR BRACKET IS CRACKED. INSTALLED BRACKET IAW SRM 51-40-02.May 6, 2026 · N423UP · Boeing 75724APF · Door Warning SystemSDR IPXA2026050947995Tee Angle · corrodedWING TO BODY T-CHORD AT STA 1037 RBL 0 - 16 IS CORRODED DOT 95305-02. INSTALLED T-CHORD IAW B757-200, SRM 51-40-02-0G-0.May 6, 2026 · N423UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026060539830Bonding Cable · corrodedRH ELEV O/B BONDING HARNESS HAS A CORROSION - ATA 55 - LR-05. REMOVED AND REPLACED RH ELEV O/B BONDING IN REF. B757-200 SWPM 20-20-10. REVIEWEDMay 6, 2026 · N417UP · Boeing 75724APF · Elevator StructureSDR IPXA2026050948140Tee Fitting · damagedWING TO BODY T-CHORD AT PANEL 198KR AT STA 1180 TO 1240 RBL 65 IS CORRODED. INSTALLED NEW T-CHORD AT WING TO BODY T-CHORD AT PANEL 198KR AT STA 1180 TO 1240 RBL 65 IAW B757-200 SRM 51-40-02. REVIEWEDMay 6, 2026 · N423UP · Boeing 75724APF · Aerodynamic FairingsSDR REXA2026060400917Floorbeam · corrodedCORROSION ON CROSSBEAMS ON FS349 BTW LBL9 TO RBL9 AT FLOOR STRUCTURE PASSENGER. CROSSBEAMS ON FS349 BTW LBL9 TO RBL9 AT FLOOR STRUCTURE PASSENGER WAS REPAIRED PER REO 690-53-21-2136 REV.--May 6, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWAA2026060396165Cargo Track · crackedCRACK ON CARGO TRACK LOCATED BS 460 RBL 14 WL 156.1 AT FWD CARGO COMPARTMENT. REPAIRED CARGO TRACK LOCATED BTW STA 400 TO STA 500 + 13 INCHES RBL 13.84 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 AND DWG 143A7500 SHEET 58 REV -.May 6, 2026 · N253WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026060396163Support · corrodedCORROSION ON SUPPORT ZEE LOCATED BTW 480 TO BS 500C LBL 22 AT FWD CARGO COMPARTMENT. REPLACED EXISTING REPAIR OF SUPORT ZEE LOCATED BTW 480 TO BS 500C LBL 22 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7501; SHEET: 112;May 6, 2026 · N253WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026060396164Tie Clip · crackedCRACK ON TIE CLIP LOCATED BS 500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED BS 500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG: 143A1225; SHEET 76; REV-.May 6, 2026 · N253WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR CALA2026060316789Frame · crackedCABIN FRAME STA 312 ABOVE L1 CUTOUT FWD CORNER (S6L) WITH CRACK AT LOWER EDGE. REF. INSTALLED REPAIR AT AT FWD MAIN CABIN FRAME STA 312 ABOVE L1 CUTOUT FWD CORNER S5L - S6L,IAW SRM 53-10-07-2R-1 AND SRM 51-40-02-0G-0,PENDING ESFR AND DIP ENTRY REQUIRED.May 6, 2026 · N73270 · Boeing 737824 · Fuselage Main, FrameSDR SWAA2026060196179Strap · corrodedCORROSION ON STRAP LOCATED BETWEEN STA794.3 TO STA807 AND RBL18 WL156 AT AFT CARGO COMPARTMENT. REPLACED STRAP LOCATED BETWEEN STA794.3 TO STA807 AND RBL18 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 ;SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 14May 6, 2026 · N7875A · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR SWAA2026060196198Light · deterioratedDETERIORATED PHOTOLUMINESCENT STRIP ALONG PASSENGER CABIN. TASK CARD COMPLETED REPLACED PHOTOLUMINESCENT STRIP ALONG PASSENGER CABIN IAW BOEING AMM 33-51-15-400-802-NG.May 6, 2026 · N477WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026060196180Support Bracket · crackedCRACKED SUPPORT BRACKET BS 867, S3R. REPLACED BRACKET SUPPORT LOCATED BS867 AT LEVEL STR 3R AT PASSENGER CABIN IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND DWG 146A7901 SHEET 58 REV-.May 6, 2026 · N7875A · Boeing 7377Q8 · Fuselage Miscellaneous StructureSDR IPXA2026051439477Fairing · debondedFOUND RH WING NO.6 FLAP TRACK FWD FAIRING DISBOND (REPAIR). 1. I.A.W. 747-8F SRM 57-53-70-2R-1 REFER TO SRM 51-70-04-2R-1 AND SRM 51-30-10-0G-0 REV. 48 PERFORM REPAIR AS BELOW STEP : REMOVE THE DISBOND MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA ( DIA : 2",May 6, 2026 · N611UP · Boeing 7478F · Trailing Edge FlapsSDR IPXA2026051439413Skin · cracked- CRACK - SKIN, R/H WING T/E NO.5 FLAP FAIRING (REPAIR). 1. I.A.W. 747-8F SRM 57-53-70-2R-1 REFER TO SRM 51-70-04-2R-1 AND SRM 51-30-10-0G-0 REV. 48 PERFORM REPAIR AS BELOW STEP : REMOVE THE CRACK MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA ( DIA : 1", 32" May 6, 2026 · N611UP · Boeing 7478F · Wing, Plate/SkinSDR IPXA2026051439256Skin · debondedDISBOND - SKIN, AFT SIDE OUTBD FACE OF L/H WING NO.1 FLAP TRACK AFT FAIRING (REPAIR). I.A.W. B747 NDT MANUAL PART 1, 51-01-01 AND PART 4, 51-00-05, REV.182 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6" ALL AROUND. RESULMay 6, 2026 · N611UP · Boeing 7478F · Wing, Plate/SkinSDR SWAA2026052895973Web · corrodedCORRODED SHIELD WEB, BTW BS 767 - 794.3, WL156, RBL22 IN THE AFT CARGO BAY. REPLACED SHIELD WEB IAW SRM-51-10-02, ITEM 9, AND DWG 146A0081, SHEET 43, REV -.May 6, 2026 · N949WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026052896172Support · corrodedCORROSION SUPPORT ZEE BTW BS 727C & 787, WL 156, LBL 21, IN THE AFT CARGO BAY. PERFORMED PERMANENT REPAIR AND REPLACED SUPPORT ZEE IAW SRM SRM 53-00-53-2R-6, AND DWG 143A7500 SHEET 157 REV -.May 6, 2026 · N949WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026052896171Support · corrodedCORRODED SUPPORT ZEE, BS 727 - 767, WL 156, RBL 21, IN THE AFT CARGO BAY. REPLACED THE SUPPORT ZEE AND FASTERNERS IAW SRM 51-40-02, SRM 51-10-02, STEP 9.A AND DWG: 146A7500, SHT 157, REV -.May 6, 2026 · N949WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026052895972Support Angle · crackedCRACKED SUPPORT ANGLE, BS 867, LBL 11 IN THE AFT CARGO BAY.. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, 51-40-02, DWG149A8102, REV A, & DWG 149A8104 REV. B. DUE TO NOT FOUND ALLOWABLE DAMAGE TO ANGLE IN SRM. MEASUREMENT OF CRACK: 1.250 INCHEMay 6, 2026 · N949WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026052895971Fitting · crackedCRACKED FITTING, FLOOR STRUCTURE BS 947, LBL 11, AFT CARGO BAY. REPLACED THE FITTING IAW SRM 51-10-02 ITEM (9) & DWG 149A8103 SHEET 8 REV-. MEASURES OF CRACK IS:0.8310May 6, 2026 · N949WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026052896173Cargo Track · crackedCRACKED TRACK LBL 17.24 BS 747 AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON CARGO TRACK LBL 17.24 BETWEEN BS 727E TO 767 AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-3, REPAIR 3.May 6, 2026 · N949WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026052651388Strap · corrodedMAIN DECK CARGO COMPARTMENT FLOOR BEAM ASSY HAS MULTIPLE NUT PLATE CORRODED AT APPROX BS1681.8, BTW BL 0 AND RBL 50. INSTALLED 5 EA NUTPLATES ASSY AT MAIN DECK CARGO COMPARTMENT FLOOR BEAM STA. 1681.8 BTW BL 0 TO RBL 52" AND APPLIED CIC UPPER SURFACE REWORKEDMay 6, 2026 · N417UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR ASAA2026050666273Web · corrodedAFT CARGO DOOR THRESHOLD HAS CORROSION ON UPPER SURFACE. GROUNDED - YES. REMOVED CORROSION, EVALUATED REMAINIG THICKNESS, ORIGINAL THICKNESS .050, REMOVED .007, REMAING THICKNESS .043 FOUND TO BE OUT OF LIMITS, REMOVED AFT CARGO WEB, LOCATED AND DRILLED NEW WMay 6, 2026 · N537AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR IPXA2026052347942Tee Fitting · corrodedWING TO BODY T-CHORD AT STA 900 RBL 46 TO LBL 27 IS CORRODED AND CHAFED DOT 95305-01. PERFORMED INSTALLATION OF THE T-CHORD 1(EA) AND REPAIR PLATES 8(EA) AT STA 900. PER B757-200 SRM 51-40-02-0G. REVIEWEDMay 6, 2026 · N423UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026052039737Skin Splice · corrodedPOWDERY CORROSION ON RT ELEV OTBD SKIN SPLICE PLATE. INSTALLED SPLICE PLATE AND FILLER ON RT ELEV OTBD SKIN IAW SRM 51-40-02-0G-0.May 6, 2026 · N417UP · Boeing 75724APF · Elevator, Plate/SkinSDR IPXA2026052040562Skin Splice · corrodedPOWDERY CORROSION ON LT ELEV OTBD SKIN SPLICE PLATE. LR-13 VERIFIED STEPS 7 & 8. OK TO INSTALL NEW CONDUCTIVE FRAME GIVEN. INSTALLED NEW FRAME CONDUCTIVE ON L/H ELEVATOR O/B SKIN LOWER SIDE IAW B757-200 DWG 183N2007 AND B757-200 SRM 51-40-02-0G-0. OK TO APMay 6, 2026 · N417UP · Boeing 75724APF · Elevator, Plate/SkinSDR SWAA2026052095780Support · corrodedCORRODED SUPPORT ZEE, BTWN BS 727+10 - 847 LBL 21. REPAIRED SUPPORT ZEE IAW SRM 53-00-53-2R, REPAIR 5.May 6, 2026 · N250WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026051995912Battery Pack · inoperativeEMERGENCY LIGHTS ON LEFT FRONT OVERHEAD BINS INOPERATIVE. REMOVED AND REPLACED LEFT FRONT EMERGENCY BATTERY PACK IAW MM 33-51-06. OPS CHECKS GOOD PER MM 33-51-00.May 6, 2026 · N8538V · Boeing 7378H4 · Emergency LightingSDR SWAA2026051996232Scuff Plate · crackedFSD SCUFF PLATE IS CRACKED. WELDED THE SCUFF PLATE IAW SRM 53-10-15-2R-2 STEP 4.B.(4). INSTALLED FSD SCUFF PLATE IAW AMM 53-11-01-420-801, SRM 53-10-15-2R-2, AND CUSTOMER CARD TTG8Q003P50Z STEP 10.May 6, 2026 · N258WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR DALA2026051903061Not Reported · not reportedDTA ER/A 634191-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL. C/W ER/A 00-634191. (1592353) (AIRCRAFT GROUNDED)May 6, 2026 · N932AT · Boeing 717200 · Standard Practices/StructuresSDR 6HUY202605180001Slide · fodON 6 MAY 2026, ESCAPE SLIDE ASSEMBLY P/N 62292-108 WITH S/N C0975 WAS RECEIVED FOR MAINTENANCE FROM AIR FRANCE UNDER CUSTOMER REPAIR ORDER NO. 6D224308HKR. THE UNIT WAS BOOKED UNDER INTERNAL WORK ORDER WHU2603936. DURING THE INSPECTION AND TESTING PHASE OF THMay 6, 2026 · Airbus A300* · Escape SlideSDR DALA2026051403014Doubler · corrodedER/A 634152-14; A220-300 / REAR BARREL FUSELAGE WASTE BOX INTERNAL DOUBLER & SERVICE DOOR CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 634152-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 FLIGHT HOURS FROM 13,074 TOTAL AIRCRAFT FLMay 6, 2026 · N304DU · Airbus BD5001A11 · Fuselage Main, Plate/SkinSDR UATA2870513265701Stiffener · crackedFOUND A CRACK IN STIFFENER ON THE LH WING FALSE SPAR AT W.S. 4900. THE CRACKED STIFFENER WAS R&R WITH NEW, FABRICATED STIFFENER MADE FROM 2024-T3 ALUMINUM .032" THICK, THE PRE-EXISTING SPACER HAD NO DAMAGE AND WAS REUSED. THE NEW STIFFENER WAS PRIMED WITH SUPEMay 6, 2026 · N439RA · Casa C212200 · Wing Main, Frame StructureSDR IPXA2026051039339Elevator · noneMAJOR REPAIR. EO-85445-JIC1. PERFORMED EO-85445-JIC1. REVIEWED TASK PER GMM-MTX 09.05.01.09.May 6, 2026 · N611UP · Boeing 7478F · Standard Practices/StructuresSDR IPXA2026051039314Elevator · noneMAJOR REPAIR. ADD SDR FOR EO-85445-JIC2. ACCOMPLISHED / PERFORM EO-85445-JIC2. REVIEWED TASK PER GMM-MTX 09.05.01.09.May 6, 2026 · N611UP · Boeing 7478F · Standard Practices/StructuresSDR IPXA2026051147515Angle · corrodedAPU SURROUND ANGLE AT BS 1787 TO 1825 AT S-6R IS CORRODED. DRILLED AND INSTALLED NUT PLATES AT APU ANGLE BS 1787 TO 1825 S-6R IAW SRM 51-40-05 AND SRM 51-40-02-0G.May 6, 2026 · N423UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026051139830Bonding Strap · corrodedAPG - RT ELEVATOR OTBD BONDING HARNESS HAS CORROSION.May 6, 2026 · N417UP · Boeing 75724APF · Elevator StructureSDR JJBA20260508004Terminal Block · meltedWOOD BURNING SMELL IN COCKPIT, NEAR GLARE SHIELD FO SIDE. FOUND RH W/S SENSORS TO SHOW EVIDENCE OF ELECTRICAL DAMAGE SUCH AS MELTING SENSORS, TERMINAL BLOCK MELTING, AND SOLDER DAMAGE TO TERMINALS P AND G. REMOVED FO'S WINDSHIELD AND ALSO WIPER AND REPLACED 4May 6, 2026 · N17146 · Emb EMB145XR · Equipment/Furnishings WiringSDR JIKA2026051201Downlock Switch · warning lightDURING APPROACH, THE LANDING GEAR WAS SELECTED TO THE DOWN AND LOCKED POSITION. THE #1 MAIN LANDING GEAR ASSEMBLY DOWN AND LOCK LIGHT DID NOT ILLUMINATE, AND THE FLIGHT CREW PERFORMED A MANUAL LANDING GEAR EXTENSION. MAINTENANCE TROUBLESHOT THE FAILURE TO A FAMay 6, 2026 · N6724D · Beech C99 · Landing Gear Position and WarningSDR SWAA2026051196783Pad · wornGIRT BAR RUBBER CHAFE PAD IS WORN. REMOVED GIRT; REPLACED CHAFE PAD; REINSTALLED GIRT IAW CMM25-60-37.May 6, 2026 · N8805L · Boeing 7378 · Emergency Equipment