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 FDEA202604240493Skin · dentedLHW OB FLAP EXTERNAL LWR SURFACE FROM OB TO IB 195 INCHES CROSS TE TO LE 5 INCHES FOUND DENTED. REPAIRED LHW OB FLAP EXTERNAL LWR SURFACE DENT AT OTEF STA 333 AS PER B777 SRM 57- 53- 01-2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4G FIGURE 210 REV 51.0Apr 24, 2026 · N874FD · Boeing 777F · Trailing Edge FlapsSDR SCNA20260424166Hydraulic System · overservicedDURING FLIGHT FA ADVISED BURNING ODOR IN CABIN AND FLICKERING LIGHTS OVERHEAD. NO SMOKE. REF FIM 21-00 TASK 806. COULD NOT DUPLICATE SMELL. FOUND HYD B SYSTEM AT 103%. DRAINED HYD B SYSTEM TO 92% REF AMM 29-00-00. NO DEFECTS FOUND TO CABIN LIGHTS. DETERMINED Apr 24, 2026 · N835SY · Boeing 7378KN · Hydraulic System, MainSDR 2026FA0000291Case · unserviceableIBERIA MAINTENANCE HAS RECEIVED A NOTIFICATION FROM AN EXTERNAL REPAIR STATION (FAA DLAY225D LUFTHANSA TECHNIK AG (“LHT”) TO INFORM OF AN OCCURRENCE STATING THAT A NUMBER OF INDIVIDUAL COMPONENTS WERE IDENTIFIED WHERE A FINAL, FULL FLUORESCENT PENETRANT INSPApr 24, 2026 · Engine (Turbine/Turboprop)SDR 1Q2R2026090250020Skin · damagedDURING INSPECTIO, FOUND 3 SPOTS OF LIGHTNING DAMAGE ON SKIN @ STR26R BTWN FS31-FS333Apr 23, 2026 · N593NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR 1Q2R2026090250017Elevator · damagedLEFT ELEVATOR TRAILING EDGE WELDED BY LIGHTNING IN A TOTAL OF (4) SPOTS.Apr 23, 2026 · N593NN · Cndair CL6002D24 · Elevator StructureSDR SWIA2026042377004Skin · dentedRH O/B GROUND SPOILER LOWER SKIN SURFACE HAS MULTIPLE DENTS. IDENTIFIED WITH RED GREASE PENCIL. (C-CHECK RO 08/28/2026)REPAIRED DENTS IN RH OB GROUND SPOILER BY CUTTING OUT DAMAGED SKIN AREA AND FABRICATING AND INSTALLING DOUBLERS, SHIMS AND FILLERS IAW MHIRApr 23, 2026 · N477CA · Cndair CL6002B19 · SpoilersSDR SWIA2026042376865Frame · crackedBS 235, RT UPPER FRAME SECTOR IS CRACKED WHERE IT ATTACHES TO THE RT WINDOW LOWER SILL. REPAIRED THE RT UPPER FRAME SECTOR IAW REO 601R-53-11-4073, REV - AND SKY CARD 51-900-1003-SKY.Apr 23, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2026042376859Frame · crackedBS 235 LT UPPER FRAME SECTOR IS CRACKED WHERE IT ATTACHES TO THE LT WINDOW LOWER SILL. REPAIRED THE LT UPPER FRAME SECTOR CRACK WHERE IT ATTACHED TO THE LH WINDOW LOWER SILL IAW REO 601R-53-11-4072, REV -, & SKY CARD 51-900-1003-SKY.Apr 23, 2026 · N926SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2026042376410Slat Track · damagedLEFT SLAT TRACK 1-2 HAS FRETTING MARKS ON THE TRACK. PERFORMED REPAIR OF LT SLAT TRACK 1-2 PER REO 670-57-42-2496 REV --. OPS CHECKS GOOD COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.Apr 23, 2026 · N770SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026042376389Slat Track · wornRIGHT HAND SLAT TRACK 3-2 HAS WEAR MARKS ON THE LOWER SURFACE AND UPPER INNER SIDE. COMPLIED WITH ALL STEPS OF REO 670-57-42-2502 REV -- FOR REPAIR OF RH SLAT TRACK 3-2 OPS AND RIG CHECK GOOD SEE CONTINUE CARD FOR DETAILS.COMPLIED WITH 51-900-1002-SKY.Apr 23, 2026 · N770SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026042376299Angle · out of limitsREMOVE AND DISCARD OLD ANGLE ASSEMBLY. REPLACE WITH NEW SAME. REPLACED NEW ANGLE AT BS 280 LT IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, DWG CC670-33199, REV B, AND DWG CC670-33052, REV-FApr 23, 2026 · N703SK · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR SWIA2026042376297Doubler · crackedSUSPECTED CRACK ON PAX DOOR AFT PULL IN CAM DOUBLER . REMOVED AND INSTALLED NEW PAX DOOR AFT PULL IN CAM DOUBLER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV N.Apr 23, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWIA2026042376286Intercostal · crackedSUSPECTED CRACK ON PAX DOOR FWD DD7 INTERCOSTAL. DRILLED AND LOCATED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. PRESSURIZED AIRCRAFT IAW AMM 21-31-0Apr 23, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWIA2026042376281Intercostal · crackedSUSPECTED CRACK ON PAX DOOR AFT DD7 INTERCOSTAL. DRILLED AND LOCATED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702, REV N. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURIZED AIRCRAFT IAW AMM 21-31-00-9Apr 23, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWIA2026042376276Intercostal · crackedSUSPECTED CRACK ON PAX DOOR FWD DD1 INTERCOSTAL. DRILLED AND LOCATED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702, REV N. INSTALLED A NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702, REV N. PRESSURIZED AIRCRAFT IAW AMM 21-Apr 23, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWIA2026042376268Doubler · crackedSUSPECTED CRACK ON PAX DOOR FWD PULL IN CAM DOUBLER. REMOVED AND INSTALLED NEW PAX DOOR FWD PULL IN CAM DOUBLER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG 601R31702 REV. N, COMPLIED WITH 51-900-1002-SKY.Apr 23, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew DoorsSDR SWIA2026042376251Intercostal · crackedSUSPECTED CRACK ON PAX DOOR AFT DD1 INTERCOSTAL MX 32130057. DRILLED AND LOCATED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702, REV. N. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702, REV. N. PRESSURIZED AIRCRAFT Apr 23, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew DoorsSDR MTNA2026061500001Probe · false indicationDURING MTNA'S 800 HR INSPECTION ON 758FX IT WAS IDENTIFIED THAT: LEFT FUEL QTY FOUND TO BE INACURATE, WITH EMPTY LEFT SIDE IS 77OLB OF FUEL MX: SYSTEM T/S PERFORMED, DETERMINED #4 PROBE AT FAULT PER C408 MM CHAPT 28-40-00. REPLACED #4 LEFT FUEL QTY PROBE AND Apr 23, 2026 · N758FX · Textrn 408 · Fuel Indicating SystemSDR IPXA2026051748003Fitting · damagedWHILE ACCOMPLISHING EO#7219-REQ001 REV1, HOLE "A", HOLE DIAMETER WAS FOUND OUT OF TOLERANCES, DWG MAPPING ATTACHED WITH DETAILS OF TOLERANCE. RECEIVED AND ACCOMPLISHED THE REPAIR EO-97617-REQ1 WITH EA# 300-5710-27-A4469 REV.-. MAJOR REPAIR.Apr 23, 2026 · N163UP · Airbus A300F4622R · Wing Main, Frame StructureSDR VNAA202606060011Seat Track · crackedCRACK ON SEAT RAIL BTW FS379 TO FS394 RBL 9 AT FLOOR PASSENGER CABIN. EVALUATED, DUE EXCESIVE DAMAGE ON SEAT RAIL BTW FS360 TO FS485 RBL9 AT FLOOR PASSENGER CABIN PER CRJ-900 SRM 53-21-49-101-001-A01 AND REPLACED PER CRJ900 AMM 53-00-49.Apr 23, 2026 · N606NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026060191946Girt Bar · deterioratedDETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR AT FWD GALLEY AREA. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR AT FWD GALLEY AREA IAW AMM 25-66-02-400-801 THE INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8R008B4KB STEP 2.A.(12).Apr 23, 2026 · N8635F · Boeing 7378H4 · Emergency EquipmentSDR REXA2026052800868Fitting · crackedLEFT AFT OVERWING EMERGENCY EXIT DOOR THE UPPER FORWARD ALIGNMENT SPIGOT FITTING STRUCTURE NEAR THE BASE IS CRACKED. REPAIRED LH AFT OVERWING EMERGENCY EXIT IAW MHIRJ REO 690-52-21-228 REV -- DATED 2026-05-25 AND MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-0Apr 23, 2026 · N691CA · Cndair CL6002D24 · Fuselage Main, StructureSDR SWAA2026052792188Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AR LOWER FUSELAGE. REPAIRED ACCESS PANEL 193AR LOWER FUSELAGE IAW B737-800 SRM 51-70-05-2R-10 REPAIR 10.Apr 23, 2026 · N8645A · Boeing 7378H4 · Fuselage Main, Plate/SkinSDR AALA202605219399Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SUPPORT BEAM AT FR 35.2 AND -Y1732. REPLACED FLOOR SUPPORT BEAM PER SRM 51-72-11.Apr 23, 2026 · N105NN · Airbus A321231 · Fuselage Main, Floor BeamSDR ASAA2026042366204Angle · crackedFWD CARGO BS 500H RT BAFFLE ANGLE FWD IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED RT BAFFLE ANGLE FWD IAW SRM 51-40-05-0G-0, & 51-40-02-0G-0.Apr 23, 2026 · N464AS · Boeing 737990ER · Fuselage Miscellaneous StructureSDR ASAA2026042366203Angle · crackedFWD CARGO LT BS 500J BAFFLE CLIP FWD SIDE CRAKED. GROUNDED - YES. REMOVED AND REPLACED LT BS 500 J BAFFLE CLIP IAW BOEING SRM 51-40-05-0G-0, & 51-40-02-0G-0.Apr 23, 2026 · N464AS · Boeing 737990ER · Fuselage Miscellaneous StructureSDR SWAA2026052092184Skin · corrodedCORROSION ON THE INTERNAL SKIN, TOILET SERVICE DOOR 145AL PERFORMED PERMANENT REPAIR LOCATED ON EXTERNAL SKIN TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE IAW SRM 52-40-01-2R-8, REPAIR 8.Apr 23, 2026 · N250WN · Boeing 7377H4 · Fluid Service DoorsSDR SWAA2026052092425Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING . REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.Apr 23, 2026 · N250WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2026051992495Crossbeam · crackedCRACKED PANEL BREAK, BS 540, RBL 2, WL 208. REMOVED AND INSTALLED PANEL BREAK IAW SRM 51-40-02, AND DWG 143A0060, REV-.Apr 23, 2026 · N258WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026051992496Crossbeam · crackedCRACKED CROSSBEAM BS 540, RBL 26, WL 208. REMOVED AND INSTALLED CROSSBEAM IAW SRM 51-40-02 AND DWG 143A0060, REV-.Apr 23, 2026 · N258WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026051992497Attach Angle · crackedCRACKED FLOORBEAM ATTACH ANGLE, BS 693, RBL 2, WL 208. REMOVED AND INSTALLED FLOORBEAM ATTACH ANGLE IAW SRM 51-40-02 AND DWG 273A9111, REV-.Apr 23, 2026 · N258WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR AALA202605188056Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID CABIN FLOOR SEAT TRACK BETWEEN FR 35 AND FR 35-.3 AT-Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.Apr 23, 2026 · N105NN · Airbus A321231 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026051392165Attach Angle · crackedRIGHT VAPOR BARRIER ATTACH ANGLE CRACKED RBL 8 AND RBL 34, BS 663. EVALUATED RT VAPOR BARRIER ATTACH ANGLE, FOUND CRACKED IN TWO PLACES. FOUND TO BE BEYOUND LIMITS IAW SRM 51-10-10-1A-2. REMOVED AND REPLACED RT VAPOR BARRIER UPPER ATTACH ANGLE IAW SRM 51-Apr 23, 2026 · N8537Z · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026051392164Attach Angle · crackedLEFT VAPOR BARRIER ATTACH ANGLE CRACKED LBL 8 AND LBL 34, BS 663. EVALUATED LT VAPOR BARRIER ATTACH ANGLE, FOUND CRACKED IN TWO PLACES. FOUND TO BE BEYOUND LIMITS IAW SRM 51-10-10-1A-2 REMOVED AND REPLACED LT VAPOR BARRIER UPPER ANGLE IAW SRM 51-40-02 AND DWApr 23, 2026 · N8537Z · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026051392224Slide · looseFWD ENTRY DOOR SLIDE IS NOT SECURE IN SLIDE SHROUD. FWD ENTRY SLIDE DOOR SECURED IN SLIDE SHROUD IAW AMM 25-66-01-340-001.Apr 23, 2026 · N474WN · Boeing 7377H4 · Escape SlideSDR ASAA2026042366001Web · corrodedAFT CARGO THRESHOLD CORRODED MARKED IN RED. GROUNDED - YES. BLENDED AWAY CORROSION ORIG. THICKNESS .056, MAT LOSS .036 NEW THICKNESS .020 WEB OUT OF LIMITS PER B737-900 SRM 53-60-15. LOCATED AND DRILLED NEW WEB P#146A8173-25 PER B737-900 SRM 51-40-05. INSTALLEApr 23, 2026 · N275AK · Boeing 737990ER · Fuselage Miscellaneous StructureSDR SWAA2026051192311Attach Angle · crackedRIGHT WING TRAILING EDGE PANEL 651FB FWD ATTACH 'L' ANGLE CRACKED.<[01] REMOVED AND REPLACED RIGHT WING T/E PANEL 651FB FWD ATTACH 'L' ANGLE PER SRM 51-40-02; AND IPC 57-50-00-38.;[02] VERIFIEDApr 23, 2026 · N8534Z · Boeing 7378H4 · Wing, Attach FittingsSDR SWAA2026050792306Intercostal · crackedRIGHT WING INTERCOSTAL WEB JUST INBOARD OF DEFLECTION CONTROL RIB CRACKED. REMOVED INTERCOASTAL WEB PER SRM 51-40-02.;[02] INSTALLED NEW RIGHT WING INTERCOASTAL WEB JUST INBOARD OF DEFLECTION CONTROL RIB PER SRM 51-40-02;[03] QC C/W FOR CA#2. INSTALLED NEW Apr 23, 2026 · N8531Q · Boeing 7378H4 · Wing Miscellaneous StructureSDR AALA202605063282Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 500 & 500I AT LBL 25. REPLACED TRANSITION PANEL PER SRM 53-00-53-2R.Apr 23, 2026 · N956NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202605054967Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO BAFFLE CLIP IS CRACKED UNDER RIGHT HAND TRANSITION PANEL AT STATION 500H. REMOVED AND REPLACED BAFFLE CLIP WITH SERVICEABLE CLIP. PER SRM 51-10-02.Apr 23, 2026 · N954NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202605055255Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR STRUCTURE BRAKE ANGLE AT BS 540 IS CRACKED AT RBL 2. INSTALLED SERVICEABLE BREAK ANGLE. PER SRM 51-40-02 AND AARD 51-00-05-01.Apr 23, 2026 · N954NN · Boeing 737823 · Fuselage Main, StructureSDR AALA202605054882Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD AT STA 986 AND RBL 47. REPAIRED CHORD PER SRM 53-70-51-2R-6 ALTERNATIVE 4.Apr 23, 2026 · N956NN · Boeing 737823 · Fuselage Main, Floor BeamSDR ASAA2026042365804Cargo Track · damagedREF LP 61173376, TRACK SECURING LOCK ASSY. IS DAMAGED AND IS MISSING PIECES SO LOCK ASSY. CANNOT BE SECURED. SECOND TH THE LEFT LOCK ASSY. REMOVED BETWEEN POSITION 1 AND 2. TRACK ASSY. REQUIRES REPAIR OR REPLACEMENT. DAMAGED TRACK IS 1 INCH LONG. GROUNDED - YEApr 23, 2026 · N627AS · Boeing 737790 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202605044117Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING #3ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING 3 ASSY ON RH HORIZONTAL STABILIZER IAW A320 FAM AMM-55-16-42-000-001-A AND IAW A320 FAApr 23, 2026 · N5007E · Airbus A319115 · Elevator StructureSDR 2026F00093Fdu · faultedLEFT ENGINE SHUT DOWN ON ITS OWN AS WE PULLED POWER BACK FOR INITIAL DESCENT FROM FL430. FIRST INDICATION WAS N1 READING ZERO. NEXT INDICATION WAS A GENERATOR FAIL, WARNING LIGHT. OIL PRESSURE WAS NOW AT 9 PSI. NO VIBRATION NOTED. SUCCESSFULLY RESTARTED ENGINEApr 23, 2026 · N525B · Cessna 525B · Engine (Turbine/Turboprop)SDR IPXA2026050139587Restraint · inoperativeFWD CARGO AFT MOST DOOR SILL ROLLOUT LOCK WON`T STAY UP LOCK 59. I.A.W AMM25-54-02-000-801 REV116 AND I.A.W AMM25-54-02-400-801 REV116 REPLACE DOOR SILL ROLLOUT WITH NEW PARTS.Apr 23, 2026 · N581UP · Boeing 7474R7F · Fuselage Main, StructureSDR 2026FA0000313Tire · failedACFT DEPARTED LIML. CREW WAS CONTACTED ABOUT 2 HOURS AFTER DEPARTURE BY ATC INFORMING THEM THEY MIGHT HAVE BLOWN A TIRE ON TAKEOFF. CREW LOOKED AT TIRE PRESSURE IN FLIGHT AND CONFIRMED ALL TIRES STILL HAD GOOD PRESSURE. INTERNATIONAL HANDLER CONTACTED CREW Apr 23, 2026 · N408SB · Gulstm GVIIG600 · TireSDR HYIA20260430004Exhaust Pipe · brokenDURING AN ENGINE CHANGE, THE LEFT EXHAUST PIPE WAS FOUND TO BE CRACKED. THE PIPE WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Apr 23, 2026 · N411CA · Tecnam P2012 · Engine Collector/Tailpipe/NozzleSDR AALA202604308032Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 4 ELEVATOR ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING 4 ASSY ON RH HORIZONTAL STABILIZER IAW AMM-55-16-42-000-001-A AND AMM-55-16-48-000-001-A AND IAW AMM-55-1Apr 23, 2026 · N5007E · Airbus A319115 · Elevator StructureSDR AALA202604304402Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING #6 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING 6 ASSY ON RH HORIZONTAL STABILIZER IAW AMM-55-16-42-000-001-A AND AMM-55-16-42-400-00Apr 23, 2026 · N5007E · Airbus A319115 · Elevator Structure