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 FDEA202602140198Safety Wire · wrong partL1 DOOR SLIDE EJECTOR BAG RELEASE CABLE ATTACHMENT HAS INCORRECT SAFETY WIRE. REQUIRES CAD PLATED COPPER SAFETY WIRE REF FEA 6-2560-F0386375 A P1 STEP 8. FEA: 6-2560-F0386375 A P1 CMM: 25-60-40 RE SAFETIED EJECTOR BAG CABLE ATTACHMENT WITH CAD PLATED COFeb 14, 2026 · N725FD · Airbus A300B4622R · Escape SlideSDR FDEA202602140197Safety Wire · wrong partPACKBOARD RELEASE CABLE SAFETY WIRE REQUIRES REPLACEMENT PER FEA 6-2560-F0386375 A P1 L1 DOOR FEA: 6-2560-F0386375 A P1 CMM: 25-60-40 SAFTIED L1 DOOR SLIDE PACKBOARD RELEASE CABLE WITH .015 STAINLESS WIRE.Feb 14, 2026 · N663FE · Airbus A300F4605R · Escape SlideSDR FDEA202602140196Safety Wire · wrong partWHILE PERFORMING F.E.A. 6-2560-F0386375 A P1 FOUND SAFETY WIRE FOR EJECTOR BAG RELEASE CABLE INCORRECT. R1 DOOR AMM: 25-61-20-05-01 REMOVED AND REPLACED SAFETY WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. OPS CHK GOOD. A/C OK FOR SERVICE. INSPECTED Feb 14, 2026 · N660FE · Airbus A300F4605R · Escape SlideSDR FDEA202602140195Safety Wire · wrong partWHILE PERFORMING F.E.A. 6-2560-F0386375 A P1 FOUND SAFETY WIRE FOR PACKBOARD CABLE WIRE INCORRECT. R1 DOOR - AMM: 25-61-20-05-01 REMOVED AND REPLACED SAFETY WIRE FROM PACKBOARD RELEASE CABLE WITH MS20995C15 STAINLESS STEEL WIRE. INSPECTED BY VENDOR. OPFeb 14, 2026 · N660FE · Airbus A300F4605R · Escape SlideSDR FDEA202602140194Safety Wire · wrong partSAFETY WIRE FOUND ON SLIDE WAS NOT THE CORRECT TYPE ACCORDING TO F.E.A.#:G-2560-F0386282 C PART: 1 (P1) REPLACED BREAKAWAY WIRE WITH CORRECT WIRE SPEC (MS20995CY16) THAT SECURES THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD. MPFeb 14, 2026 · N864FD · Boeing 777FS2 · Escape SlideSDR FDEA202602140193Safety Wire · wrong partRIGHT SLIDE, REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER SMIS 25-60/5696 (F.E.A. G-2560-F0386294 C PART 1) CMM: 25-61-31 EA: 9-2560-T0386431 FEA: Feb 14, 2026 · N857FD · Boeing 777FS2 · Escape SlideSDR DXTA2026021606905Sign · inoperativeEMERGENCY EXIT SIGN LIGHT ON FRONT OF LAV IS INOP CORRECTIVE ACTION: REMOVED OLD LAV EXIT LIGHT AND INSTALLED A NEW EXIT LIGHT. FUNCTION TEST IS GOOD AT THIS TIME. WORK PERFORMED IAW AMM 33-50-02.Feb 14, 2026 · N689QS · Cessna 560XL · Emergency LightingSDR CALA2026021613822Battery Pack · dischargedTHE EMERGENCY LIGHT POWER SUPPLY BATTERY PACK (M33302) FOUND LOW CAPACITY. REPLACED BATTERY PACK AND TEST CARRIED OUT, NORMAL IAW AMM 33-51-06-960-802, REV.106.Feb 14, 2026 · N2639U · Boeing 777300ER · Emergency LightingSDR CALA2026021613820Battery Pack · dischargedTHE AFT EMERGENCY LIGHT POWER SUPPLY BATTERY PACK (M33401) AT THE DOOR 4R FOUND LOW CAPACITY. REPLACED THE AFT EMERGENCY LIGHT POWER SUPPLY BATTERY PACK, TESTED NORMAL IAW AMM 33-51-06-960-802, REV.106.Feb 14, 2026 · N2639U · Boeing 777300ER · Emergency LightingSDR CALA2026021613818Sill Drain · corrodedR4 DOOR LOWER SILL, UNDER DRAIN GUTTER BTWN BS 1640 - 1681, HAS CORROSION. REMOVED CORROSION IN R4 DOOR LOWER SILL, FOUND OUT OF LIMITS IAW SRM 51-10-02-0G, REMOVED SUPPORT AND CLIP IAW SRM 51-40-02-0G, DRILLED NEW PART IAW SRM 51-40 05-00 AND INSTALLED IFeb 14, 2026 · N57869 · Boeing 75733N · Fuselage Main, StructureSDR CALA2026021613816Wire · disconnectedLAV S EPL MONUMENT LIGHT INOPERATIVE FOUND LIGHT DISCONNECTED UNDERNEATH SEAT 4B. RECONNECTED. OPS CHKD GOOD IAW AMM 33-51-11.Feb 14, 2026 · N13113 · Boeing 757224 · Light System WiringSDR CALA2026021613776Battery Pack · inoperativeROW 15 A B C EMERGENCY EXIT LIGHTING BURNT OUT. REPLACED FLOOR PROXIMITY RED LIGH ASSY AND BATTERY PACK OPS NORMAL IAW AMM 33-51-00Feb 14, 2026 · N66803 · Boeing 737924ER · Emergency LightingSDR DALA2026021501048Floor Support · corrodedCORRODED FLOOR SUPPORT -Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AR EA (SSI 534147). REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11 SRM 51-72-11 AND DWG 10N01036. (LP 1451289)Feb 14, 2026 · N377NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2026021401045Power Supply · inoperativeROW 27 EMERGENCY LIGHT INOP. (AISLE UNDERSEAT LIGHT). REPLACED EMERGENCY POWR SUPPLY ABOVE SEAT 29C PER A321 AMM 33-55. CHKS NORMAL. (LP 8449782)Feb 14, 2026 · N534DT · Airbus A321271NX · Emergency LightingSDR DALA2026021401044Power Supply · inoperativeROW 28 EMERGENCY LIGHT INOPERATIVE. (AISLE UNDERSEAT LIGHT). REPLACED EMERGENCY PWR SUPPLY IAW AMM 33-55. (LP 8449783)Feb 14, 2026 · N534DT · Airbus A321271NX · Emergency LightingSDR REXA2026080301407Beam · corrodedSEVERAL CORROSION ON BEAM LBL 9.00 BTW FS477.40 TO FS830.00 WERE FOUND BEAM LBL 9.00 BTW FS477.40 TO FS 830.00 WAS REPAIRED PER REO 670-53-41-833 REV --, REO 670-55-41-835 REV --,REO 670-53-31-1169 REV -- AND EA CRJ753-21644 REV IRFeb 13, 2026 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR A6WA202602138898Floor Support · corrodedCORROSION WAS FOUND ON THE FWD LOWER END OF THE SERVICE DOOR THRESHOLD/FLOOR SUPPORT BRACKET. UPON CLEANING OF THE CORROSION, FASTENER HOLES WERE ELONGATED AND REMOVED MATERIAL WAS BEYOND SRM LIMITS. BLENDED DISCREPANT AREAS OF CORROSION AND DID HFEC OF THE BFeb 13, 2026 · N471ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026021376161Drag Angle · crackedVERTICAL STAB LEFT DRAG ANGLE SHOWS SIGN OF POSSIBLE CRACK. REPAIRED LT VERTICAL STAB DRAG ANGLE IAW SRM 55-31-00-201-001-A01.Feb 13, 2026 · N716SK · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR AALA202604281730Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: REPLACE CONTINUITY FITTING LH SIDE IAW EA 372184. MAINTENANCE REPLACED CONTINUITY FITTING LOCATED Y0 AND FR2 LH SIDE BY EA 372184.Feb 13, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202604249438Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: MAINTENANCE: WINDSHIELD FRAMING CENTER POST FITTING LOWER FITTING FOUND CRACKED AT Y0 AND FR2. MAINTENANCE REPLACE LOWER FITTING YO AND FR2 IAW EA 372184.Feb 13, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR 3EJA202603250001Outflow Valve · failedCABI ALT HIGH CAS/DEPRESSURIZATION AT FL290. R&R OUTFLOW VALVE.Feb 13, 2026 · N301JT · Honda HA420 · Pressure Regulator/Outflow ValveSDR SWAA2026032370679Scuff Plate · crackedCRACKED CENTER SCUFF PLATE. REPAIRED BY WELDING CENTER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, & BAC 5975.Feb 13, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032370682Scuff Plate · crackedCRACKED CENTER SCUFF PLATE. REPAIRED CENTER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1.Feb 13, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032370681Scuff Plate · crackedCRACKED AFT CORNER SCUFF PLATE. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.Feb 13, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032370680Scuff Plate · crackedCRACKED FWD CORNER SCUFF PLATE. REPAIRED FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.Feb 13, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032370683Scuff Plate · crackedCRACKED FWD CORNER SCUFF PLATE. REPAIRED THE FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC5975.Feb 13, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032370675Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 194E OF BODY FAIRING. REPAIRED THE ACCESS PANEL 194E OF THE BODY FAIRING IAW SRM 51-70-05-2R-10 REPAIR 10.Feb 13, 2026 · N245WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2026031370655Stringer · crackedCRACKED STRINGER 25R, BS 540. REPAIRED STRINGER 25R BTWN BS 500C - 540 IAW SRM 53-00-03-2R-1, REPAIR 1.Feb 13, 2026 · N240WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026031370656Stringer · crackedCRACKED STRINGER 26R, BS 540. REPAIRED STRINGER 26R, BTWN BS 500D - 540 IAW SRM 53-00-03-2R-1, REPAIR 1.Feb 13, 2026 · N240WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026031370651Stringer · crackedCRACKED STRINGER 23L, BS 540. REPAIRED STRINGER 23L, BTW BS 500D - 540 IAW SRM 53-00-03-2R-1, REPAIR 1.Feb 13, 2026 · N240WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026031370654Stringer · crackedCRACKED STRINGER 25L, BS 540. REPAIRED THE STRINGER 25L, BTWN BS 500D - 540 IAW SRM 53-00-03-2R-1, REPAIR 1.Feb 13, 2026 · N240WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026031370658Stringer · crackedCRACKED STRINGER 26L, BS 540. REPAIRED STRINGER 26L BTWN BS 500D - 540 IAW SRM 53-00-03-2R-1, REPAIR 1.Feb 13, 2026 · N240WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR 3EJA20260310326Outflow Valve · failedCABI ALT HIGH CAS/DEPRESSURIZATION AT FL290. EXECUTED EMERGENCY PROCEDURES AND DIVERTED TO FXE. /R & R OUTFLOW VALVE.Feb 13, 2026 · N301JT · Honda HA420 · Pressure Regulator/Outflow ValveSDR SWAA2026031270649Handle · brokenBROKEN ASSIST HANDLE DOOR LINING FWD ENTRY DOOR AT FWD GALLEY AREA 2EA. REPLACED ASSIST HANDLE DOOR LINING FWD ENTRY DOOR AT FWD GALLEY AREA 2EA IAW AMM-52-11-31-400-802, STEP 3.G.Feb 13, 2026 · N8629A · Boeing 7378H4 · Passenger/Crew DoorsSDR SWAA2026031170657Light · brokenBROKEN PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (12EA). REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN IAW AMM-33-51-15-400-802.Feb 13, 2026 · N240WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026031170228Bulkhead Web · crackedRIGHT BS 663, RBL 38, WEB CRACKED AT FASTENER HOLE. REMOVED & FABRICATED RT WEB IAW SRM 57-10-10-01-3; SRM 51-40-02. REPLACEMENT WEB IAW SRM 57-10-10-01-3. INSTALLED REPLACEMENT WEB IAW SRM 51-40-02. REF DWG 111A1141 APPROVED THRU BAC SMAL FOR 111A1141-30Feb 13, 2026 · N8525S · Boeing 7378H4 · Fuselage Main, BulkheadSDR SWAA2026030970479Angle · corrodedCORROSION ON PRESSURE DECK WEB STIFFENER ANGLE, BS 685+8. LBL 71, WL 200. REMOVED AND REPLACED THE STIFFENER ANGLE IAW SRM 51-40-02-0.Feb 13, 2026 · N472WN · Boeing 7377H4 · Fuselage Main, KeelSDR SWIA2026030675426Skin · dentedDENT IN OUTER SKIN LOCATED 2"AFT OF FRAME 99 AND 1.125" INBOARD STRINGER 29L. DENT IS 1.010" WIDTH AND 1.043" LENGTH. HEIGHT IS .015". (C-CHECK RO 03/05/2026)PERFORMED PERMANENT DOUBLER AND FILLER REPAIR AT FR 99 STGR 29L - 29R REF ETD2026-170-003204. SEE Feb 13, 2026 · N140SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR WX0A2026030432749Outflow Valve · faulted(AIRCRAFT NOT GROUNDED) (EMERGENCY DECLARED) CAB PRESS EXCESS CAB ALT AT CRUISE. / REMOVED AND REPLACED PRESS CONT 2 (12HL) REF. AMM 21-31-34-000-001 AND REF. AMM 21-31-34-400-001. REMOVED AND REPLACED OUTFLOW VALVE (10HL) REF. AMM 21-31-51-000-001 AND REF. AMFeb 13, 2026 · N331NV · Airbus A319111 · Pressure Regulator/Outflow ValveSDR AALA202602273371Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT RIGHT HAND FLOOR TRANSITION PANEL HAS AREAS OFCORROSION ON UPPER SURFACE BETWEEN BS 500D AND BS 500I AT RBL22. FABRICATED NEW TRANSITION PANEL AND INSTALLED. PER SRM 53-30-53-0I-2 AND SRM 53-00-53-1A.Feb 13, 2026 · N989AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202602274424Tie Down · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR FLOOR MOUNTED FORWARD GIRT BAR TIEDOWN AT BS 312 , LBL 64. REPLACED TIEDOWN PER AARD 51-00-05-1.Feb 13, 2026 · N983AN · Boeing 737823 · Emergency EquipmentSDR AALA202602277110Tie Down · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 DOOR FLOOR MOUNTED AFT GIRT BAR TIEDOWN AT BS 344, LBL 64. REPLACED TIEDOWN PER AARD 51-00-05-1.Feb 13, 2026 · N983AN · Boeing 737823 · Emergency EquipmentSDR SWAA2026022670665Floor Support · corrodedCORROSION ON ACB FLOOR SUPPORT SPLICE, BS 727D+4, WL 157, REPLACED THE FLOOR SUPPORT SPLICE IAW SRM 51-40-02, SRM 51-10-02, SRM 51-40-05, SRM 51-20-01, AMM 51-21-91, & DWG 146A9401, REV C.Feb 13, 2026 · N247WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022670666Floor Support · corrodedCORROSION ON ACB FLOOR SUPPORT SPLICE, BS 767+5, WL 157. REPLACED THE FLOOR SUPPORT SPLICE IAW SRM 51-40-02, SRM 51-10-02, SRM 51-40-05, SRM 51-20-01, & DWG 146A9401, REV C.Feb 13, 2026 · N247WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026022670664Floor Support · corrodedCORROSIN ON ACB FLOOR SUPPORT SPLICE, BS 887, WL 157. REPLACED ACB FLOOR SUPPORT SPLICE IAW SRM 51-40-02, SRM 51-10-02, SRM 51-40-05, SRM 51-20-01, & DWG 146A9401, REV C.Feb 13, 2026 · N247WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR DALA2026022601355Tachometer · failedAUTO BRAKE FAIL ON FINAL WHEN GEAR HANDLE PUT DOWN. AFTER LANDING BRAKE TEMPS: 215 - 245 40 - 530. POST FLIGHT REPORT SHOWS BRAKES AUTO BRK FAULT WITH FAILURE MESSAGE TACHOMETER 3(20GG), BSCU (10GG), BSCU 2, & BSCU 1. FWD TO MCO & PLACARD IAW MEL 32-42-05, Feb 13, 2026 · N370NB · Airbus A319114 · Landing Gear Brake SystemSDR FDEA202602130268Recorder · faultedPASSING 3000 MSL, ALL THREE SCREENS LOST ALL DATA. ONLY THE GRAY LINES REMAINED. TCAS FAIL MESSAGE APPEARED ALONG WITH A COUPLE OF OTHER STATUS MESSAGES. CAPTAIN PRESSED HIS PFD BUTTON AND THE CENTER SCREEN REAPPEARED AND SHOWED THE EICAS SCREENS. CAPTAIFeb 13, 2026 · N296FE · Boeing 7673S2F · Data Recorders (Flight/Maintenance)SDR FDEA202602130267Recorder · failedWHILE IN CRUISE EICAS MONITOR, CPT PFD MONITOR, FO PFD MONITOR AND 8 STATUS MESSAGES APPEARED. COMPLIED WITH QRH, ALL DISPLAYED DATA APPEARED NORMAL. AMM: 34-22-99-4. REMOVED AND REPLACED C GGU REF AMM. OPS CHECK GOOD. A/C OK FOR SERVICE.Feb 13, 2026 · N296FE · Boeing 7673S2F · Data Recorders (Flight/Maintenance)SDR SWAA2026022470563Rib · crackedL/H HORIZONTAL STABILIZER NR 4 RIB, & NR 2 STIFFENER CRACKED. REPAIRED THE RIB & STIFFENER IAW SRM 55-10-09-2R.Feb 13, 2026 · N948WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2026022470564Rib · crackedLEFT HORIZONTAL STABILIZER NR 4 RIB, NR 3 STIFFENER CRACKED. REPAIRED THE RIB, & STIFFENER IAW SRM 55-10-09-2R.Feb 13, 2026 · N948WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib