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 DALA2026022701387Channel · damagedFORWARD SIDE OF FRAME 60 AT JUST INBOARD OF P'2 TOOLING DAMAGE ON J CHANNEL STIFFENER. STRINGER BEING SPLICED FROM C59.5 TO 63.5 ON ERA 632531-14 REV ORIG. (1469534)Feb 26, 2026 · N858NW · Airbus A330223 · Fuselage Miscellaneous StructureSDR FDEA202602260284Safety Wire · wrong partREMOVED RH DOOR SLIDE MPN 62771-128 MSN M10748 REF FEA G-2560-F0386294 REV NO. A PS P1 AND AMM 25-66-01-4 AND WRI 25-60/513. INSTALLED COPPER SAFETY WIRE (MS20995CY16). REPACKED/ LACED RH SLIDE AND INSTALLED ON AIRCRAFT PER CMM 25-61-31, FEA G-2560-Feb 26, 2026 · N883FD · Boeing 777FHT · Emergency EquipmentSDR FDEA202602260283Safety Wire · wrong partREMOVED LH SLIDE MPN 62771-127 MSN M10268 REF FEA G-2560-F0386282 REV NO. A PS P1 AND AMM 25-66-01-4 AND WRI 25-60/5712 PLACED SLIDE IN LINESHACK 380 INSTALLED COPPER SAFETY WIRE (MS20995CY16). REPACKED/ LACED LH SLIDE AND INSTALLED ON AIRCRAFT PER Feb 26, 2026 · N883FD · Boeing 777FHT · Emergency EquipmentSDR UIEA2026022600069Valve · inoperativeEQUIPMENT COOLING MESSAGE. SUSPECT FLT DECK FLOW REG VALVE INOP. OPENED FLOOR PANEL AND MANUALLY MOVED VALVE TO OPEN. TRANSFER TO DMI 248403 PER MEL 21-61-13 CAT C. R & R FD FLOW REG VALVE AS PER AMM 21-61-09 & AIPC 21-21-06. OPS AND LEAK CHK GOOD. DMI 24840Feb 26, 2026 · N450PA · Boeing 74746NF · Air Distribution SystemSDR N6WA2026022706Angle · corrodedCORROSION AT STGR26R ON ANGLE AT AVI BAY DOOR SURROUND STRUCTURE. REMOVED AND REPLACED ANGLE AT STGR26R AT AVI BAY DOOR SURROUND STRUCTURE IAW CRJ SRM 51-42-06Feb 26, 2026 · N523GJ · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR N6WA2026022705Panel · crackedPAX DOOR STEP AFT SIDE PANEL CRACKED AT HANDRAIL SUPPORT FITTING. REPAIRED ZONE 4, TYPE 1 AND REPAIRED ZONE 2 ON PAX DOOR STEP SIDE PANEL IAW CRJ SRM 52-11-04Feb 26, 2026 · N523GJ · Cndair CL6002C11 · Passenger/Crew DoorsSDR N6WA2026022704Intercostal · corrodedCORROSION AT STGR27L ON INTERCOSTAL AT AVI BAY DOOR SURROUND STRUCTURE. REMOVED AND REPLACED INTERCOSTAL AT STGR27L AT AVI BAY DOOR SURROUND STRUCTURE IAW CRJ SRM 51-42-06Feb 26, 2026 · N523GJ · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR N6WA2026022703Intercostal · corrodedCORROSION ON STGR27R ON INTERCOSTAL ON AVI BAY DOOR SURROUND STRUCTURE. REMOVE AND REPLACED INTERCOSTAL AT STGR27R IAW CRJ SRM 51-42-06.Feb 26, 2026 · N523GJ · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR N6WA2026022702Skin · gougedFUSELAGE SKIN GOUGED AT FS977.00 AT STGR27. REPAIRED FUSELAGE SKIN AT FS977.00 AT STGR27 IAW GOJET EO-C550-53MR-119-OFeb 26, 2026 · N523GJ · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR N6WA2026022701Floorbeam · damagedFUSELAGE CENTER FLOOR ANGLE AND DOOR POST AT FS280.00 AND BL11.128 DAMAGED. REPAIRS FUSELAGE CENTER FLOOR ANGLE AND DOOR POST AT FS280.00 BL11.128 IAW GOJET EO-C550-53MR-053Feb 26, 2026 · N503GJ · Cndair CL6002C11 · Fuselage Main, Floor BeamSDR HNAA2026022700158Unknown · odorSULFER BURNING SMELL IN FLIGHT DECK AND CABIN WITH PACK 2 RUNNING. PERFORMED A GVI AND PACK 2 OPERATIONAL TEST IAW AMM 21-51-00 NO DEFECTS NOTED. A/C OK FOR SERVICE AT THIS TIME.Feb 26, 2026 · N651AE · Emb EMB145LR · Cabin Cooling SystemSDR YENA2026022700243Unknown · odorFLT 466 RSW-BOS. LEVEL 2 MAGIC MARKER ODOR NOTICEABLE ONCE LEVEL AT FL340, ODOR NOTICEABLE IN CABIN FROM ROWS 11 TO FORWARD CABIN. RAN ISOLATION CHECKLIST AND SHUT PACK 1 OFF WITH CROSS BLEED. ODOR STILL NOTICEABLE.;ACCOMPLISHED INFO NOTICE 2017-T015M AND PERFFeb 26, 2026 · N905JB · Airbus A321231 · Air Distribution SystemSDR YENA2026022700240Control Unit · faultedFLT 20, LHR-JFK (ETOPS). CLASS II MAINTENANCE MSG FUEL ( CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY 1) FAULT(S) INDICATED BY FUEL ).; REMOVED AND REPLACED 9QJ PER AMM 28-46-34. NO FAULTS NOTED. OPS CHK GOOD. CLASS 2 MSG Feb 26, 2026 · N4058J · Airbus A321271NX · Fuel Indicating SystemSDR CALA2026022714122Battery Pack · no testPOWER SUPPLY M1672 FAILED CAPACITY CHECK. REPLACED EMERGENCY LIGHT BATTERY PACK M1672. OP CKS GOOD. MM 33-51-06-960-805.Feb 26, 2026 · N18220 · Boeing 737824 · Emergency LightingSDR CALA2026022714121A/C Pack · contaminatedSMOKE/FUMES IN CABIN AFTER RESET OF PACK 2. VERIFIED WITH FLIGHT CREW AND OPERATIONS THAT ACFT WAS DE-ICED WITH APU & PACKS ON. RAN PACKS TO CLEAR GLYCOL SMOKE ODOR, PACK 2 OVERHEATED AGAIN. ACCOMPLISHED TSM 05-50-00 AND AMM 05-51-10 AFTER RUNNING PACK 1Feb 26, 2026 · N461UA · Airbus A320232 · Cabin Cooling SystemSDR CALA2026022714120Battery Pack · inoperativeEMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCHES PROCEDURE - ALL EMERGENCY LIGHTS CONNECTED TO POWER SUPPLY M33099 INOP REPLACED BATTERY PACK AT M33098 REF AMM 33-51-06-960-802. OPS CK GOOD.Feb 26, 2026 · N776UA · Boeing 777222 · Emergency LightingSDR CALA2026022714118Battery · inoperativeEMERGENCY LIGHTS AT ON SEAT ROWS 33-38 F AND D SIDES WILL NOT TURN ON WHEN EMERGENCY LIGHTS ARE POWERED ON. REMOVED AND REPLACED AISLE LIGHTS IN ROW 33-38 IAW AMM 33-51-06. NO FIX. REMOVED AND REPLACED WELS CONTROL UNIT NR 26 AND BATTERY IAW AMM 33-51-07. OPFeb 26, 2026 · N26906 · Boeing 7878 · Emergency LightingSDR CALA2026022714117Battery Pack · no testEMERGENCY CEILING AREA LIGHTS OVER 29D AND 34D DO NOT ILLUMINATE. REMOVED AND REPLACED THE BATTERY PACK AT POWER SUPPLY M2627. OPS CHECKED GOOD IAW AMM 33-51-06-960-805.Feb 26, 2026 · N75429 · Boeing 737924ER · Emergency LightingSDR CALA2026022714116A/C Pack · odorTHE CABIN CREW REPORTED SMELLING AN ACRID ODOR ON ARRIVAL. SUSPECT RELATED TO THE PACK 1 OVERHEAT. THE ODOR WAS ABLE TO BE DUPLICATED ONLY WHEN RUNNING PACK 1 OFF THE APU. ACCOMPLISHED CONDITIONAL INSPECTION IAW AMM 05-51-10-200-801-C1, PARA 1, ODOR WAS ISOLAFeb 26, 2026 · N836UA · Airbus A319131 · Cabin Cooling SystemSDR 2026FA0000146Fuel Tank · misinstalledFOLLOWING REMOVAL OF BOTH WINGS FOR CENTRAL WING PANELS REPLACEMENT, ACCESSES ARE PERFORMED IN THE FEEDER TANKS. PIPES, BRACKETS, PUMPS WERE REMOVED. DURING THESE ACCESSES, COMPONENTS IN THE FEEDERS TANKS ARE DISCOVERED INSTALLED WITHOUT PRC & PAINT PROTECTIONFeb 26, 2026 · N990HA · Amd FALCON7X · Fuel StorageSDR DALA2026022701384Web · corrodedCORROSION WEB FRAME LOCATED BTW FR 69 TO FR 70 STR 23L IN AFT GALLEY AREA. FINAL REPAIR RESOLUTION: WELL WRITTEN SIGN OFF; REPLACED WEB FRAME LOCATED BTW FR 69 TO FR 70 STR23L IN AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11, DWG: D53474180, ISSFeb 26, 2026 · N377NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2026022701382Floor Support · corrodedCORROSION FLOOR SUPPORT -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR SUPPORT -Y1162.5 AND FASTENERS LOC FR68 TO FR 69 AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG: DWG D53472780 RELEASE DATE: 26/APR/Feb 26, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2026022701380Seat Track · corrodedCORROSION SEAT TRACK +Y1292 LOCATED AT FR 66 AT AFT GALLEY AREA (SSI 534147). REPLACED SEAT TRACK Y1292 LOCATED AT FR64 TO FR 66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG :10N01048 , ISSUE: F. RELEASE DATE: 19-MAY-15, MEASURE OF CORRFeb 26, 2026 · N327NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026022674574Wedge · delaminatedLEFT WING INBOARD FLAP WEDGE APPEARS TO BE DELAMINATED. VERIFIED NEW REPLACEMENT WEDGE FIT CHECK GOOD IAW SRM 51-40-05. VERIFIED NEW REPLACEMENT WEDGE FIT. INSTALLED NEW FLAP WEDGE IAW AMM 27-51-12.Feb 26, 2026 · N273WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2026022674474Light · dislodgedPASSENGER CABIN SEAT ROW 27ABC PHOTOLUMINESCENT STRIP WORN AND DISLODGED. R & R CABIN PHOTO LUMINESCENT STRIP IAW AMM 33-51-15. INSPECTION C/W.Feb 26, 2026 · N211WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026022674569Battery Pack · inoperativeEXTERIOR EMERGENCY LIGHT AFT OF FWD SERVICE DOOR INOPERATIVE. TROUBLESHOT IAW FIM 33-50 TASK 801. CLEANED CONTACTS AT L730. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK M01674 IAW AMM 33-51-06. OPS CHECKED GOOD.Feb 26, 2026 · N299WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026022674378Seal · crackedLEFT STABILIZER TO BODY UPPER FRONT SPAR SLIDING SEAL CRACKED. REMOVED AND REPLACED THE LT STABILIZER UPPER SLIDING SEAL IAW AMM 53-31-31.Feb 26, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026022674384Seal · crackedRIGHT STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL CRACKED. R & R RT HORIZONTAL STAB FWD UPPER SLIDING SEAL IAW AMM 53-31-31.Feb 26, 2026 · N925WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR JR2R20260226388Shear Tie · corrodedSHEAR TIE AT FR26 STR28R IN FWD CARGO CORRODED. REPLACEDFeb 26, 2026 · N86312 · Emb ERJ170200LL · Fuselage Internal Mounting StructureSDR JR2R20260226041Skin · gougedLEFT WING BEHIND SLAT 1 ON WING L/E SKIN HAS 11 GOUGES. REPAIRED PER ETD.Feb 26, 2026 · N86312 · Emb ERJ170200LR · Leading Edge DevicesSDR GTIA2026022639286Megaphone · inoperativeFORWARD MEGAPHONE VOLUME KNOP MISSING-R&R FWD MEGAPHONE AND OPS CHECK IAW AMM 25-65-51-710-002-A. OPS CHECKED OK. A/C OK FOR SERVICE. MOC # 70473.Feb 26, 2026 · N985NK · Airbus A320271N · Emergency EquipmentSDR JR2R20260226951Shear Tie · corrodedAFT CARGO COMPT, SHEAR TIE CORRODED, FR 86, STR 29R - 29LFeb 26, 2026 · N88310 · Emb ERJ170200LL · Fuselage Internal Mounting StructureSDR JR2R20260226953Shear Tie · corrodedAFT CARGO COMPT, SHEAR TIE CORRODED, FR 86, STR 27R - 28RFeb 26, 2026 · N88310 · Emb ERJ170200LL · Fuselage Internal Mounting StructureSDR FDEA202602260282Skin · dentedHAIL STRIKE (12 EA'S) ON OUTBOARD FLAP TOP SKIN BETWEEN OTEF STA 25 & OTEF STA 222.5, LH WING. OUTBOARD FLAP TOP SKIN BETWEEN OTEF 25 & OTEF STA 222.5 LH WING WAS REPAIRED IAW B767 SRM 57-53-01-2R AND SRM 51-70-10-2R REPAIR 4 FIG 201 SHEET 1 REV 94 DEC15-2Feb 26, 2026 · N135FE · Boeing 7673S2F · Trailing Edge FlapsSDR FDEA202602260281Slide · faultedWHILE ACCOMPLISHING F.E.A. 6-2560-F0386375 FOUND RIVETS PULLED THROUGH AND METAL STRIP PULLED AWAY FROM SLIDE HOUSING. AMM: 25-61-21-04 FEA: 6-25-0-F0386375 REMOVED AND REPLACED L1 DUAL ESCAPE SLIDE - SAFETY PIN PULLED - ARMED AND DISARMED INDICATIONSFeb 26, 2026 · N687FE · Airbus A300F4605R · Escape SlideSDR DALA2026022601365Battery · inoperativeAIRCRAFT 3041, DURING EPSU SYS TEST CIDS1 FAULTING BAT/EPSU (10WL) FWD L. CORRECTIVE ACTION: REPLACED EPSU 10WL BATTERY PER A321 AMM 33-51-38. EPSU SYSTEM TEST GOOD. CIDS INTERFACE AND POWER UP TEST GOOD. (LP 8100287)Feb 26, 2026 · N341DN · Airbus A321213 · Emergency LightingSDR QR9R2026022600001Ejector · inoperativeHEATER EJECTOR ASSEMBLY WAS RECEIVED FROM SUPPLY WITH ZERO HOURS TIME SINCE REPAIR. AN OPERATIONAL CHECK REVEALED THE CLOSED LIGHT WILL NOT ILLUMINATE ON HEATER EJECTOR ASSEMBLY.Feb 26, 2026 · Bolkms BK117C2 · Heating SystemSDR DALA2026022601358Web · crackedWEB AFT LOWER CORNER AT STR-44L BETWEEN C20 AND C21 OF THE FWD CARGO COMPT FOUND CRACK. CUT OUT THE CRACK AREA AND PERFORMED DOUBLER REPAIR ON SHEAR WEB AT FR20-21 S-44LH PER A330 SRM 53-21-14-300-008. (1468507)Feb 26, 2026 · N406DX · Airbus A330941 · Fuselage Miscellaneous StructureSDR JR2R20260226406Rib · crackedLEFT HORIZONTAL STABILIZER OTBD END CAP RIB 14 CRACKED. REPLACED PER SRM.Feb 26, 2026 · N86312 · Emb ERJ170200LR · Horizontal Stabilizer, Spar/RibSDR REXA2026080601523Skin · corrodedAFTER REMOVAL INTERNAL PRODUCTION DOUBLER, CORROSION ON FUSELAGE INNER SKIN, BETWEEN FS= 295 TO FS= 310 AND STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS FOUND CORROSION ON FUSELAGE INNER SKIN, BETWEEN FS= 295 TO FS= 310 AND STGR 26LH TO 26RH AT MAIN AVIOFeb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR U2RA2026051100014Frame · crackedWHILE IN C CHECK - PERFORMED SURFACE HFEC INSPECTION OF FCD 744-53-0017 R2 A 1 INCH CRACK WAS FOUND ON CHORD BETWEEN S-37R AND S-38R. REPAIR PERFORMED PER BOEING BCS MUA N952CA / 25238 FRAME CRACK BS 1140 RH, RBL 80 / WL 330.Feb 25, 2026 · N952CA · Boeing 747428 · Fuselage Main, FrameSDR REXA2026042800412Stringer · corrodedCORROSION ON STRG 23RH BTW FS349 TO FS364 AT MAIN AVIONICS COMPARTMENT CORROSION ON STRG 23RH BTW FS349 TO FS364 AT MAIN AVIONICS COMPARTMENT WAS EVALAUTED OUT OF LIMITS , THEREFORE WAS REPLACED PER CRJ 900 SRM 53-00-00-101-001-A01, SRM 51-42-06-001-001-A01 Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026042800411Stringer · corrodedCORROSION ON STRG 21RH BTW FS364 TO FS379 AT MAIN AVIONICS COMPARTMENT CORROSION ON STRG 21RH BTW FS364 TO FS379 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS , THEREFORE WAS REPLACED PER CRJ-900 SRM 53-00-00-101-001-A01 AND SRM 51-42-06-001-001-A0Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026042800409Stringer · corrodedCORROSION ON STRG 25RH BTW FS 295 TO FS 326 AT MAIN AVIONICS COMPARTMENTT. STRG 25RH BTW FS 280 TO FS 326 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026042800408Channel · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER OF ANTENNA IN FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. PRODUCTION DOUBLER LOCATED ON FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMIFeb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026042800406Channel · corrodedCORROSION ON SEVERAL CHANNEL NUT BTW WS 148.01 TO WS 48.00 LEFT WING FRONT SPART FORWARD, LOWER SECTION. DUE TO EXCESSIVE CORROSION ON SEVERAL CHANNEL NUT BTW WS 148.01 TO WS 48.00 LEFT WING FRONT SPART FORWARD, LOWER SECTION WERE REPLACED PER CRJ900 SRM 51-10Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Wing Miscellaneous StructureSDR REXA2026042800404Floorbeam · crackedCRACK ON ANGLE FS 280 RBL 25 AT E/E COMPARTMENT. ANGLE ON FS 280 RBL 25 AT E/E COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01 .Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026042800403Support Angle · crackedCRACK ON ANGLE SUPPORTS (2EAS) BTW FS=1000, STGR 8LH AND FS= 1051.30, STGR 7LH ANGLE SUPPORTS (2EAS) BTW FS=1000, STGR 8LH AND FS= 1051.30, STGR 7LH WERE FABRICATED AND REPLACED PER EA CRJ953-21721 REV IR , EA CRJ953-21787 REV IR , CRJ 900 SRM 51-42-06-001-00Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026042800402Angle · crackedCRACK ON ANGLE SUPPORTS (2EAS) BTW FS=1000, STGR 8LH AND FS= 1051.30, STGR 7LH ANGLE SUPPORTS (2EAS) BTW FS=1000, STGR 8LH AND FS= 1051.30, STGR 7LH WERE FABRICATED AND REPLACED PER EA CRJ953-21721 REV IR , EA CRJ953-21787 REV IR , CRJ 900 SRM 51-42-06-001-00Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026042800385Channel · corrodedCORROSION ON SEVERAL CHANNEL NUT BTW WS 178.00 TO WS 88.00 RIGHT WING FRONT SPART FORWARD, LOWER SECTION. DUE TO EXCESSIVE CORROSION ON SEVERAL CHANNEL NUTS BTW WS 178.00 TO WS 88.00 RIGHT WING FRONT SPART FORWARD, LOWER SECTION WERE REPLACED PER CRJ 900 SRM Feb 25, 2026 · N297PQ · Cndair CL6002D24 · Wing Miscellaneous Structure