Service difficulty reports

1,770,704 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 FDEA202609111315Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1486, X= 47.5" FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM Sep 11, 2026 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202609111314Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1321, X= -27.5" FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-Sep 11, 2026 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202609111313Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1199, X= 8.5" FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00Sep 11, 2026 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202609111312Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= 27.5" FOUND CROWN WORN. THE SEAT TRACK BS 6-10, X= 27.5" WAS EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT Sep 11, 2026 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202609111311Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 47.5" FOUND THE CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTISep 11, 2026 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202609111310Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= 8.5", FOUND CROWN WORN. THE SEAT TRACK BS 6-10, X= 8.5", EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISSep 11, 2026 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202609111309Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= -8.5" FOUND CROWN WORN. THE SEAT TRACK BS 6-10, X= -8.5", EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT ESep 11, 2026 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202609111308Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= -27.5" FOUND CROWN WORN. THE SEAT TRACK BS 6-10, X= -27.5" EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMESep 11, 2026 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202609111307Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= -47.5" FOUND CROWN WORN. THE SEAT TRACK BS 6-10, X= -47.5" EVALUATED & FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT Sep 11, 2026 · N625FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR QEMY20260911002Disk · indication THE CONDITION IDENTIFIED HAS BEEN EVALUATED AND A RECOMMENDATION TO RETURN TO SERVICE CANNOT BE PROVIDED. TO BE REPORTED I.A.W AMC-20 8A (J) ANY DEFECT IN A LIFE-CONTROLLED CRITICAL PART THAT CAUSES ITS RETIREMENT BEFORE THE COMPLETION OF ITS FULL-SERVICE LSep 11, 2026 · N446L · Boeing 777 · Turbine SectionSDR QEMY20260911001Seal · crackedTHE SUBJECT SEAL-ROTATING CDP HPT DISPLAYS CRACKING TO ALL SEAL TEETH 360’. THE CONDITION IDENTIFIED HAS BEEN EVALUATED AND A RECOMMENDATION TO RETURN TO SERVICE CANNOT BE PROVIDED. FMD HAS BEEN SUBMITTED. TO BE REPORTED I.A.W AMC-20 8A (J) ANY DEFECT IN A LIFSep 11, 2026 · N446L · Boeing 777 · Turbine Engine Compressor SectionSDR IPXA2026110476328Support Fitting · crackedRH HORIZONTAL STAB. FRONT SPAR ABOVE I/B L/E PANEL 341AB UNDER APRON PANEL 343AT STRUCTURE HAS A BROKEN MOUNT BRACKET/DOT.130.034 REJECTED. INCOMPLETE CORRECTIVE ACTION. 2. SUBTASK INCOMPLETE.Sep 10, 2026 · N146UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026102688064Strap · corrodedAFT CARGO CEILING STABILIZATION STRAP RH OTBD SIDE BS 1420 HAS CORROSION ON UPPER SURFACE. INSTALLED NEW REPLACEMENT STABILIZATION STRAP IN AFT CARGO CEILING BS 1360-1450 IAW SRM 51-70-11-0G-0 FIG 1 DETAIL II STEP 10.Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102776662Bracket · corrodedWIRE HARNESS CLAMP SUPPORT BRACKETS ATTACHED TO BS 1885 BULKHEAD HAVE LITE CORROSION AND MISSING PROTECTIVE FINISH. INSTALLED 1EA BRACKET TO STA 1885 BL 0 BULKHEAD, RESTORED 1EA WIRE CLAMP TO BRACKET AT STA 1885 BL 0 REF SRM 51-40-02-0G-0.Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR HNAA2026102901072Housing · corrodedPANEL 191JR HAS UNDERLYING CORROSION ON THE OUTER RING OF THE LIGHT HOUSING. REMOVED AND REPLACED PANEL 191JR OUTER RING OF THE LIGHT HOUSING (SPACE PLATE) P/N 145-40346-001 PER EMB 145 AMM 33-50-10.Sep 10, 2026 · N681AE · Emb EMB145LR · Emergency LightingSDR HNAA2026102901071Floor Support · corrodedCORROSION ON RT OMEGA BEAM HOLE AT FR 60. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER TO RT OMEGA BEAM AT FR 60 PER ETD-2026-145-015572 REV A AND EO EO1-53-26-0460Sep 10, 2026 · N681AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026102901051Rib · crackedLEFT WING OTBD RIB 21 HAD A CRACK ON UPPER FLANGE, PERFORMED CUT-OUT AND DOUBLER REPAIR OF LT WING OTBD RIB ON UPPER FLANGE IAW IAW SRM 57-20-07-RE, STEP 4.Sep 10, 2026 · N681AE · Emb EMB145LR · Wing, Rib/BulkheadSDR HNAA2026102901050Floor Support · crackedDURING POST REMOVAL INSPECTION FOR THE 1EA RH FLOOR GUSSET AT FR 59, FOUND A CRACK ON RT OMEGA BEAM FWD HOLE AT FR 59. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER TO RT OMEGA BEAM AT FR 59 PER ETD 2026-145-015572 REV A AND EO 1-53-26-0460Sep 10, 2026 · N681AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR IPXA2026102586680Door · gougedSTR, APU COMPARTMENT ACCESS DOOR 316 AR EDGE MEMBER HAS MULTIPLE GOUGE AND EVIDENCE OF CRACK AT BOTTOM SURFACE APPROX BTW STA 1885 AND STA 1963, INSTALLED 2EA REPAIR DOUBLERS, 2EA REPAIR FILLERS AND 2EA ALIGNMENT PIN HOLE PLATES ON APU COMPARTMENT ACCESS DOOSep 10, 2026 · N402UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR IPXA2026102376207Bulkhead · dentedAPU COMPARTMENT STA 1885 BULKHEAD REPAIR DOUBLE 10" INCHES RIGHT OF LIGHT SWITCH DENTED IN AND EDGES ROLLED UP. RL019. FABRICATED -1 REPAIR DOUBLER AND -2 REPAIR FILLER, DRILLED THE FASTENER HOLES, DEBURRED AND SMOOTHEN ALL HOLES AND SHARP EDGES ON WEB AND THESep 10, 2026 · N402UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA2026102388112Strap · crackedAFT CARGO CEILING STABILIZATION STRAP LH SIDE BS 1340 LBL 24 IS CRACKED. INSTALLED NEW REPLACEMENT STABILIZATION STRAP AND SPLICE PLATE IAW SRM 51-70-11-0G-0 FIG 1 DETAIL 2 AND 51-40-02-0G-0 PAR4.Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102188082Strap · corrodedAFT CARGO CEILING STABILIZATION STRAP 2ND FROM RH OTBD SIDE STA 1400-1420-1420 HAS CORROSION ON UPPER SURFACE. INSTALLED REPLACEMENT STABILIZATION STRAP BETWEEN STA. 1440 TO 1390 AND REINSTALLED STABILIZATION STRAP BETWEEN STA. 1390 TO 1360 AND INSTALLED REPASep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR SWAA2026102141175Angle · crackedCRACKED ANGLE, BS 500I, STRINGER 21L, IN THE FWD CARGO BAY. REPLACED WITH A NEW ANGLE IAW SRM 51-40-02-0G, SRM 51-10-02-0G, & DWG 143A7902, SHT 256, REV B.Sep 10, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102180419Support Angle · crackedCRACKED SUPPORT ANGLE, BS 500H, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 143A7505, SHT 152, REV -.Sep 10, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102102907Support Angle · crackedCRACKED SUPPORT ANGLE, BS 500H, STR 26R IN THE FWD CARGO BAY. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A7505, SHT 152, REV -.Sep 10, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102120424Gusset · crackedCRACKED GUSSET ANGLE, BS 500I, STRINGER 19R IN THE FWD CARGO BAY. REPLACED WITH A NEW GUSSET ANGLE IAW SRM 51-40-02-0G, SRM 51-10-02-0G, AND DWG 143A7902, SHEET 256, REV B.Sep 10, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102121247Support · corrodedCORROSION SUPPORT ZEE BTWN BS 500E - 500I, STR 26R IN THE FWD CARGO BAY. REMOVED CORROSION ON THE SUPPORT ZEE AND EVALUATED REWORKED AREA, & FOUND WITHIN LIMITS IAW SRM 53-00-53-1A-2, ALLOWABLE DAMAGE 2.Sep 10, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102133742Support Angle · crackedCRACKED SUPPORT ANGLE, BS 695, RBL 1, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, & DWG 273A9110, SHT 8, REV-.Sep 10, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102173856Support Angle · crackedCRACKED SUPPORT ANGLE, BS 400, STRINGER 26L. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DWG 143A7505, SHT 151, REV- .Sep 10, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR IPXA2026101986516Pad · chafedNR 2 PYLON AFT FAIRING I/B ACCESS DOOR 445AL AFT LATCH AND PAD HAS DEEP CHAFE WEAR. 83-009. INSTALLED NEW PLATE (STOP PAD) ON #2 PYLON AFT FAIRING I/B ACCESS DOOR 445AL I.A.W B757-200PF SRM 51-40-02-0G-0 PAR. 4 AND PAR. 9.Sep 10, 2026 · N402UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR ASAA2026091069377Floorbeam · corrodedFORWARD LAVATORY INBD AFT MOUNT CORRODED STRUCTURE FS 300. GROUNDED - YES. REMOVED DAMAGE ON FWD WET AREA LAV MOUNT INTERCOSTAL, FOUND TO BE OUT OF LIMITS, REMOVE AND REPLACED LAV MOUNT INTERCOSTAL STA 291.5 - 312 LBL 11.5 IAW B737-800 SRM 51-40-02-0G-0 STEP 7Sep 10, 2026 · N564AS · Boeing 737890 · Fuselage, Equipment Attach FittingsSDR HNAA2026102001023Support · crackedBAGGAGE DOOR MECHANISM SUPPORT CRACKED BTW FR 67-68 AT STR 4R. RAR SUPPORT IAW SRM 51-40-02Sep 10, 2026 · N650AE · Emb EMB145LR · Cargo/Baggage DoorsSDR SWAA2026101929413Attach Angle · crackedCRACK FOUND ON THE INTERCOSTAL ATTACH ANGLE AT BS 380+13, LBL 11, WL 208. R & R THE ATTACH ANGLE IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, & DWG 143A5400, REV-.Sep 10, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026101964468Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT BS 380+10, LBL 52, WL 208. R & R THE ATTACH ANGLE IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, AND DWG 143A5400, REV-.Sep 10, 2026 · N8657B · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026101973041Floor Support · crackedCRACK FOUND ON FLOOR SUPPORT AT BS 380+13, RBL 11, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT BTWN BS 380 - 400, RBL 11, WL 208 IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, AND DWG 143A5400 REV-.Sep 10, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101929534Floor Support · crackedCRACK FOUND ON INTERCOSTAL ATTACH ANGLE, BS 380+11, RBL 41, WL 208. REMOVED & REPLACED THE INTERCOSTAL BS380-400 RBL 41 WL 208 IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, AND DWG 143A5400, REV -.Sep 10, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR IPXA2026101876234Stiffener · wornAPU COMPARTMENT BULKHEAD STA 1885 HORZ STIFFENER JUST BELOW LIGHT SWITCH ASSY DOOR SAFETY CATCH EDGE WORN. INSTALLED NEW RETAINER AT APU COMPARTMENT BULKHEAD STA 1885 HORZ STIFFENER I.A.W B757-200PF SRM 51-40-02-0G-0.Sep 10, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR SWAA2026101616604Support Angle · corrodedCORRODED SUPPORT ANGLE, BS 500I BTWN LBL 22 - RBL 22. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DWG 143A7902, SHT 257, REV B, & DWG 143A9481, SHT 17, REV-.Sep 10, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101678997Support · corrodedCORRODED SUPPORT ZEE, LOCATED BTWN BS 500B - 500I, STR 25L IN THE FWD CARGO BAY. REPLACED SUPPORT ZEE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 153, REV-.Sep 10, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101655295Support · corrodedCORRODED SUPPORT ZEE BTWN BS 500A - 500I, STR 25R. REPLACED THE SUPPORT ZEE IAW SRM 51-40-02, DWG 143A7500, SHEET 10, REV-, & DWG1437505 SHEET 153, REV-.Sep 10, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR HNAA2026101601004Support · cracked53-2263 BAGGAGE DOOR ROD SUPPORT CRACKED AT FR68. RAR SUPPORT IAW SRM 51-40-02Sep 10, 2026 · N650AE · Emb EMB145LR · Cargo/Baggage DoorsSDR HNAA2026101601003Support · crackedBAGGAGE DOOR MECHANISM SUPPORT CRACKED BTW FR67-68 AT STR5R. RAR SUPPORT IAW SRM 51-40-02Sep 10, 2026 · N650AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026101601002Firewall · crackedAPU FIREWALL CRACKED AT RH EDGE BTW STR11-12R. REPAIRED IAW ETD 2026-145-015767Sep 10, 2026 · N650AE · Emb EMB145LR · APU Cowling/ContainmentSDR HNAA2026101601001Support · crackedBAGGAGE DOOR SUPPORT MECHANISM CRACKED AT BTW FR67-68 AT STR5R. RAR SUPPORT IAW SRM 51-40-02Sep 10, 2026 · N650AE · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026101601000Firewall · cracked53-2245 APU FIREWALL CRACKED AT RH EXTINGUISHER NOZZLE. REPAIRED IAW ETD 2026-145-015767 REV C AND EO 1-53-26-0481Sep 10, 2026 · N650AE · Emb EMB145LR · APU Cowling/ContainmentSDR HNAA2026101500981Support · crackedCARGO DOOR SUPPORT MECHANISM SUPPORT CRACKED AT BTW FR61-62. RAR SUPPORT IAW SRM 51-40-02Sep 10, 2026 · N650AE · Emb EMB145LR · Fuselage Main, StructureSDR SWAA2026101453533Floor Panel · delaminatedDELAMINATED UPPER SURFACE ON FLOOR PANEL 241EF AT PASSENGER CABIN. REPAIRED THE FLOOR PANEL 241EF IAW SRM 53-00-50-2R-7, REPAIR 7.Sep 10, 2026 · N8656B · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026101306104Angle · corrodedFWD ENTRY DOOR THRESHOLD MOST INBOARD ATTACH FASTENER HOLES ON Z ANGLE HAVE CORROSION AROUND THEM(PHOTO) FWD ENTRY DOOR THRESHOLD MOST INBOARD ATTACH FASTENER HOLES ON Z ANGLE HAVE CORROSION AROUND THEM(PHOTO) REMOVED DAMAGE PER SRM 51-10-02. MATERIAL REMOVED Sep 10, 2026 · N8711Q · Boeing 7378 · Fuselage Miscellaneous StructureSDR HNAA2026101300978Angle · bent53-2255 CARGO DOOR ENTRY, AFT T-PROFILE AND ANGLE BENT AT FR67. R & R T-PROFILE AND ANGLE IAW SRM 51-40-02Sep 10, 2026 · N650AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026101300977Angle · corrodedCARGO DOOR ENTRY, FWD TEE PROFILE AND ANGLE CORRODED AT FR66. R & R TEE PROFILE AND ANGLE IAW SRM 51-40-02.Sep 10, 2026 · N650AE · Emb EMB145LR · Fuselage Miscellaneous Structure