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 JR2R20260218650Fairing · chafedLEFT WING TIP, ENHANCED FAIRING CHAFED FROM RIVET HEADS. REPAIREDFeb 18, 2026 · N88310 · Emb ERJ170200LL · Wing Main, Frame StructureSDR JR2R20260218603Slat Track · chafedLEFT WING SLAT INBD SLAT TRACK CHAFED. REPAIRED.Feb 18, 2026 · N88310 · Emb ERJ170200LL · Leading Edge DevicesSDR JR2R20260218930Skin · gougedUPON REMOVAL OF FWD FUSLAGE HOT DRAIN, FOUND EXTERNAL SKIN GOUGED AT AFT END. REPAIRFeb 18, 2026 · N88310 · Emb ERJ170200LL · Fuselage Main, Plate/SkinSDR JR2R20260218704Crossbeam · corrodedAFT WET AREA FR 84 CROSSBEAM HAS CORROSION AT APPROX LBL 24. REPAIREDFeb 18, 2026 · N88310 · Emb ERJ170200LL · Fuselage Main, StructureSDR JR2R20260218692Support · corrodedAFT WET AREA ANGLE SUPPORT AT RBL 11, FR 90 - 90A CORRODED. REPLACED.Feb 18, 2026 · N88310 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR JR2R20260218696Gusset · corrodedAFT WET AREA SPLICE GUSSET AT FR 90 BL 0 CORRODED. REPLACEDFeb 18, 2026 · N88310 · Emb ERJ170200LL · Fuselage Main, StructureSDR JR2R20260218695Sill Drain · corrodedAFT WET AREA LT MOP SILL AT LBL 36 FR 88 - 90 CORRODED. REPLACEDFeb 18, 2026 · N88310 · Emb ERJ170200LL · Fuselage Main, StructureSDR JR2R20260218701Sill Drain · corrodedAFT WET AREA RT MOP SILL AT FR 84, RBL 36 CORRODED. REPLACEDFeb 18, 2026 · N88310 · Emb ERJ170200LL · Fuselage Main, StructureSDR JR2R20260218700Floor Support · corrodedAFT WET AREA FLOOR SUPPORT FWD OF FR 87 AT RBL 24 CORRODED. REPLACEDFeb 18, 2026 · N88310 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR 2026FA0000133Pressure Switch · leakingREPEATED FAILURE OF FUEL PRESSURE SWITCH P/N: 9912033-2 CAUSING FUEL TO LEAK FROM THE WEEP HOLE OF THE SWITCH BODY. FUEL THEN LEAKS INTO THE COWLING. FAILURES INCLUDE SWITCH S/N'S: 13646, 13661, 13262 ALL FAILURES HAVE OCCURRED WITHIN A 12-MONTH PERIOD OF 01/2Feb 18, 2026 · N79SG · Cessna 510 · Aircraft Fuel Distribution SystemSDR QR9R2026021800001Rotor Head · out of limitsRECEIVED LAMINATED PILE ASSEMBLY FROM SUPPLY WITH .013'' GAP IN LAMINATED PILE. MAX IS .008''.Feb 18, 2026 · Bolkms BK117C2 · Tail Rotor HeadSDR WX0A1900010032734Epsu · faulted(AIRCRAFT NOT GROUNDED) EPSU 11WL BATTERY FAULT. REMOVED AND INSTALLED NEW EPSU BATTERY IAW A320 AMM 33-51-38-000-002-A / 400-002-A. PERFORMED BITE CHECK IAW AMM 33-51-00-710-001.OP'S CHECK GOOD.Feb 18, 2026 · N286NV · Airbus A320214 · Emergency LightingSDR IPXA2026021866915Warning Message · illuminatedDIVERSION, EMERGENCY DECLARED, RT ENG OVHT AT CRUISE 4512 MSG WENT OUT AFTER 2 MIN AND ENGINE AT IDLE THRUST. ALL ENGINE INDICATIONS WERE NORMAL.Feb 18, 2026 · N455UP · Boeing 75724APF · Overheat DetectionSDR DALA2026021801174Bottle · low pressureDOOR 2R DOOR SLIDE CAUTION ON TAXI IN. CHECK DOOR PRESSURE. SERVICED DOOR ASSIST BOTTLE PER A330 AMM 52-15. (8431247)Feb 18, 2026 · N402DX · Airbus A330941 · Escape SlideSDR DALA2026021801173Frame · corrodedFORWARD SIDE OF FRAME 62 AT P'2 LIGHT TOOLING DAMAGE ON FRAME LOWER EDGE. REPAIRED PER A330 SRM 51-73-00. (1456631)Feb 18, 2026 · N858NW · Airbus A330223 · Fuselage Main, FrameSDR DALA2026021801172Seat Frame · corrodedCABIN SEAT TRACK UPPER SURFACE FOUND CORROSION AT Y450, FR36 TO FR37. REPAIRED SEAT TRACK PER A330 SRM 53-00-15-300-009. (1456158)Feb 18, 2026 · N406DX · Airbus A330941 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026021801171Seat Frame · corrodedCABIN SEAT TRACK UPPER SURFACE FOUND CORROSION AT - Y450, FR74 TO FR75. REPAIRED SEAT TRACK PER A330 SRM 53-00-15-300-009. (1456148)Feb 18, 2026 · N406DX · Airbus A330941 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026021801170Seat Track · corrodedCABIN SEAT TRACK UPPER SURFACE FOUND CORROSION AT Y2462, FR62 TO FR63. REPAIRED SEAT TRACK PER A330 SRM 53-00-15-300-009. (1456136)Feb 18, 2026 · N406DX · Airbus A330941 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026021801169Seat Track · corrodedCABIN SEAT TRACK UPPER SURFACE FOUND CORROSION AT Y1959, FR61 TO FR62. REPAIRED SEAT TRACK PER A330 SRM 53-00-15-300-009. (1456126)Feb 18, 2026 · N406DX · Airbus A330941 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026021801168Seat Track · corrodedCABIN SEAT TRACK UPPER SURFACE FOUND CORROSION AT - Y2462, FR53.1 TO FR53.2. REPAIRED SEAT TRACK PER A330 SRM 53-31-15-300-001. (1456114)Feb 18, 2026 · N406DX · Airbus A330941 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026021801146Frame · damaged(LOG 1456145) LEFT HAND STA 727 FRAME INNER CHORD, 737 REPAIR. ACCOMPLISHED AMDS 5311-01251-02A - LEFT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02. SHIM WAS INSTALLED.Feb 18, 2026 · N377DA · Boeing 737832 · Fuselage Main, FrameSDR DALA2026021801145Frame · damagedACCOMPLISH AMDS 5311-01251-02B - RIGHT HAND STA 727 FRAME INNER CHORD, 737 REPAIR. ACCOMPLISHED AMDS 5311-01251-02B - RIGHT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02. SHIM WAS INSTALLED.Feb 18, 2026 · N377DA · Boeing 737832 · Fuselage Main, FrameSDR FDEA202602180231Battery · inoperativeEMERGENCY LIGHTS DOOR TEST INOP AMM: 33-51-14-04 REMOVED/INSTALLED EMERGENCY POWER SUPPLY UNIT PER AMM REF. ABOVE, OPS CHECK GOOD. A/C OK FOR SERVICE.Feb 18, 2026 · N687FE · Airbus A300F4605R · Emergency LightingSDR FDEA202602180230Safety Wire · wrong partWHILE ACCOMPLISHING EA 6-2560-F386375 REV A PART 1. FOUND THE EJECTOR BAG RELEASE CABLE SAFETY WIRE WAS IN CORRECT. L1 DOOR SLIDE - 3831690 EA: 6-2560-F0386375 REV A PART 1 INSTALLED CAD PLATED SAFETY WIRE TO THE EJECTOR BAG RELEASE CABLE.Feb 18, 2026 · N688FE · Airbus A300F4605R · Escape SlideSDR FDEA202602180229Safety Wire · wrong partWHILE PERFORMING INSPECTION E.A. 6-2560-F0386375 REV A, FOUND EJECTOR BAG RELEASE CABLE SAFTIED WITH WRONG WIRE. AMM: 25-61-20-05-01 INSTALLED CORRECT SAFETY WIRE ON R1 DOOR SLIDE EJECTOR BAG CABLE IAW A300MM 25-61-20-05-01. A/C OK FOR SERVICE.Feb 18, 2026 · N657FE · Airbus A300F4605R · Escape SlideSDR FDEA202602180228Safety Wire · wrong partL1DOOR ESCAPE SLIDE NEEDS TO BE REMOVED TO ACCOMPLISH EA G-2560-F0386282 PART 1 REF WRI 25-60-8181. ESCAPE SLIDE DID NOT HAVE THE CAD PLATED SAFETY WIRE INSTALLED. EA: G-2560-F0386282 C PART 1 AMM: 25-61-21-04 REMOVED AND REINSTALLED L1 DOOR SLIDE AFTER CFeb 18, 2026 · N688FE · Airbus A300F4605R · Escape SlideSDR FDEA202602180227Safety Wire · wrong partL1 DOOR EJECTOR BAG RELEASE CABLE/INFLATOR ACTUATING ARM CLIP HAD IMPROPER BREAKAWAY COPPER WIRE INSTALLED. INSTALLED CORRECT CAD PLATED BREAK AWAY WIRE MS20995CY AS PER CMM AND E.A. LISTED ABOVE FOR THE L1 DOOR SLIDE SERIAL NUMBER 0443TH EJECTOR BAG REFeb 18, 2026 · N680FE · Airbus A300F4605R · Escape SlideSDR IXXA20260218001Bracket · corrodedLEFT LANDING GEAR ELECTICAL CONNECTOR BRACKET CORRODEDFeb 18, 2026 · N752CX · Boeing 7572G5 · Wing Miscellaneous StructureSDR AALA202602184477Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.Feb 18, 2026 · N470AN · Airbus A321253NX · Passenger/Crew DoorsSDR 2026FA0000132Skin · debondedDISBONDS ON THE UPPER WINGS BETWEEN THE OUTBOARD END OF STRINGERS AND THE COMMON SKIN DOUBLERS. THE SKIN AND COMMON DOUBLERS MAY ALSO EXHIBIT A GRADUAL DEVIATION FROM CONTOUR IN THESE REGIONS. THE EXTENT OF THE DEFECT IS LOCATED USING ULTRASONIC INSPECTION ANDFeb 18, 2026 · N569QS · Cessna 680A · Wing, Plate/SkinSDR ABXA20260218069Warning Message · false activationDURING TAXI OUT, AND AFTER ENGINE START, ENG EEC PROBE AND MACH PROBE LIGHT AFTER START STILL ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE T/S IAW ABX FIM 30-34 FAULT TREE 803. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.Feb 18, 2026 · N651GT · Boeing 767231 · Central WarningSDR AALA202602187005Bottle · low pressureAIRCRAFT IN BASE MAINTENANCE: R2 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED R2 DOOR EMERGENCY ASSIST BOTTLE IAW AMM 52-10-00.Feb 18, 2026 · N815AW · Airbus A319132 · Passenger/Crew DoorsSDR AALA202602180991Accumulator · low pressureAIRCRAFT WAS NOT GROUNDED: AFTER L4 DOOR DOOR EMERGENCY CYLINDER/ACCUMULATOR REQUIRES SERVICING. MAINTENANCE SERVICED AFT L4 DOOR EMERGENCY CYLINDER/ACCUMULATOR IAW AMM 52-10-00.Feb 18, 2026 · N680AW · Airbus A320232 · Passenger/Crew DoorsSDR SCNA20260218087Carpet · unsecureAFT GALLEY FLOOR TRIM BETWEEN CARPET AND LINOLEUM IS LIFTING-TRIPPING HAZARD. REMOVED & REPLACED AFT GALLEY TO CARPET THRESHOLD IAW AMM 25-27-21. OK FOR SERVICE.Feb 18, 2026 · N840SY · Boeing 737800* · Passenger Compartment EquipmentSDR JR2R20260218895Shear Tie · crackedWHILE RECONTOURING DENTS IN FUSLAGE SKIN FOUND SHEAR TIE AT FR13 BETWEEN STR4R AND STR5R CRACKED. REPLACED THE SHEAR TIE.Feb 18, 2026 · N88310 · Emb ERJ170200LL · Fuselage Internal Mounting StructureSDR PN1R202602180001Seal · leakingDURING INSPECTION, FOUND #1 ENGINE NO. 5 BEARING SEAL LEAKING.Feb 18, 2026 · N614CJ · Agusta AW139 · Turbine Engine Oil SystemSDR CALA2026021813862Lamp · inoperativeDOOR 2R EXTERIOR EMERGENCY LIGHT INOP. RELAMPED DOOR 2R EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-06, OPS CHECKED GOOD.Feb 18, 2026 · N14120 · Boeing 757224 · Emergency LightingSDR SWIA2026021776587Window Frame · crackedPILOTS SIDE WINDSHIELD SIDE POST LOWER OUT BOARD CLIP CRACKED. REMOVED CRACKED CLIP AND INSTALLED NEW OUTBOARD CLIP AT PILOTS SIDE WINDSHIELD LOWER POST IAW SRM 51-42-21-001-001-A01, AND DWG CC670-33055 REV -F. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKYFeb 17, 2026 · N813SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2026070676520Beam · chafedRIGHT ENGINE LOWER C DUCT, THE INBD INNER BEAM ARE CHAFED, WHERE IT MEETS THE FIRE SEAL. BLENDED CHAFE ON RT ENGINE LOWER C DUCT INBD INNER BEAM IAW SRM 51-12-00-001-001-A01L 16. NO DAMAGE ALLOWED IN THIS AREA. REPAIRED PER REO 690-54-22-122 REV--. SEE CONTFeb 17, 2026 · N813SK · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR SWIA2026021776126Hinge Fitting · gougedPAX DOOR HINGE ON THE FUSELAGE SIDE 11TH, 13TH, 14TH LUGS FROM FWD SIDE OF HINGE ARE GOUGED. REPLACED PAX DOOR HINGE ON THE FUSELAGE SIDE IAW SRM 53-21-23 AND REO 601R-53-21-656 REV--DATED 2024-03-15. COMPLETED TASK CARD 51-900-1003-SKY .Feb 17, 2026 · N457SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2026021776123Pan · corrodedSERVICE DOOR LOWER PAN IS CORRODED. INSTALLED NEW SERVICEABLE SERVICE DOOR PAN P/N:601R38437-2 IAW CRJ 200 SRM 51-42-06, 51-42-13, 51-42-21, 51-40-11 AND 51-42-22. COMPLETED TASK CARD 51-900-1003-SKY.Feb 17, 2026 · N457SW · Cndair CL6002B19 · Service DoorsSDR SWIA2026021776120Hinge · gougedPAX DOOR HINGE ON THE DOOR SIDE 11TH, 12TH, 13TH, 16TH LUG LANDINGS FROM FWD SIDE OF HINGE ARE GOUGED. REMOVED UNSERVICEABLE PAX DOOR HINGE ON THE DOOR SIDE AND REPLACED WITH A SERVICEABLE HINGE IAW SRM 52-10-31. CFeb 17, 2026 · N457SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2026021775988Stringer · corrodedSTRINGER 25L IS CORRODED BETWEEN FS 485.00 TO 501.00 (C-CHECK RO 05/03/2026)REMOVED AND REPLACED STGR 25L BETWEEN FS 485 AND 501 WITH A NEW SERVICEABLE STGR25L P/N SH670-33254-3 IAW CRJ700 SRM 51-42-06-001-001-A01.Feb 17, 2026 · N795SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026021775986Stringer · corrodedSTRINGER 23L IS CORRODED BETWEEN FS 485.00 AND 533. REMOVED AND REPLACED WITH NEW SERVICEABLE STGR 23L IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01Feb 17, 2026 · N795SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026021775920Door · chafedAFT CARGO DOOR CHAFED AND GOUGED IN MULTIPLE LOCATIONS AROUND OUTER HANDLE HOUSING. REMOVED AND INSTALLED NEW AFT CARGO DOOR HANDLE ASSY IAW SRM 51-42-21-001-001-A01 AND DWG CC670-38702 REV. -F. LEAK CHECK AND OPS TESTED GOOD. COMPLIED WITH TASK CARD 51-900-1Feb 17, 2026 · N732SK · Cndair CL6002C10 · Cargo/Baggage DoorsSDR ASAA2026021765614Frame · corrodedFWD PIT AFT BULKHEAD SUPPORT FRAME AT STA 500I BOTTOM MIDDLE HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACE FWD PIT AFT BULKHEAD SUPOPRT FRAME AT STA 5001 BOTTOM MIDDLE IAW B737-800 SRM 51-40-02-OG-OW: 1 O: .063 R: .040 L: 1/2 D: .023.Feb 17, 2026 · N546AS · Boeing 737890 · Fuselage Main, FrameSDR ASAA2026021765613Frame · corrodedFWD PIT AFT BULKHEAD SUPPORT FRAME L/H SIDE LOWER AT STA 500I HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FWD PIT AFT BULKHEAD SUPPORT FRAME L/H SIDE LOWER AT STA 5001 IAW B737-800 SRM 51-70-02-OG-OW: 1 O: .063 R: .046 L: 3 D: .017.Feb 17, 2026 · N546AS · Boeing 737890 · Fuselage Main, FrameSDR SWIA2026021775719Pressure Deck · corrodedLEFT PRESSURE FLOOR SKIN IS CORRODED AT (1EA) LOCATION AT F.S. 529.00. REPAIRED LH PRESSURE FLOOR SKIN AT FS529.00 IAW REO 601R-53-41-666 REV-C DATED 2012-11-06 06 COMPLETED TASK CARD 51-900-1003-SKY .Feb 17, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026021775717Pressure Deck · corrodedRIGHT PRESSURE FLOOR SKIN IS CORRODED AT (2EA) NUTPLATE LOCATIONS BETWEEN F.S. 499.00 AND F.S .513.00. (C-CHECK RO 04/16/2026)REPAIRED R/H PERESSURE FLOOR SKIN AT 2EA NUTPLATE LOCATIONS BETWEEN FS499.00 AND FS513.00 IAW REO 601R-53-41-666 REV-C DATED 2012-11Feb 17, 2026 · N915EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026021775708Floor Skin · gougedRIGHT PRESSURE FLOOR SKIN IS GOUGED AT (1EA) NUTPLATE LOCATION BETWEEN F.S. 424.00 AND F.S. 439.00. REPAIRED RH FLOOR SKIN GOUGE AT 1EA NUTPLATE LOACTION BETWEEN FS424.00 AND FS439.00 IAW REO 601R-53-41-3409 REV-- . COMPLETED TASK CARD 51-900-1003-SKY.Feb 17, 2026 · N915EV · Cndair CL6002B19 · Fuselage Floor Panel