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 VNAA20260508014Rib · damagedRIGHT WING I/B FLAP L/E RIB (P/N CC670-14102-2) HAS 1EA ELONGATED NUTPLATE HOLE ON THE O/B SIDE. REPAIRED IAW REO 670-57-52-644 REV-A DATED 2026-02-16Feb 18, 2026 · N512AE · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2026021875877Cleat · corrodedPASSENGER DOOR FS338.963 FRAME AND INTERCOSTAL DD6 CLEAT INBD SIDE CORRODE. PAX DOOR FS338.963. FRAME AND INTERCOSTAL DD6 CLEAT. ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00. CORROSION EXIST ON 2 ELEMENT, OUT OF LIMITS, REPLACE CLEAT IAW SRM 52-0Feb 18, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026021875876Former · corrodedPASSENGER DOOR FS338.963 FORMER CORRODE. INSTALLED NEW PASSENGER DOOR FS338.963 FORMER. IAW. SRM 51-42-06-00 AND SRM 51-42-21-00. AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKYFeb 18, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026021875869Cleat · corrodedPASSENGER DOOR FS338.963 FRAME AND INTERCOSTAL DD1 CLEAT INBD SIDE CORRODE. PAX DOOR FS338.963. FRAME AND INTERCOSTAL DD1 CLEAT. ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00. CORROSION EXIST ON 2 ELEMENT, OUT OF LIMITS, REPLACE CLEAT IAW SRM 52-Feb 18, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026021875863Cleat · corrodedPASSENGER DOOR FS338.963 FRAME AND INTERCOSTAL DD5 CLEAT CORRODE. INSTALLED NEW PAX DOOR FS338.963 FRAME AND INTERCOSTAL DD5 CLEAT. IAW. SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.Feb 18, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026021875848Cleat · corrodedPASSENGER DOOR FS338.963 FRAME AND LOWER CHANNEL CLEAT INBD SIDE CORRODE. PASSENGER DOOR FS338.963 FRAME AND LOWER CHANNEL CLEAT INBD SIDE. ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00. CORROSION EXIST ON 2 ELEMENT, OUT OF LIMITS, REPLACE CLEAT IFeb 18, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026021875835Intercostal · corrodedPASSENGER DOOR FS338.963 FRAME AND INTERCOSTAL DD5 CLEAT INBD SIDE CORRODE. PAX DOOR FS338.963. FRAME AND INTERCOSTAL DD5 CLEAT. ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00. CORROSION EXIST ON 2 ELEMENT, OUT OF LIMITS, REPLACE CLEAT IAW SRM 52-0Feb 18, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR IPXA2026033182348Web · crackedLEFT WING T/E, RIB 9 INNER UPPER WEB ATTACHED TO SKIN HAD ONE CRACK. INSTALLED, THE WEB IAW SRM 51-40-21-001Feb 18, 2026 · N135UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR SWAA2026033172071Strap · corrodedCORROSION ON OUTER RT WING LEADING EDGE LOWER ATTACH STRAP, OSS 60.69. REPAIRED THE RT WING OTBD FIXED LEADING EDGE ATTACH STRAP OTBD IAW EA 26-157-00485, SRM 51-40-02; DWG 112A4401, SHEET 55, & SHEET 56, REV A, DWG 112A4402, SHEET 40, REV A, & DWG 116A5300,Feb 18, 2026 · N8633A · Boeing 7378H4 · Wing, Attach FittingsSDR IPXA2026032582927Shear Tie · crackedLEFT WING T/E ABOVE FLAP TRACK NR 4, OTBD SHEAR TIE CRACKED. INSTALLED A NEW LT WING T/E SHEAR TIE IAW SRM 51-40-21.Feb 18, 2026 · N135UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2026032973627Structure · corrodedAFT CARGO- FR 54.2 CEILING STRUCTURE HAS CORROSION, 46 PLACES FROM LH TO RH SIDE. REMOVED CORROSION ON CEILING STRUCTURE (03 SECTION) ON FR 54.2FROM LT TO RT SIDE. IAW SRM 51-74-10. INSTALLED NEW CEILING STRUCTURE IAW SRM 51-40-21.Feb 18, 2026 · N135UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026031880048Landing · crackedRIGHT WING LOWER SURFACE PANEL 675DB ATTACHMENT STRUCTURE HAS A CRACKED ON MARKED AREA. REMOVED CAMLOC FASTENER AND RIVETS ON RH WING LOWER SURFACE PANEL 675DB ATTACHMENT STRUCTURE IAW SRM 57-41-12-201 PAR 5 C(3)(A) AND SRM 51-40-21-001. INSTALLED NEW CAMLOC Feb 18, 2026 · N135UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2026031882408Landing · crackedLEFT WING T/E, PANEL 575DB CUTOUT, SUPPORT PANEL HAD ONE CRACK. REMOVED THE CAMLOC FASTENER & RIVETS ON THE LT WING T/E SUPPORT PANEL 575DB CUTOUT IAW SRM 57-41-12-201, PAR 5, C(3)(A) & SRM 51-40-21-001. INSTALLED A NEW CAMLOC IAW SRM 57-41-12-201, PAR 5 C 3Feb 18, 2026 · N135UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2026032582890Web · crackedLEFT WING T/E ABOVE FLAP TRACK NR 4, INBD WEB CRACKED. REMOVED CRACKED WEB AT LT WING T/E FLAT TRACK NR 4, INBD IAW SRM 51-40-21-001. INSTALLED WEB AT LT WING T/E ABOVE FLAP TRACK NR 4, INBD IAW SRM 51-40-21-001.Feb 18, 2026 · N135UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2026031782997Angle · crackedLEFT WING OTBD FLAP, INBD EDGE ANGLE BROKEN. REMOVED THE BROKEN ANGLE IAW SRM 51-40-21-001. INSTALLED THE ANGLE IAW SRM 51-40-21-001, & SRM 51-24-00-001.Feb 18, 2026 · N135UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2026032079785Support Bracket · crackedLEFT WING KRUEGER BOX AREA, STOP FITTING BRACKET SUPPORT IS CRACKED. REMOVED THE BRACKET SUPPORT CRACKED ON L/H WING KRUEGER BOX AREA IAW SRM 51-40-21-001 STEP 6 D. INSTALLED NEW STOP FTG BRACKET SUPPORT IAW SRM 51-40-21-001.Feb 18, 2026 · N135UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2026032079826Support Bracket · crackedFAULT-STR-Z500- L/H WING KRUEGER BOX AREA, KRUEGER FLAP CONNECTOR BASE BRACKET SUPPORT IS CRACKED. DOT 21-09 INSTALLED NEW SUPPORT BRACKET (ANGLE) AND SUPPORT BRACKET IAW A300 SRM 51-40-21-001.Feb 18, 2026 · N135UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2026032182096Rub Strip · crackedLEFT WING TRAILING EDGE, OTBD AILERON ACTUATOR AREA, LOWER INBD RUB STRIP HAD ONE HOLE. INSTALLED A NEW RUB STRIP IN LT WING TE, OTBD AILERON ACTUATOR AREA, LOWER INBD IAW SRM 51-40-21-001.Feb 18, 2026 · N135UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR SWAA2026032472094Scuff Plate · crackedCRACKED FWD CORNER SCUFF PLATE. REPAIRED BY WELDING FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, & BAC 5975.Feb 18, 2026 · N920WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032471800Light · deterioratedDETERIORATED PHOTOLUMINESCENT FLOOR LIGHT. REPLACED THE PHOTOLUMINESCENT PROXIMITY LIGHTING IAW AMM-33-51-15-400-802.Feb 18, 2026 · N920WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026032372089Support · crackedCRACKED SUPPORT ZEE, BTWN BS 747 - 847, STRINGER 25L. REPLACED THE SUPPORT ZEE SECTION IAW SRM 51-40-02, SRM 53-00-53-2R-5, SRM 51-10-02, ITEM 9, AND DWG 146A7502, SHEET 29, REV -, DWG 146A7500, SHEET 85, REV A.Feb 18, 2026 · N7889A · Boeing 73779L · Fuselage Miscellaneous StructureSDR SWAA2026032372078Gusset · crackedCRACKED GUSSET, BS 500D, STRINGER 19L. REPLACED GUSSET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, STEP 9, AND DWG 143A7902, SHEET 174, REV -.Feb 18, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032372087Bulkhead · corrodedCORRODED BULKHEAD BS 727, BTWN STRINGERS 27L - 27R, RBL 5, WL 150.1. REPAIRED THE BULKHEAD IAW 26-153-00585-WIP1.Feb 18, 2026 · N7889A · Boeing 73779L · Fuselage Main, BulkheadSDR SWAA2026032372079Angle · crackedCRACKED ANGLE, AFT FACE OF FRAME BS 500, STRINGER 26L, REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A7505, SHEET 82, REV -.Feb 18, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032372080Pin · corrodedPITTING CORROSION ON LOWER PIN AT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR LUGS. REPLACED LOWER PIN AT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR LUGS AND INSTALLATION IS TO BE ACCOMPLISHED ON TTG8Q002BC0D.Feb 18, 2026 · N245WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026032072090Cargo Track · crackedCRACK CARGO TRACK BS 460 ; RBL 14 FWD CARGO COMPARTMENT. REPAIRED CARGO TRACK LOCATED BTW BS400 TO BS500 PLUS 14INCH AND RBL14 FWD CARGO COMPARMENT IAW SRM 53-00-53-2R-3 REPAIR 3 AND DWG 143A7500 SHEET 59 REV -.Feb 18, 2026 · N7889A · Boeing 73779L · Fuselage, Seat/Cargo Attach FittingsSDR WRNA202603190003Door Frame · puncturedDURING INSPECTION OF AFT CARGO DOOR, FOUND FRAME PUNCTURE HOLE AND CRACK ON AFT SECTION OF CARGO DOOR SKIN.Feb 18, 2026 · N903AR · Boeing 747428F · Fuselage Main, StructureSDR WRNA202603190002Spar · corrodedLOWER FUSELAGE AT LH AND RH FWD SPAR OF CENTER TANK AT STA. 987 (APROX), SHOWS CORROSION.Feb 18, 2026 · N903AR · Boeing 747428F · Fuselage Main, StructureSDR WRNA202603190001Skin · corrodedLOWER FUSELAGE CENTER WING FRONT SPAR AT STA. RBBL 127.50, LOWER PANEL CORROSION.Feb 18, 2026 · N903AR · Boeing 747428F · Fuselage Main, Plate/SkinSDR SWAA2026031972060Access Panel · damagedELONGATED HOLE ON THE RT WING T/E ACCESS PANEL 661AB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.Feb 18, 2026 · N463WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2026031972061Access Panel · damagedELONGATED HOLE ON THE RT WING ACCESS PANEL 661CB TRAILING EDGE. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.Feb 18, 2026 · N463WN · Boeing 7377H4 · Wing, Plate/SkinSDR 2026FA0000190Fuel Tank · corrodedLOWER FUSELAGE LEFT CENTER TANK STA. 987 (APROX), SHOWS CORROSION ,MKD 66, FWD SPAR.Feb 18, 2026 · N903AR · Boeing 747428F · Fuel StorageSDR 2026FA0000189Skin · puncturedDURING INSPECTION OF AFT CARGO DOOR, FRAME FOUND PUNCTURED HOLE AND CRACK ON AFT SECTION OF CARGO DOOR SKIN.Feb 18, 2026 · N903AR · Boeing 747428 · Cargo/Baggage DoorsSDR QXEA2026031800062Seat Track · corrodedRH SEAT TRACK AT FRAME 84 RBL 11 CORRODED. BLENDED AREA AND REMOVED MATERIAL OUT OF LIMITS. FABRICATED DOUBLER IAW E175 SRM 53-23-10. HEAT TREATED AND APPLIED TOP COAT. INSTALLED REPAIR AND RESTORED FINISH IAW E175 SRM 53-23-10.Feb 18, 2026 · N633QX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR QXEA2026031800061Shear Web · corrodedAFT WET AREA RH SHEAR WEB IS CORRODED AT FRAME 87.BLENDED AREA AND FOUND OUT OF LIMITS AFTER EVALUATION. REPLACED SHEAR WEB IAW E175 SRM 51-40-08, RESTORED FINISH.Feb 18, 2026 · N633QX · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR QXEA2026031800060Gusset · corrodedAFT WET AREA GUSSET AT FRAME 90 RBL 11 IS CORRODED. BLENDED OUT CORROSION AND MATERIAL LOSS WAS 100% . REPLACED GUSSET IAW E175 SRM 51-40-08Feb 18, 2026 · N633QX · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR QXEA2026031800059Gusset · corrodedAFT WET AREA GUSSET AT FRAME 90 RBL 24 IS CORRODED.BLENDED CORROSION AND MATERIAL LOSS WAS 100% AND OUT OF LIMITS. REPLACED GUSSET IAW E175 SRM 51-40-08.Feb 18, 2026 · N633QX · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR QXEA2026031800058Sill Drain · corrodedAFT WET AREA RH MOP SILL IS CORRODED AT FRAME 88-89 RBL 36-40. BLENDED CORROSION AND MATERIAL LOSS WAS 100% AND OUT OF LIMITS. REPLACED THE SILL IAW E175 SRM 51-40-08.Feb 18, 2026 · N633QX · Emb ERJ170200LR · Fuselage Main, StructureSDR IPXA2026031281437Web · chafedRIGHT WING, MLG CYLINDER DOOR CUTOUT (WING SIDE), AFT I/B SKIN PLATE WITH CHAFFING. DOT 73-019. REWORKED CHAFING WITH HAND ABRASION ON R/H WING, MLG CYLINDER DOOR CUTOUT (WING SIDE), AFT I/B SKIN IAW A300-600 SRM 51-73-10-001. REMOVED WEB AT R/H WING, MLG CYLIFeb 18, 2026 · N135UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR SWAA2026031371733Vapor Barrier · crackedTWO CRACKS ON THE VAPOR BARRIER, BS 663, RBL 45. REPAIRED THE VAPOR BARRIER IAW SRM 51-70-04-2R-10, REPAIR 10.Feb 18, 2026 · N240WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2026030972037Diffuser · missingCEILING PANEL EXIT LIGHT ASSY FOR OVERWING EXITS IS MISSING DIFFUSER ATTACH CLIP. REMOVED AND REPLACED CEILING PANEL EXIT LIGHT ASSY FOR OVERWING EXITS IAW AMM 33-51-01-960-802.Feb 18, 2026 · N246LV · Boeing 7377H4 · Emergency LightingSDR IPXA2026030580676Rib · crackedLEFT WING KRUEGER BOX STRUCTURE, CENTER CLOSING RIB IS CRACKED AT THE LOWER ATTACHED FLANGE. REMOVED ATTACHED FLANGE AT L/H WING KRUEGER BOX STRUCTURE CENTER CLOSING RIB IAW A300-600 SRM 51-40-21. INSTALLED NEW ATTACHED FLANGE IAW SRM 51-40-21 AT LT WING KRUFeb 18, 2026 · N135UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA2026030566915Connector · faultedRIGHT ENG OVERHEAT AT CRUISE, 4512 MSG WENT OUT AFTER TWO MINUTES & ENGINE AT IDLE THRUST. ALL ENGINE INDICATIONS WERE NORMAL. R & R FLEX-CONNECTOR AND COUPLING V-BAND CLAMP IAW AMM 36-11-15,. LEAK CHECKED GOOD. OK FOR SERVICE.Feb 18, 2026 · N455UP · Boeing 75724APF · Fire Protection System WiringSDR SIMA20260218003Stringer · corrodedSTGR 27R CORRODED BTW FR 90-90A. (MAJOR REPAIR) (LEVEL 2 CORROSION) REMOVED AND REPLACED STGR 27R BETWEEN FR 89-90A IAW ERJ 170 SRM 51-40-08.Feb 18, 2026 · N770JM · Emb ERJ170100LR · Fuselage Main, Longeron/StringerSDR SIMA20260218002Shear Tie · corrodedSSI 53-23-003 SHEAR CLIP AT FR 88 BTW STGR 27R-28R CORRODED. (LEVEL 2 CORROSION) REMOVED AND REPLACED SHEAR CLIP AT FR 88 BTW STGR 27R-28R IAW ERJ 170 SRM 51-40-08.Feb 18, 2026 · N770JM · Emb ERJ170100LR · Fuselage Internal Mounting StructureSDR SIMA20260218004Shear Tie · corrodedSSI 53-23-003 SHEAR CLIP AT FR 89 STGR 27R-28R CORRODED. (MAJOR REPAIR) (LEVEL 2 CORROSION) REMOVED AND REPLACED SHEAR CLIP AT FR 89 STGR 27R-28R IAW ERJ 170 SRM 51-40-08.Feb 18, 2026 · N770JM · Emb ERJ170100LR · Fuselage Internal Mounting StructureSDR SIMA20260218006Shear Tie · corrodedSSI 53-23-003 SHEAR CLIP AT FR 90 STGR 25R-27R CORRODED. (MAJOR REPAIR) (LEVEL 2 CORROSION). REMOVED AND REPLACED SHEAR CLIP AT FR 90 STGR 25R-27R IAW ERJ 170 SRM 51-40-08.Feb 18, 2026 · N770JM · Emb ERJ170100LR · Fuselage Internal Mounting StructureSDR SIMA20260218005Shear Tie · corrodedSSI 53-23-003 SHEAR CLIP AT FR 90 STGR 28R-29R CORRODED. (LEVEL 2 CORROSION) REMOVED AND REPLACED SHEAR CLIP AT FR 90 STGR 28R-29R IAW ERJ 170 SRM 51-40-08.Feb 18, 2026 · N770JM · Emb ERJ170100LR · Fuselage Internal Mounting StructureSDR CALA2026030314257Transition Panel · corrodedFWD CARGO BAY LT TRANSITION PANEL FROM BS 500C+15 - 500L, LBL 21 CORRODED. THE CORRODED AREA ON THE TRANSITION PANEL FROM BS 500C+15 - 500K, LBL 21 FOUND TO BE 100% MATERIAL LOSS IN MULTIPLE AREAS IAW SRM 53-00-53-1A-2, FIG 103, REMOVED DAMAGED TRANSITION PAFeb 18, 2026 · N37437 · Boeing 737924ER · Fuselage Miscellaneous StructureSDR AALA202603021155Support Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SUPPORT ANGLE AT BS 992 BETWEEN LBL 33 AND LBL 44. REPLACED SUPPORT PER AARD 51-00-05-1.Feb 18, 2026 · N983AN · Boeing 737823 · Fuselage Miscellaneous Structure