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 HNAA2026102901067Floor Support · corrodedLEFT OMEGA BEAM UPPER GUSSET AT FR 56 HAS CORROSION. REMOVED AND REPLACED LT OMEGA BEAM UPPER GUSSET AT FR 56 IAW SRM 51-40-02-PR.Sep 8, 2026 · N681AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026102901066Floor Support · corrodedLH FLOOR SILL FROM FR 54 TO FR 55 HAS CORROSION. REMOVED AND REPLACED WITH NEW LH FLOOR SILL FROM FR 54 TO FR 55 IAW EMB 145 SRM 51-40-02-PRSep 8, 2026 · N681AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026102901065Gusset · corrodedRIGHT FLOOR GUSSET AT FR 59 HAS CORROSION. REMOVED AND REPLACED RH FLOOR GUSSET AT FR 59 IAW EMB 145 SRM 51-40-02-PR.Sep 8, 2026 · N681AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026102901064Floor Support · corrodedRIGHT OMEGA BEAM DOUBLER AT FR 20 CORRODED AT NUTPLATE HOLE. REMOVED AND REPLACED WITH NEW R/H OMEGA BEAM DOUBLER IAW SRM 51-40-02-PR. RESTORED SURFACE PROTECTION TO THE AREA IAW CPM 51-21-06.Sep 8, 2026 · N681AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026102901063Door Frame · corrodedSERVICE DOOR CUT-OUT LWR STRUCTURE FROM FR 20 - FR 22 CORRODED AT NUTPLATE HOLE. PERFORMED DOUBLER REPAIR ON SERVICE DOOR CUT-OUT LWR STRUCTURE AT FR 20 NUT PLATE HOLE IAW EMB 145 SRM 53-21-02-RE ITEM 3 FIG 202.Sep 8, 2026 · N681AE · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026102901062Floor Support · corrodedLEFT FLOOR SILL FR 23 - FR 29 CORRODED AT NUTPLATE HOLES. REMOVED AND REPLACE LT FLOOR SILL FROM FR 23 - FR 29 IAW SRM 51-40-02-PR.Sep 8, 2026 · N681AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026102901061Floorbeam · corrodedLEFT CROSS FLOOR SUPPORT AT FR 18 CORRODED ON AFT SIDE. REMOVED AND REPLACED CNTR CROSS FLOOR SUPPORT AT FR 18 PER EMB 145 SRM 51-40-02-PRSep 8, 2026 · N681AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR HNAA2026102901060Floorbeam · corroded00274 CNTR CROSS FLOORBEAM AT FR 20 CORRODED. REMOVED AND REPLACED CNTR CROSS FLOORBEAM AT FR 20 PER EMB 145 SRM 51-40-02-PRSep 8, 2026 · N681AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR HNAA2026102901059Skin · delaminatedRIGHT ENGINE THRUST REVERSER INBD SKIN HAS MULTIPLE AREAS OF UNDERLYING DELAMINATION AND CORROSION. COMPLIED WITH PERMANENT REPAIR OF THE RT THRUST REVERSER EXHAUST INBD BEAM SKIN IAW ETD2026-145-015931 REV.: A AND EO1-05-26-0438.Sep 8, 2026 · N681AE · Emb EMB145LR · Engine Thrust ReverserSDR HNAA2026102901058Skin · delaminatedLEFT ENGINE THRUST REVERSER INBD SKIN HAS MULTIPLE AREAS OF UNDERLYING DELAMINATION AND CORROSION. COMPLIED WITH PERMANENT REPAIR OF THE LT THRUST REVERSER EXHAUST INBD BEAM SKIN IAW TD2026-145-015863, REV A AND EO1-05-26-0438.Sep 8, 2026 · N681AE · Emb EMB145LR · Engine Thrust ReverserSDR HNAA2026102901049Floorbeam · corrodedFLOOR SUPPORT ANGLE AT FR 18 CORRODED AT IB EDGE AROUND THE NUTPLATE HOLE. REMOVED CORROSION FROM FLOOR SUPPORT ANGLE AT FR 18 PER EMB 145 SRM 51-10-03 STEP 5.A. TYPE A, AND RESTORED SURFACE PROTECTION PER EMB 145 CPM 51-21-04, AND 51-21-05, 51-21-06Sep 8, 2026 · N681AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR IPXA2026102435766Bracket · crackedRT WW L BRACKET IS CRACKED NEAR WW SEAL. INSTALLED 1EA NEW BRACKET PIN RT WW AREA SRM 51-40-02-0G-0.Sep 8, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102435745Support Channel · crackedRIGHT WW GUSSET SUPPORT STRUCTURE L BRACKET WAS CRACKED. INSTALLED GUSSET SUPPORT STRUCTURE L BRACKET ASSY. (SUPPORT CHANNEL) AND SEAL RETAINER ASSY. ON RH W/W IAW SRM 51-40-02-0G-0 AND 51-40-04-0G-0.Sep 8, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102341715Hook · corrodedMAIN DECK CARGO DOOR AFT LOWER HOOK HAS PITTING MARKS, LOST MATERIAL. INSTALLED NEW AFT LOWER HOOK AT MAIN DECK CARGO DOOR IN REF TO CMM 52-32-03 AND AMM 20-11-00-912-001.Sep 8, 2026 · N402UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA2026102041943Support · corrodedFWD CARGO FR 38.2, BETWEEN Y805 AND -Y805 CEILING/LINNING SUPPORT HAS (5EA) SPOTS OF CORROSION. INSPECTED REMOVED CORROSION FROM CEILING SUPPORT AT FR 38.2, BETWEEN Y805 AND -Y805 IAW A300 SRM 51-74-10. FOUND TO BE NEGLIGIBLE DAMAGE IAW SRM 53-15-18.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100240081Support · corrodedFAULT-STR-Z100, AFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 54.2 WITH SPOTS OF CORROSION FROM CROSSBEAM Y450 TO -Y450 DOT 31-029. INSTALLATION CEILING SUPPORT IAW A300-600 SRM 51-40-21. REVIEWEDSep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026101940236Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR57 WITH SPOTS OF CORROSION FROM CROSSBEAM -Y450 TO -Y953. REMOVAL OF CORROSION FROM CEILING SUPPORT PANEL FR57, -Y450 TO -Y95 FOUND TO BE NEGLIGIBLE DAMANGE WITHIN LIMITS IAW SRM 51-73-11.3. IAW A300 SRM 51-74-10.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026101940166Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT BETWEEN FR56/FR57 WITH SPOTS OF CORROSION FROM CROSSBEAM -Y450 TO -Y963. REMOVED CORROSION FROM CEILING AT SUPPORT PANEL FR56/FR57 -Y450 TO -Y953. IAW A300 SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063.MATERIAL LOSS ISep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026102135715Bracket · crackedRIGHT WW GUSSET IS CRACKED. INSTALLED GUSSET SUPPORT (BRACKET) ON RT WW IAW SRM 51-40-02-0G-0.Sep 8, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026102136117Gusset · crackedLH WW HAS A CRACKED GUSSET. INSTALLED NEW GUSSET AT LH WW PER B757-200PF SRM 51-40-02-0G-0.Sep 8, 2026 · N402UP · Boeing 75724APF · Wing Miscellaneous StructureSDR SWAA2026102160442Panel · crackedCRACK FOUND ON THE RT FWD CUTOUT PANEL 142KW, BS 792. IN THE CARGO BAY. REPLACED FWD CUTOUT PANEL IAW SRM 51-10-02 ITEM 9 AND DWG 146A9403, SHT 99, REV-.Sep 8, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102178761Cover · missingMISSING COVER ON EMERGENCY EXIT HATCH ESCAPE STRAP. LEFT DOOR. INSTALLED THE COVER IAW SOPM 20-50-12, REV 58.Sep 8, 2026 · N8658A · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026102178002Battery Pack · inoperativeEMERGENCY BATTERY PACK, POWER SUPPLY M1694 INOPERATIVE. REPLACED THE BATTERY PACK. TESTED OK IAW AMM 33-51-06-960-805.Sep 8, 2026 · N8658A · Boeing 7378H4 · Emergency LightingSDR IPXA2026102042390Crossbeam · corrodedFWD CARGO FR 34, BETWEEN -Y140 AND -Y805 CEILING SUPPORT HAS CORROSION. INSPECTED REMOVED CORROSION FROM CEILING SUPPORT AT FR 34, BETWEEN -Y140 AND -Y805. IAW SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063 MATERIAL LOSS IS .003 REMAING MATERIAL IR .060.FOSep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026101940470Crossbeam · corrodedAFT CARGO COMPARTMENT, CEALING SUPPORT (Z PROFILE) AT FR57.3 AT CROSSBEAM -Y1959 HAS A SCREW HOLES WITH CORROSION. REMOVED CORROSION FROM CEILING SUPPORT (Z PROFILE) AT FR57.3 AT CROSSBEAM -Y1959. IAW SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063.MATERIAL Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR REXA2026102001958Seat Track · corrodedCORROSION ON RT & LT SEAT TRACKS BTWN BS 693 - 977 IN THE PAX CABIN. THE SIDE SEAT TRACKS WERE REPLACED IAW AMM 53-00-49, & AMM 20-21-00.Sep 8, 2026 · N479PX · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026102001955Seat Track · corrodedCORRODED SEAT TRACKS BTWN BS 379 - 485, LBL 9 & BTWN BS 677 - 847+16, RBL 9. THE SEAT TRACKS WERE REPLACED IAW AMM 53-00-49.Sep 8, 2026 · N479PX · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026101935723Gusset · crackedRT WW GUSSET SUPPORT STRUCTURE IS CRACKED. INSTALLED GUSSET SUPPORT (BRACKET) ON RH W/W I.A.W B757-200 S.R.M 51-40-02-0G-0.Sep 8, 2026 · N402UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2026101941134Crossbeam · corrodedAFT CARGO COMPARTMENT, ANGLE SUPPORT OF SMOKE DETECTOR BOX AT FR62 CROSSBEAM Y0 WITH CORROSION. REMOVED CORROSION FROM CEILING AT SUPPORT PANEL FR62, IAW A300 SRM 51-74-10. ORIGINAL MATERIAL THICKNESS IS .063- MATERIAL LOSS IS .001 REMAINING MATERIAL IS .062 TSep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR SWAA2026101954042Floor Support · corrodedCORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE AT BS 987 RBL 42, BS 947 RBL 52, BS 987 LBL 42 WL 208 CORRODED.Sep 8, 2026 · N8657B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR IPXA2026101835885Retainer · crackedRIGHT WW AFT SEAL RETAINER HAS A GOUGE. INSTALLED NEW SEAL RETAINER AFT OF RH WW IAW SRM 51-40-02-0G-0.Sep 8, 2026 · N402UP · Boeing 75724APF · Landing Gear DoorsSDR IPXA2026101840963Crossbeam · crackedAFT CARGO COMPARTMENT FWD BULKHEAD AT FR54 CROSSBEAM Y0 ANGLE SUPORT WITH CRACKED INSTALLED NEW ANGLE SUPPORT, AFT CARGO COMPARTMENT FWD BULKHEAD AT FR54 Y0, IAW SRM 51-40-21.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026101841001Support Angle · crackedAFT CARGO COMPARTMENT FWD BULKHEAD AT FR54 CROSSBEAM Y963 ANGLE SUPORT WITH CRACK. INSTALLED NEW ANGLE SUPPORT, AFT CARGO COMPARTMENT FWD BULKHEAD AT FR54 Y953, IAW SRM 51-40-21. REVIEWEDSep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026101840973Support Angle · crackedAFT CARGO COMPARTMENT FWD BULKHEAD AT FR54 CROSSBEAM Y1963 ANGLE SUPORT WITH CRACK. INSTALLED NEW ANGLE SUPPORT AT Z100, AFT CARGO COMPARTMENT FWD BULKHEAD AT FR54 Y1959, IAW SRM 51-40-21.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR SWAA2026101639375Access Panel · crackedCRACK ACCESS PANEL 844DZ OF GALLEY DOOR AT AFT GALLEY AREA. REPLACED THE ACCESS PANEL 844DZ IAW AMM 12-25-13-640-802, STEP 3.G.(1)(C).Sep 8, 2026 · N8656B · Boeing 7378H4 · Galley DoorsSDR HNAA2026101600997Floor Support · cracked53-2117 CTR OMEGA BEAM OB ANGLE CRACKED AT BTW FR46-50. RAR ANGLE IAW SRM 53-23-02Sep 8, 2026 · N650AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026101600995Floor Support · cracked5-2114 CTR OMEGA BEAM, IB ANGLE CRACKED BTW FR46-50. RAR ANGLE IAW SRM 53-23-02Sep 8, 2026 · N650AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASAA2026090869247Cargo Track · crackedAFT CARGO RBL 14 CARGO TRACK CRACKED AT BS 727H - 727G. GROUNDED - YES. AFT CARGO RBL 14 CARGO TRACK CRACKED AT BS 727H - 727G.Sep 8, 2026 · N564AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2026090869246Channel · corrodedAFT CARGO LT TRANSITION CORRODED FROM BS 727 - 847. GROUNDED - YES. REMOVED DAMAGE FROM BS 727 - 847, FOUND TO BE OUT OF LIMITS, REPAIRED IAW SRM 53-00-53-2R-5.Sep 8, 2026 · N564AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026090869245Doubler · corrodedAFT CARGO RH FRAME BS 787 DOUBLER CORRODED. GROUNDED - YES. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS, REMVOED AND REPLACE DOUBLER IAW SRM 51-40-02-0G-0Sep 8, 2026 · N564AS · Boeing 737890 · Fuselage Main, FrameSDR ASAA2026090869244Transition Panel · corrodedAFT CARGO RH TRANSITION FROM STA 727 TO 767 CORRODED. GROUNDED - YES. REMOVED DAMAGE ON RH SIDEPLATE TRANSITION PANEL, FOUND TO BE OUT OF LIMITS, REPAIRED SIDEPLATE TRANSITION FROM STA 727-767 IAW B737-800 SRM 53-00-53-2R-5 W: 1" O: .040 R: .020 L: 2" D: .020.Sep 8, 2026 · N564AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026090869243Support Bracket · corrodedAFT CARGO RH SUPPORT BRACKET AT STA 767 FWD SID OF FWD SHIELD CORRODED. GROUNDED - YES. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02-0G-0.Sep 8, 2026 · N564AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026090869242Baffle · corrodedAFT CARGO RH BAFFLE BETWEEN STA 767 TO 787. GROUNDED - YES. REMOVED DAMAGE, FAOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED BAFFLE AIW SRM 51-40-02-0G-0.Sep 8, 2026 · N564AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026090869241Shield · corrodedAFT CARGO FWD SHIELD CORRODED. GROUNDED - YES. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SHIELD IAW SRM 51-40-02-0G-0.Sep 8, 2026 · N564AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR SWAA2026101493744Web · crackedCRACKED WEB, BS 847 - 867, LBL 28. REPLACED THE WEB & FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 149A8100, SHEET 1, REV-.Sep 8, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101453587Angle · crackedCRACKED GUSSET ANGLE, BS 500I STR 19R. REPLACED THE GUSSET ANGLE IAW SRM 51-40-02-0G, AND DWG 143A7902, SHEET 256, REV BSep 8, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101413677Angle · crackedCRACKED ANGLE, BS 500H, STR 26R. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 143A7505, SHEET 151, REV-.Sep 8, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101406078Angle · crackedCRACKED ANGLE, BS 500H, STR 26R. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 143A7505, SHEET 151, REV-.Sep 8, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101468248Angle · crackedCRACKED BLADE ACCESS PANEL 343AT ANGLE, RT HORIZONTAL STAB. REPLACED BLADE ON ACCESS PANEL ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, AND SRM 51-40-02.Sep 8, 2026 · N8656B · Boeing 7378H4 · Horizontal Stabilizer StructureSDR SWAA2026101405555Access Panel · damagedELONGATED HOLES ACCESS PANEL 644BB AT RT WING (2 EA). REPAIRED THE ACCESS PANEL 644BB IAW SRM 51-70-04-2R-9, REPAIR 9.Sep 8, 2026 · N8656B · Boeing 7378H4 · Wing, Plate/Skin