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 ABXA20260410156Warning Message · illuminatedDURING TAXI, CTR R FUEL PUMP EICAS MESSAGE ILLUMINATED AFTER PUSHBACK. T/S IAW FIM 28-22 FT 805. FOUND UFI INDICATION. RESET UFI IAW SUP AMM 28-23-00. OPS CHECK GOOD. ACFT REMAINS NO ETOPS. ACFT RETURNED TO SERVICE.SDR 2026F00070Angle · crackedREPAIRED CRACKED CLIP INSIDE EQUIPMENT BAY ON RH SIDE OF CANTED BULKHEAD PER AQRD ERO-988018, REV. IR, TITLED "N317QS- TAILCONE CANTED BULKHEAD RH CLIP CRACKS", DATED APR 06, 2026. F&DT EVALUATION DUE DATE: MAR 31, 2027. NOTE 1: THE FATIGUE AND DAMAGE TOLERANCSDR 2026F00069Spar · corrodedFOUND 2 AREAS OF CORROSION ON VERTICAL STAB AFT SPAR LH CLIP. MECHANICALLY REMOVED CORROSION VERTICAL STAB LEFT AFT SPAR IN 2 AREAS. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 680 SRM 51-70-02. REPAIRED LEVEL 2 CORROSION ON VERTICAL STAB AFT SPAR LHSDR QR9R2026041000001Valve · malfunctioned#2 ENG OIL PRESSURE CAUTION DISPLAYED WHILE ON GROUND AT FLY (1.3 FOR APPROXIMATELY 10 SECS). DURING T/F MOC, #2 ENGINE OIL PRESSURE NEVER WENT ABOVE 1.4 BAR WHILE IN THE FLIGHT POSITION AND WITH INCREASED COLLECTIVE INPUT. WHEN ENGINE WAS REDUCED TO IDLE, PRESDR IXXA20260410001Strap · crackedWHILE PREFORMING INSP AT STA. 1725.5 OF BULKHEAD OUTER CHORD STRAP FOUND CRACK AT STRINGER 6R INTERNAL FWD OF APU INTAKE DOORSDR SWIA2026040977419Skin · corrodedCORROSION FOUND ON INNER FUSELAGE SKIN BETWEEN BS 280 & 295, STR 24R -25R. PERFORMED A CUT OUT OF THE CORRODED FUSELAGE SKIN BTWN BS 280 - 310, STR 24R - 26R AND APPLIED DOUBLER IAW REO 670-53-21-2866, REV -.SDR SWIA2026040976354Fitting · gougedLEFT WING REAR SPAR AT WS162.49 HAS A FITTING GOUGED & DAMAGED. REMOVED, REPLACED, AND INSTALLED FITTING ON LT WING REAR SPAR AT WS 162.49 IAW SRM 57-51-14,51-40-11,51-21-11,51-25-06,51-25-16,51-42-06, & 51-42-20,51-23-00.SDR SWIA2026040976344Bulkhead Web · crackedUPON REMOVAL FWD FLOORBEAM ANGLE AT BS 280 BETWEEN RBL 9 AND LBL 9, FOUND CRACKED. REPAIRED BULKHEAD WEB IAW REO 601R-53-11-926, REV -B, & REO 601R-53-21-3811, REV -, COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR VNAA202606120060Axle · corrodedLEFT RUSTED AND MISSING TOPCOAT ON ROOT RADIUS INBD AND OTBD SECTIONS PISTON, PISTON AXLE LT MLG. ROOT RADIUS INBD AND OTBD SECTIONS PISTON, PISTON AXLE LT MLG. WERE REPAIRED AND ATTENDED PER REO 670-32-11-361 REV. A.SDR VNAA202606120059Axle · corrodedEXPOSED MATERIAL ON ROOT SETTLEMENT AREA AT RH MLG PISTON AXLE. EXPOSED MATERIAL ON ROOT SETTLEMENT AREA AT RH MLG PISTON AXLE WAS ATTENDED PER REO 670-32-11-361 REV A.SDR SWIA2026040976208Floorbeam · tornRH CABIN SILL @ FS589.00 HAS TORN NUTPLATE HOLE FOR FLOORBOARD. REPAIRED TORN NUTPLATE HOLE IN RH CABIN SILL AT FS589.00 IN REFERENCE TO REO 601R-53-61-8519 REV-- 2026-04-22. PERFORMED EDDY CURRENT INSPECTION IN REFERENCE TO NDTM PART 1 51-20-06 AND PART 6 5SDR IPXA2026052625637Floor Panel · damagedMAJOR REPAIR. THS COMPARTMENT FR83-84 LH FWD FLOOR PANEL DISBONDED. VERIFIED REMOVAL OF ACCESS PANEL FROM THS COMPT. FR83 - FR84 LH IAW A300-600 SRM 51-40-21-001SDR IPXA2026051825110Bracket · damagedVERTICAL STABILIZER RH FWD LOWER FAIRING SUPPORT BRACKET NR 4 HAS ELONGATED HOLE. SUPPORT BRACKET ON VERTICAL STABILIZER RH FWD LOWER FAIRING WAS REMOVED IAW SRM 51-40-21-001. INSTALLED NEW BRACKET ON VERTICAL STABILIZER RH FWD LOWER FAIRING IAW SRM 51-40-21SDR HNAA2026052000429Yoke · crackedRIGHT ENGINE YOKE LOWER FWD FITTING HAS A POSSIBLE CRACK. REMOVED AND REPLACED CRACKED RT ENGINE YOKE LOWER FWD FITTING IAW PDT FCD1-54-21-0017 REV D.SDR IPXA2026051025803Support Angle · corrodedLEFT UPPER APRON AFT ANGLE SUPPORT CORRODED. REMOVED LH UPPER APRON AFT ANGLE SUPPORT I.A.W A300-600 SRM 51-40-21. INSTALLED NEW (ANGLE SUPPORT) I.A.W SRM 51-40-21.SDR IPXA2026040919324Floor Panel · brokenMCD FLOOR PANEL 231MJ IS BROKEN. FLOOR PANEL 231MJ FABRICATION IS COMPLETE IAW SREO-16407-REQ001.SDR IPXA2026041025522Strap · corrodedEMPENAGE THROUGHT ACCESS PANEL 311AL STRUCTURE THAT ATTACH APU INLET DOOR HAVE CORROSION 07-005 INSTALLED APU AIR INTAKE DOOR IAW B757 AMM 49-15-05-404-016. AND INTAKE DOOR HOUSING IAW B757 AMM 49-15-08-404-008.SDR SCNA20260508188Angle · crackedCRACK ON ANGLE OF VAPOR BARRIER STA 663 AND RBL 2 AT MLG WHELL WELL. - - ANGLE OF VAPOR BARRIER STA 663 AND RBL 2 AT MLG WHELL WELL WAS REPLACED PER B737-800 SRM 51-40-02-0G-0.SDR IPXA2026042920047Floor Panel · damagedMAJOR REPAIR. FLOOR PANEL 231RG IS DAMAGED FLOOR PANEL 231RG FABRICATION IS COMPLETE IAW SREO-16407-REQ001.SDR REXA2026050700516Plate · bentWEAR AND BENT IN LOWER PLATE AND SEAL RETAINER OF FWD/CTR BAGGAGE-BAY CARGO DOOR LOWER PLATE (2 EA) ON FWD/CTR BAGGAGE-BAY CARGO DOOR WERE REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01SDR SWAA2026050687867Mount · corrodedNR 2 ENGINE AFT MOUNT HAS EVIDENCE OF FRETTING ON THE OUTBOARD LINK AT TRF ATTACHMENT. REMOVED NR 2 ENGINE AFT MOUNT IAW AMM 71-21-03. INSTALLED NR 2 ENGINE AFT MOUNT IAW AMM 71-21-03. INSTALLED INBD AND OB THRUST LINKS ONTO NR 2 ENGINE AFT MOUNT IAW AMM 71SDR SWAA2026050687935Web · crackedNR 2 ENGINE OB FAN COWL OIL SERVICE DOOR REINFORCEMENT WEB IS CRACKED. FAN COWL REPLACED ON ANOTHER FAULT. REF TTG8Q00S5H2J FOR REPLACEMENT DETAILS.SDR SWAA2026050687861Pin · corroded315A (APU COWL DOOR) CENTER LATCH ALIGNMENT PIN IS RUSTED. CLEANED DIRT ACCUMULATION FROM STOP PIN PER SOPM 20-30-03.SDR SWIA2026040976000Skin · gougedFUSELAGE SKIN HAS 2EA GOUGES UNDER AFT WING TO BODY FAIRING APPROX BS 985 - 988, BL27. REPAIRED FUSELAGE SKIN 2EA GOUGES UNDER AFT WING TO BODY FAIRING APPROX BS 977 - 988, STR 27 IAW REO 670-53-00-290, REV -F. SRM 51-42-21-001-001-A01 REVISON 38 AND SRM 51-SDR SWAA2026050587998Attach Angle · crackedLEFT WING TRAILING EDGE ATTACH ANGLE FOR OTBD END OF TRANSVERSE WEB CRACKED. REMOVED AND REPLACED LEFT WING TRAILING EDGE ATTACH ANGLE FOR OTBD END OF TRANSVERSE WEB IAW SRM 51-40-02-0G-0.SDR IPXA2026050121290Beam · damagedFWD CARGO DOOR LOWER FRAME BEAM, FWD EDGE BEAM HAS PUNCTURE. INSTALLED NEW FRAME BEAM AND PANEL SUPPORT LIGHT DOOR ON FWD CARGO DOOR IAW SRM 51-40-02-0G-0.SDR HNAA2026050500374Bulkhead Web · crackedMULTIPLE CRACKS IN THE RH AFT WHEEL WELL WEBS. REMOVED AND REPLACED WITH NEW RH AFT WHEEL WELL WEB IAW EMB 145 SRM 51-40-02-PRSDR IPXA2026050107936Attach Angle · corrodedLEFT ELEVATOR OB BONDING JUMPER ATTACHMENT HAS CORROSION. REMOVED INTERCOSTAL TO GAIN ACCESS AT LH STABILIZER HORIZONTAL TIP AREA REF SRM 51-40-02-0G-0. INSTALLED INTERCOSTAL, NEW BONDING JUMPER AND FABRICATED ANGLE AT LH OB HORIZONTAL STABILIZER TIP AREA, IASDR ASAA2026040965745Shield · corrodedMULTIPLE SPOTS OF CORROSION ON THE SHIELD ON THE RIGHT HAND SIDE OF THE AFT CARGO PIT BETWEEN STATIONS 767 AND 787,18 INCHES FROM THE BUTT LINE. GROUNDED - YES. REMOVED CORROSION FROM THE AFT PIT, FWD SHIELD FROM STA 767 TO 787 IAW B737-800 SRM 53-60-15-1A-1.2SDR IPXA2026042711816Cover · crackedFAULT - R/H WING L/E VARIABLE CAMBER FLAP #17 INBD ROTARY ACTUATOR HAS CRACKED OTBD COVER. NO.5385. I.A.W AMM 27-81-07-004-001 REV 116 REMOVE NO.17 V.C FLAP INBD'S OUTBD ROTARY ACTUATOR. I.A.W AMM 27-81-07-404-008 REV.116 STEP 3.F.(2).(P) TO STEP 3.G.(2) ACCSDR IPXA2026042711853Cover · crackedFAULT - R/H WING L/E VARIABLE CAMBER FLAP #17 OTBD ROTARY ACTUATOR HAS CRACKED OTBD COVER. NO.5311. I.A.W AMM 27-81-07-004-001 REV 116 REMOVE NO.17 V.C FLAP ROTARY ACTUATOR. I.A.W AMM 27-81-07-404-008 REV.116 STEP 3.F.(2).(P) TO STEP 3.G.(2) ACCOMPLISHED THE ISDR IPXA2026042711764Cover · crackedLT WING L/E VARIABLE CAMBER FLAP NR 2 ROTARY ACTUATOR AT HAS CRACKED COVER. IAW AMM 27-81-07-004-001 REV 116 REMOVE NR 2 V.C FLAP ROTARY ACTUATOR. IAW AMM 27-81-07-404-008, REV.116, STEP 3.F.(2).(P) TO STEP 3.G.(2). ACCOMPLISHED THE INSTALLATION AND ADJUST SDR IPXA2026042713748Cover · crackedRIGHT WING L/E VARIABLE CAMBER FLAP 24 ROTARY ACTUATOR AT HAS CRACKED COVER. IAW AMM 27-81-07-004-001, REV 116. REMOVE 24 V.C FLAP ROTARY ACTUATOR. IAW AMM 27-81-07-404-008, REV 116. STEP 3.F.(2).(P) TO STEP 3.G.(2). ACCOMPLISHED THE INSTALLATION AND ASDR IPXA2026042711916Cover · crackedLEFT WING LE VARIABLE CAMBER FLAP NR 5, ROTARY ACTUATOR AT HAS CRACKED COVER. 5386. IAW AMM 27-81-07-004-001, REV 116. REMOVED NR 5 VC FLAP ROTARY ACTUATOR. I.A.W AMM 27-81-07-404-008 REV.116 STEP 3.F.(2). P TO STEP 3.G. (2). ACCOMPLISHED THE INSTALLATION ANSDR R61A2026042600113Doubler · corrodedWHILE IN HEAVY CHECK - LT COCKPIT FLOOR DOUBLER HAS MULTIPLE AREAS OF CORROSION AND MISSING SURFACE PROTECTION. PERFORMED REPAIR SPLICE OF LT COCKPIT FLOOR DOUBLER IAW SRM 53-10-10 R07SDR R61A2026042600112Doubler · corrodedWHILE DURING HEAVY CHECK - RT COCKPIT FLOOR DOUBLER HAS CORROSION AND SURFACE PROTECTION MISSING IN MULTIPLE AREAS. PERFORMED REPAIR SPLICE OF RT COCKPIT FLOOR DOUBLER IAW SRM 53-10-10 R07.SDR R61A2026042600110Crossbeam · corrodedWHILE DURING HEAVY CHECK - CROSSBEAM 11 HAS MULTIPLE AREAS OF CORROSION AS MARKED. REPAIRED CROSSBEAM 11 IAW ETD2026-170-006564.SDR IPXA2026042411547Cover · crackedCRACK- COVER, NO.4 ENG R/H T/R ACTUATOR ACCESS PNL 446B, 446C, 445C. I.A.W.AMM 78-31-10-004-001-J00 REV116 REMOVED THE PANEL 446B 446C 445C. I.A.W.AMM 78-31-10-404-008-J00 REV116 INSTALLED THE PANEL 446B 446C 445C WITH NEW.SDR IPXA2026042411487Cover · crackedCRACK- COVER, NO.3 ENG R/H T/R ACTUATOR ACCESS PNL 436B, 436C. I.A.W.AMM 78-31-10-004-001-J00 REV116 REMOVED THE PANEL 436B 436C. I.A.W.AMM 78-31-10-404-008-J00 REV116 INSTALLED THE PANEL 436B 436C WITH NEW.SDR IPXA2026042014756Rub Strip · chafedCHAFED RUB STRIP, NR 3 ENG RT CORE COWL AFT UPR RUB STRIP. I.A.W SRM 51-40-02-0G REV. 106 AND CMM IPL 71-13-24 REV.50 INSTALLED NEW STRIP.SDR IPXA2026042114858Seal · brokenBROKEN - SEAL, NR 4 ENG RT T/R CLOSURE DOOR FWD AREA. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE SEAL. I.A.W SRM 51-40-02-0G REV. 106 AND ST ENGINEERING IPC 78-32-22 REV. 96 INSTALLED NEW SEAL.SDR IPXA2026042014715Rub Strip · chafedCHAFING AND MISSING - STRIP AND RIVET, NO.3 ENG L/H CORE COWL AFT UPR WEAR STRIP. IAW SRM 51-40-02-0G REV. 106 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-23 REV.47 INSTALLED NEW STRIP.SDR IPXA2026042315124Nose Cowl · dentedDENTED SKIN, NR 2 ENG NOSE COWL INNER BARREL NEAR 2:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.4", 5.5" FROM AFT EDGE, 59.5" FROM LWR EDGE, AT 2 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CUREDSDR IPXA2026041323730Tee Angle · corrodedRH WING TO BODY T-CHORD AT BS 1040 HAS CORROSION AROUND NUTPLATE HOLES. BLENDED AREA AROUND THE NUTPLATES HOLES TO REMOVE THE CORROSION PER SRM 51-10-02-0G-0 AND AFTER PERFORMED EVALUATION T-CHORD AT STA 1040 WAS FOUND TO BE WHITIN ALLOWABLE LIMITS. PER SRM 5SDR IPXA2026042214799Seal Depressor · crackedCRACKED DEPRESSURE SEAL, AFT CARGO DOOR CUTOUT AFT SIDE. I.A.W SRM 51-40-02-0G REV.106 REMOVE DAMAGE DRPRESSOR SEAL AND DEPRESSOR. I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO.65B01865 SH10 REV E AND BOEING DWG NO.65B06880 SH2 REV B INSTALL NEW DRPRESSOR SDR IPXA2026041815210Fairing · dentedDENTED SKIN, LT WING T/E FLAP NR 4 AFT FAIRING EXTERNAL SURFACE LOWER SIDE ADJACENT AFT CONE. IAW SRM 57-53-70-2R-1 REFER TO SRM 51-70-17-0G-0 REV. 106 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE DAMAGE MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CSDR REXA2026042200297Handle · stuckPASSENGER DOOR INNER HANDLE GETTING STUCK MOVING UP TRYING TO OPEN DOOR. COULD NOT OPEN DOOR FROM INSIDE OR FROM THE OUTSIDE. RAMPERS TRIED. HANDLE WAS STUCK BETWEEN BEING FULLY DOWN AND FULLY UP. FELT LIKE LIKE ANY MORE PRESSURE WOULD BREAK OFF HANDLE, IN EISDR IPXA2026042127320Actuator · faultedUPON LANDING RECEIVED A RIGHT REVERSER YELLOW CAS UPON EXITING THE RUNWAY TOWER INFORMED HAD SMOKE OUT OF THE RIGHT ENG. COMPLETED QRH EVACUATION CHECKLIST AND EVACUATED THE AIRPLANE ON TAXI WAY. REMOVED AND REPLACED RT ENGINE OTBD THRUST REVERSER UPPER ACTUSDR MASA20260420095Doubler · corrodedDURING HEAVY CHECK, INSPECTIONS OF THE INTERANAL FWD FUSE, FLOOR SUPPORT STRUCTURE, DOUBLER AT FR 16, LBL 11, CORROSION AT ANCHOR NUT HOLE BLENDED IAW SRM 51-10-03, MAX MATRL REMOVED .002. WITH IN LIMITS IAW SRM 53-10-10, ALLOWABLE LIMITS, FIG 101, SHT 4 10X MSDR MASA20260420092Floorbeam · corrodedDURING HEAVY CHECK, INSPECTIONS OF THE INTERANAL FUSELAGE STRUCTURE AT CFIII, CORROSION FOUND ON ANGLE SUPPORT, FR 90, RBL 12. REPLACED IAW ERJ 175 SRM 51-41-02, SRM 51-41-01, REV# 45, MAY-28-2021.