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 SWIA2026021977508Coaming · crackedLH UPPER TRANSCOWL INNER COAMING IS CRACKED. REPAIRED WITH NEW LH UPPER TRANSCOWL INNER COAMING IAW REO 670-54-21-1803 REV --Feb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026021977506Stiffener · gougedRT UPPER TRANSCOWL ZED STIFFENER IS GOUGED. REPAIRED RT UPPER TRANSCOWL IAW REO 670-54-21-1810 REV -.Feb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026021977505Coaming · chafedRT UPPER TRANCCOWL INNER COAMING IS CHAFED FWD LATCH. COMPLIED WITH REPAIR OF THE RT UPPER TRANCCOWL INNER COAMING IAW REO 670-54-21-1812, REV-.Feb 19, 2026 · N611SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026021977445Skin · dentedLEFT INBD FLAP HAS DENT ON LOWER EXTERNAL SKIN AT APPROX WS 70. REPAIRED LT INBD FLAP ON LOWER EXTERNAL SKIN AT APPROX WS70, IAW SRM 57-52-01-201-005-A01, 57-52-01-995-803.Feb 19, 2026 · N611SK · Cndair CL6002C10 · Trailing Edge FlapsSDR CALA2026092319705Bulkhead Web · crackedVERTICAL PRESSURE DECK WEB CRACKED 4 INCH BELOW HORIZONTAL DECK AT STA 663 RBL 34. INSTALLED A REPAIR IAW SRM 57-10-10-2R-3, ALTERNATIVE 2.Feb 19, 2026 · N14735 · Boeing 737724 · Fuselage Main, BulkheadSDR REXA2026080601526Hinge · crackedCRACK ON HINGES (2EAS) IN STEP PANEL 832ET, 832FT (1EA), AT PASSENGER DOOR. (L1) (PTAS) HINGE (2EAS) IN STEP PANEL 832ET WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-41-02-001-001-A01 AND CRJ-900 AMM 20-21-00-910-801 (CONFIG A01), HINGE (Feb 19, 2026 · N297PQ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026080601525Hinge · crackedCRACK ON HINGES (2EAS) IN STEP PANEL 832ET, 832FT (1EA), AT PASSENGER DOOR. (L1) (PTAS) HINGE (2EAS) IN STEP PANEL 832ET WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-41-02-001-001-A01 AND CRJ-900 AMM 20-21-00-910-801 (CONFIG A01), HINGE (Feb 19, 2026 · N297PQ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026080601524Hinge · crackedCRACK ON HINGES (2EAS) IN STEP PANEL 832ET, 832FT (1EA), AT PASSENGER DOOR. (L1) (PTAS) HINGE (2EAS) IN STEP PANEL 832ET WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-41-02-001-001-A01 AND CRJ-900 AMM 20-21-00-910-801 (CONFIG A01), HINGE (Feb 19, 2026 · N297PQ · Cndair CL6002D24 · Fuselage, Door HingeSDR SWIA2026021975919Skin · gougedRIGHT WING LEADING EDGE, NR 2 SLAT, CENTER UPPER AFT IS GOUGED, REMOVED DAMAGE ON THE RT SLAT NR 2 LEADING EDGE AFT UPPER SIDE IAW SRM 51-12-00-001-001-A01. COMPLIED WITH STEPS OF REO 670-57-42-2441 REV-- FOR TRIM/BLENDED AREAS. COMPLIED WITH SKYWEST TASK CARFeb 19, 2026 · N732SK · Cndair CL6002C10 · Leading Edge DevicesSDR REXA2026042800393Angle · corrodedCORROSION ON MOUNTING ANGLE OF LOWER SILL AREA AT SERVICE DOOR CUTOUT DUE TO EXCESSIVE CORROSION ON MOUNTING ANGLE OF LOWER SILL AREA AT SERVICE DOOR CUTOUT WAS REPLACED PER CRJ900 SRM 53-21-23-101-001-A02,CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-Feb 19, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026042800379Seat Track · corrodedCORROSION ON MID CAP ANGLE OF LOWER SILL AREA AT PASSENGER DOOR CUTOUT MID CAP ANGLE OF LOWER SILL AREA AT PASSENGER DOOR CUTOUT WAS REPLACED BY EXCESSIVE CORROSION PER CRJ900 SRM 53-21-23-101-001-A02 AND SRM 51-41-02-001-001-A01Feb 19, 2026 · N297PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026042800371Protector · crackedCRACK ON HARNESS PROTECTOR OF FWD HINGE ARM AT CENTER BAGGAGE BAY DOOR HARNESS PROTECTOR OF FWD HINGE ARM AT CENTER BAGGAGE BAY DOOR WAS REPAIRED PER EA CRJ952-21859 REV. IRFeb 19, 2026 · N297PQ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026042800370Bracket · corrodedCORROSION ON BOTH SUPPORT (2EA) OF ELECTRICAL CONECTORS PX19, PX34, PX17 AND PX33 AT MLG WHEEL WELL SUPPORT (2EA) OF ELECTRICAL CONECTORS PX19, PX34, PX17 AND PX33 AT MLG WHEEL WELL WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01Feb 19, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026042800369Support · corrodedCORROSION ON BOTH SUPPORT (2EA) OF ELECTRICAL CONECTORS PX19, PX34, PX17 AND PX33 AT MLG WHEEL WELL SUPPORT (2EA) OF ELECTRICAL CONECTORS PX19, PX34, PX17 AND PX33 AT MLG WHEEL WELL WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01Feb 19, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026042800368Diaphragm · crackedCRACK ON DIAPHRAGM AT FWD AREA OF MLG W/W BTW FS= 797 TO FS= 807 LBL/RBL 35. (2EA). DIAPHRAGM (2EA) AT FWD AREA OF MLG W/W BTW FS= 797 TO FS= 807 LBL/RBL 35 WERE REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 & SRM 51-41-02-001-001-A01Feb 19, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, BulkheadSDR REXA2026042800367Diaphragm · crackedCRACK ON DIAPHRAGM AT FWD AREA OF MLG W/W BTW FS= 797 TO FS= 807 LBL/RBL 35. (2EA). DIAPHRAGM (2EA) AT FWD AREA OF MLG W/W BTW FS= 797 TO FS= 807 LBL/RBL 35 WERE REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 & SRM 51-41-02-001-001-A01Feb 19, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, BulkheadSDR REXA2026042800366Striker · corrodedCORROSION ON STRIKER SEAL OF LOWER SILL AREA AT SERVICE DOOR CUTOUT STRIKER SEAL OF LOWER SILL AREA AT SERVICE DOOR CUTOUT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01.Feb 19, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR IPXA2026031499164Floorbeam · corrodedMAJOR REPAIR, MAIN DECK FLOOR AREA STA 1600 LBL 49 FLOORBEAM UNDERNEATH SURFACE HAS CORROSION. REMOVED CORROSION AT MAIN DECK FLOOR AREA STA 1600 LBL 49 FLOOR BEAM UNDERNEATH SURFACE REF SRM 51-10-02-0G-0 REPAIRED PER BOEING 757-200PF SRM 53-00-51-2R-6 REPAIFeb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026033097727Bracket · crackedBEHIND BULK CARGO FR 78-79 ON RH SIDE WIRE BRACKET IS BROKEN. INSPECTED AND VERIFIED INSTALLED NEW BRACKET IAW SRM 51-40-21-001Feb 19, 2026 · N135UP · Airbus A300F4622R · Fuselage Main, Attach FittingsSDR IPXA2026032593744Rib · crackedCRACK IN TOP OF AFT EXTERIOR SKIN JUST AFT OF RIB 7, INBD SIDE, RIB 7 INSTALLED IAW SRM 51-40-21-001.Feb 19, 2026 · N135UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2026022498959Angle · crackedE & E COMPARTMENT, FRAME 10 LT MAIN DECK FLOOR STRUCTURE HAD A BRACKET CRACKED. INSTALLED A NEW BRACKET ON FRAME 10 LT MAIN DECK FLOOR STRUCTURE IAW SRM 51-40-21.Feb 19, 2026 · N135UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR ASAA2026021965187Rib · crackedLEFT HORIZONTAL STAB RIB 182A5302 AT APPROXIMATELY HSS 92.70 HAS MULTIPLE CRACKS. GROUNDED - YES. REPAIRED LT HORIZONTAL STAB RIB 182A5302, IAW SRM 55-10-09-2R-4.Feb 19, 2026 · N546AS · Boeing 737890 · Horizontal Stabilizer, Spar/RibSDR SWAA2026033072075Fitting · deterioratedDETERIORATED HARDWARE ON GIRT BAR FITTINGS ENTRY AND SERVICE DOOR. REPLACED THE HARDWARE ON GIRT BAR FITTINGS IAW SOPM 20-50-01, REV 40.Feb 19, 2026 · N8633A · Boeing 7378H4 · Emergency EquipmentSDR IPXA2026031988378Fairing · crackedNR 2 OTBD, THRUST REVERSER UPPER AFT TRANSITION FAIRING STRUCTURE WAS CRACKED. INSTALLED A NEW TRANSITION FAIRING STRUCTURE IAW SRM 51-40-21-001; AT NR 2 OTBD THRUST REVERSER UPPER AFT TRANSITION FAIRING STRUCTURE.Feb 19, 2026 · N135UP · Airbus A300F4622R · Engine Thrust ReverserSDR HNAA2026032600238Skin · corrodedLEFT MAIN LANDING GEAR BAY LOWER SKIN FWD OF MAIN LANDING GEAR MAIN SIDE STRUT CORRODED. R & R THE LT MAIN LANDING GEAR BAY LOWER SKIN FWD OF THE MAIN LANDING GEAR SIDE STRUT IAW SRM 51-40-02.Feb 19, 2026 · N699AE · Emb EMB145LR · Wing, Plate/SkinSDR SWAA2026032472502Pressure Deck · crackedCRACK INDICATION FOUND ON THE HORIZONTAL PRESSURE DECK, LBL 31, BS 663 - 675 IN THE MAIN WHEEL WELL. PERFORMED CATEGORY A REPAIR IAW SRM 53-40-51-2R-2, REPAIR 2.Feb 19, 2026 · N920WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026032472504Stub Frame · crackedCRACK INDICATION ON STUB FRAME, BS 294.5 - 296.5, STRINGERS 8R - 9R. REPLACED THE STUB FRAME IAW SRM 51-10-02-0G-0, ITEM 9, & DWG 141A8370, SHEET 9, REV D.Feb 19, 2026 · N920WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2026032472500Floor Support · crackedCRACKED FLOOR SUPPORT, BS 312 - 328, LBL 45. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 141A5400, SHEET 26, REV-.Feb 19, 2026 · N920WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032472334Floorbeam · crackedCRACKED FLOORBEAM ANGLE BS 695, RBL 24.75. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-02-0G-0, AND DWG 273A9110, SHEET 6, REV A.Feb 19, 2026 · N920WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2026032472327Strap · corrodedCORRODED STRAP, INTERNAL CAVITY OR LEADING EDGE OFSS456, RT WING. REPAIRED THE ATTACH STRAP IAW EA-26-157-00508WIP1, EA-26-157-00508WIP2, EA-26-157-00508WIP3, & EA-26-157-00508.Feb 19, 2026 · N920WN · Boeing 7377H4 · Wing, Attach FittingsSDR IPXA2026032299492Stringer Splice · corrodedAFT CARGO COMP FLOOR STGR AT STA. 1460, RBL 15 HAS CORROSION AT BOTTOM SIDE. INSTALLED 1 EA NEW FLOOR STRINGER AT AFT CARGO COMPARTMENT STA. 1460, RBL 15 IAW B757-200PF SRM 51-40-02-0G-0 PAR 4 AND PAR 7.Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Longeron/StringerSDR SWAA2026032372084Light · deterioratedDETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ALONG PASSENGER CABIN (1KT). REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ALONG PASSENGER CABIN (1KT) IAW AMM 33-51-15-400-802. AND INSTALLATION IS COVERED WITH TTG8Q01AEKT8 AND TTG8Q002B7TQ STEP 22Feb 19, 2026 · N245WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026032372493Tie Clip · crackedCRACKED TIE CLIP, BS 277, STRINGER 10R. REPLACED THE TIE CLIP IAW SRM-51-10-02, ITEM 9, AND DWG 141A1110, SHEET 18, REV -.Feb 19, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032372323Fitting · crackedCRACKED FITTING, BS 947.5, STRINGER 26L REPLACED THE FITTING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 149A8103, SHEET 7, REC A.Feb 19, 2026 · N7889A · Boeing 73779L · Fuselage Main, Attach FittingsSDR SWAA2026032372313Support Bracket · crackedCRACKED SUPPORT BRACKET ON PNEUMATIC DUCT, BS 540, LBL 6. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02-0G-0, & SRM 51-10-02, ITEM 9.Feb 19, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026031493675Support Angle · corrodedAPU INLET SUPPORT STRUCTURE UPPER SUPPORT ANGLE HAS CORROSION. LOWER SUPPORT ANGLE APU INLET P/N 148N3152-2 WILL BE INSTALLED ON JOB CARD T3F18E008AL0N LINE # 614Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR CALA2026032314726Intercostal · crackedMAIN CABIN STA 312-328 LBL45 INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN STA 312@328 LBL 45. IAW SRM 51-40-02-0G-0 AND DWG 141A5400Feb 19, 2026 · N57439 · Boeing 737924ER · Fuselage Miscellaneous StructureSDR SWAA2026032072325Web · crackedCRACKED WEB BTW BS 500A - 500B, STRINGER 26R, WL 152. REPAIRED THE WEB, BS 500A - 500B, S26R, WL 152. IAW SRM 53-30-53-2R-1, REPAIR 1.Feb 19, 2026 · N7889A · Boeing 73779L · Fuselage Miscellaneous StructureSDR SWAA2026032072326Shield · corrodedCORROSION SHIELD WEB LOCATED BTW BS 492.4 TO BS 500A RBL 23 WL 208. 1 AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB LOCATED BTW BS 492.4 TO BS 500A RBL 23 WL 208. 1 AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 143A0080 SHEET 23 REV -.Feb 19, 2026 · N7889A · Boeing 73779L · Fuselage Miscellaneous StructureSDR SWAA2026032072314Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED PNEUMATIC DUCT BS540 AT LEVEL RBL6 AT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET LOCATED PNEUMATIC DUCT BS540 AT LEVEL RBL6 AT AIR CONDITIONING BAY IAW SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9.Feb 19, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032072494Support Angle · crackedCRACK CARGO LINER SUPPORT ANGLE LOCATED STA 867 AND RBL 55 AT AFT CARGO BAY. PERFORMED REPAIR ON CARGO LINER SUPPORT ANGLE LOCATED BETWEEN BS847 AND BS867+14IN IAW B737-700 SRM 51-70-11-2R-0 AND DWG 149A9490 SHEET 21 REV -.Feb 19, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032072497Support Angle · crackedCRACK CARGO LINER SUPPORT ANGLE LOCATED STA 747 AND LBL 51 AT AFT CARGO BAY. REPAIRED CARGO LINER SUPPORT ANGLE LOCATED BETWEEN BS727A AND BS 767 LBL 51 AT AFT CARGO COMPARTMENT IAW SRM 51-70-11-2R-0.Feb 19, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032072496Support Angle · crackedCRACK CARGO LINER SUPPORT ANGLE LOCATED STA 727B AND LBL 51 AT AFT CARGO BAY. REPAIRED CARGO LINER SUPPORT ANGLE LOCATED BETWEEN BS727A AND BS727D LBL 51 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-70-11-2R-0.Feb 19, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032072495Support Angle · crackedCRACK CARGO LINER SUPPORT ANGLE LOCATED STA 727C AND LBL 51 AT AFT CARGO COMPARTMENT. REPAIRED CARGO LINER SUPPORT ANGLE LOCATED STA 727C AND LBL 51 AT AFT CARGO BAY IAW SRM 51-70-11-2R-0 . IFeb 19, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026031699642Strap · corrodedAFT CARGO COMP LH SIDE CEILING DECOMPRESSION PANEL STRAP BETWEEN BS 1560 & 1580 IS CORRODED. INSTALLED NEW CEILING DECOMPRESSION PANEL STABILIZATION STRAP, AND 1EA. REPAIR SPLICE AT STA. 1610 L/H  IAW B757-200PF SRM 51-40-02-0G-0.Feb 19, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR SWAA2026031972308Crossbeam · crackedCRACKED CROSSBEAM, BS 540, RBL 24.75 - RBL 45.5. REPLACED THE CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, STEP 9, & DWG 143A0060, SHEET 36, REV A.Feb 19, 2026 · N463WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026031972307Stiffener · crackedCRACKED VERTICAL STIFFENER, BS 540, LBL 24.75. REPLACED THE VERTICAL STIFFENER IAW SRM 51-10-02-0G-0, PARAGRAPH 9, AND DRAWING 111A2001, REV -, SHEETS 53;54, & 55.Feb 19, 2026 · N463WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026031972305Fitting · corrodedCORRODED LOWER LUG FITTING, AFT FACE OF LT HORIZONTAL STAB. REPAIRED LOWER LUG FITTING LOCATED AFT FACE POSITION LT HORIZONTAL STAB IAW 26-155-00498-WIP1, 26-155-00498-WIP2, 26-155-00498-WIP3, 26-155-00498-WIP4, 26-155-00498-WIP5, & EA 26-155-00498.Feb 19, 2026 · N463WN · Boeing 7377H4 · Fuselage, Stabilizer Attach FittingsSDR SWAA2026031972306Fitting · corrodedCORRODED LOWER LUG FITTING, AFT FACE POSITION OF THE RT HORIZONTAL STAB. REPAIRED LOWER LUG FITTING ON THE RT HORIZONTAL STAB IAW 26-155-00499-WIP1, 26-155-00499-WIP2, 26-155-00499-WIP3, 26-155-00499-WIP4, AND EA 26-155-00499.Feb 19, 2026 · N463WN · Boeing 7377H4 · Fuselage, Stabilizer Attach FittingsSDR CALA2026031814636Structure · corrodedR2 DOOR CUTOUT INNER CHORD WITH SEVERAL CORROSION AREAS ON UPPER SURFACE. REMOVED AND REPLACED R2 INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 147A8501. REMOVED AND REPLACED R2 INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 147A8501.Feb 19, 2026 · N14735 · Boeing 737724 · Service Doors