Service difficulty reports

1,771,154 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 IPXA2026091326044Strip · crackedNR 2 PYLON, BETWEEN RIB 4 AND RIB 5, RH STRIP CORNER IS BROKEN. REMOVED 1EA EXTRUSION-EDGING AT NR 2 PYLON BETWEEN RIB 4 AND RIB 5, RH STRIP IAW SRM 51-40-21-001. INSTALLED 1EA EXTRUSION-EDGING AT NR 2 PYLON BETWEEN RIB 4 AND RIB 5, RH STRIP IAW SRM 51-Jul 12, 2026 · N136UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026091426061Plate · crackedNR 2 PYLON, TOP SKIN RH SIDE AT RIB 3 IS CRACKED. REMOVED CRACKED FISHPLATE FROM NO. 2 PYLON, TOP SKIN RH SIDE AT RIB 3 IAW SRM 51-40-21. INSTALLED FISHPLATE BRACKET AT PYLON NR 2 TOP SKIN R/H O/B RIB 3 PER SRM 51-40-21-001.Jul 12, 2026 · N136UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026091125874Web · crackedLH WING, WEB UNDERNEATH SPOILER #5 HAS A CRACK AT I/B SIDE (DOT64-037) INSTALLED NEW INTERCOSTAL WEB P/N 2024-T3.032C B/N 0004481575 TRAVELER# T26/1872446 IAW A300-600PF SRM 51-40-21Jul 12, 2026 · N136UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2026091125996Skin · crackedNR 2 PYLON, TOP SKIN RT SIDE AT RIB 8 IS CRACKED. WELD REPAIRED ON TRAVELER T26/1874956Jul 12, 2026 · N136UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2026090325692Stiffener · crackedLEFT WING, LEADING EDGE INTERNAL STRUCTURE, STIFFENER CRACKED INSIDE FLAP KRUEGER BAY. INSTALLED NEW STIFFENER AT LT WING, LEADING EDGE INTERNAL STRUCTURE IAW SRM 51-40-21,Jul 12, 2026 · N136UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2026082721712Shear Tie · crackedCENTER FUSELAGE FR 45 RH SIDE BASE FRAME FITTING WITH CRACK. ACCOMPLISHED STEP 43 TO STEP 53 FOR REPAIR FRAME 45 RT IAW E0-46789-JIC008 REV2.Jul 12, 2026 · N136UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR IPXA2026081825839Gusset · corrodedNR 2 PYLON, INSIDE PANEL 484BR, AFT BRACKET SHOWS EVIDENCE OF CORROSION. GUSSET BRACKET WAS INSTALLED IAW SRM 51-40-21.Jul 12, 2026 · N136UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR VNAA202609010025Hinge Fitting · corrodedAFTER BUSHING REMOVAL CORROSION WAS FOUND ON CENTER HINGE FITTING L2 AND L6 IN REF TASK CARD TRFKE00GM97B. LUG BORE L2 WAS REPAIRED PER REO 670-57-61-237 REV-, AND LUG BORE L6 WAS CLEANED IAW SRM 51-26-00-001-001-A01, CLEANING THEN INSPECTIONED PER NDT MANUJul 12, 2026 · N642NN · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR VNAA202609010024Hinge Fitting · corrodedAFTER BUSHING REMOVAL CORROSION WAS FOUND ON CENTER HINGE FITTING R2 AND R5 IN REF TASK CARD TRFKE00GM9V5. LUG BORES R2 AND R5 AT CENTER FITTING WERE REPAIRED PER REO 670-57-61-237 REV. - -Jul 12, 2026 · N642NN · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR IPXA2026080624433Support Web · crackedFWD CARGO COMPARTMENT FLOOR STRUCTURE, SUPPORT WEB IS CRACKED BTWN FR 20 AND FR 21 AT Y1470. INSTALLED NEW SUPPORT WEB ON FWD CARGO COMPARTMENT FLOOR STRUCTURE, IAW A300 SRM 51-40-21-001. REVIEWEDJul 12, 2026 · N136UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR REXA2026082401629Skin · corrodedCORROSION AND SCRATCHES AROUND OF SETTLEMENT AREA WERE FOUND. CORROSION AND SCRATCHES AROUND OF SETTLEMENT AREA WERE REPAIRED PER EA NO. CRJ953-22761 REV. IRJul 12, 2026 · N928XJ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202608210033Angle · corrodedAFT INNER SKIN WAS REMOVED, CORROSION ON INTERNAL ANGLE WAS FOUND AT PASSENGER DOOR. INTERNAL ANGLE OF PASSENGER DOOR WAS REPLACED IAW SRM 51-42-06-001-001-A01.Jul 12, 2026 · N544EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWAA2026081943397Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 241AF HAD AREAS OF EXPOSED FIBERS. REMOVED & REPLACED THE FLOOR PANEL IAW AMM 53-21-00.Jul 12, 2026 · N8706W · Boeing 7378 · Fuselage Floor PanelSDR SWAA2026081940734Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 231XF HAS AREAS OF EXPOSED FIBERS. REMOVED & REPLACED THE FLOOR PANEL 231XF IAW AMM 53-21-00.Jul 12, 2026 · N8706W · Boeing 7378 · Fuselage Floor PanelSDR ASAA2026071268097Support Beam · wornRT SUPPORT BEAM LOWER CHORD WORN BEYOND SRM LIMIT AT ECS DOOR LATCH LOCATION. MIG-5 300011971 GROUNDED - YES. REPAIRED PER SRM 57-10-13-2R-3Jul 12, 2026 · N592AS · Boeing 737890 · Wing Main, Frame StructureSDR SWAA2026081754292Angle · crackedCRACKED ANGLE, BS 380 - 400, LBL 50, PAX CABIN. REPLACED WITH A NEW ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A5400, SHT 183, REV-.Jul 12, 2026 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026081713353Angle · crackedCRACKED ANGLE BTWN BS 380 - 400, RBL 41, IN PAX CABIN. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A5400, SHT 140, REV-.Jul 12, 2026 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026081766876Angle · crackedCRACKED ANGLE, BS 380 - 400, LBL 13. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A5400, SHEET 182, SHEET 184, REV -.Jul 12, 2026 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026081709513Angle · crackedCRACKED ANGLE, BS 380 - 400, BL 0 IN THE PAX CABIN. REPLACED ANGLE & FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A5400, SHEET 154, REV- .Jul 12, 2026 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026081746886Bracket · crackedCRACKED BRACKET ON ACCESS PANEL 834DZ IN PAX CABIN. REPLACED THE BRACKET ON ACCESS PANEL 834DZ IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.Jul 12, 2026 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026081768736Web · crackedCRACKED WEB, BS 500G - 500H, STR 26R. REPLACED THE WEB & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7505, SHT 151, REV-.Jul 12, 2026 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026081751933Angle · crackedCRACKED ANGLE FLOOR STRUCTURE BTWN BS 380 - 400, RBL 10. REPLACED THE ANGLE IAW SRM 51-40-02, & SRM 51-10-02, ITEM 9, DWG 143A5400, SHT 139, REV-, & DWG 143A5400 SHT 184, REV-.Jul 12, 2026 · N8651A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR HNAA2026081400670Floor Support · corrodedCENTER FLOOR OMEGA BEAM GUSSET #5 IN MULTIPLE AREAS HAVE CORROSION. REMOVED AND REPLACED CENTER FLOOR OMEGA BEAM GUSSET #5 IAW EMB145 SRM 51-40-02.Jul 12, 2026 · N942LL · Emb EMB145LR · Fuselage Miscellaneous StructureSDR AALA202608142136Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: REMOVED INTERCOSTAL AT STATION 947 RBL 51 FOM IAW SRM 51-40-02 IN PREPARATION FOR T-CAP REPAIR SRM 53-70-51. SEE NR 89 FOR T-CAP REPLACEMENT. ALL WORK COMPLETED IAW B737-MAX8 SRM 53-70-51-2R-5 REPAIR 5 WITH MINOR DEVIATIONS AS NOTJul 12, 2026 · N306RC · Boeing 7378 · Fuselage Main, Floor BeamSDR HNAA2026081400705Rib · crackedF138593 R/H WING RIB 21 IS CRACK. ACCOMPLISHED DOUBLE REPAIR ON R/H WING RIB 21. IAW EMB 145 SRM 57-20-07RE FIGURE 203 AND EO1-57-26-0371.Jul 12, 2026 · N942LL · Emb EMB145LR · Wing, Rib/BulkheadSDR HNAA2026081400691Floor Support · corrodedLEFT FLOOR OMEGA BEAM GUSSET #7 BETWEEN FR-57 - 58 HAS CORROSION. R & R LT FLOOR OMEGA BEAM GUSSET NR 7 BETWEEN FR-57 - 58 IAW SRM 51-40-02.Jul 12, 2026 · N942LL · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026081400690Floor Support · corrodedCENTER FLOOR OMEGA BEAM GUSSET #5 IN MULTIPLE AREAS HAVE CORROSION. REMOVED AND REPLACED CENTER FLOOR OMEGA BEAM GUSSET #5 IAW EMB145 SRM 51-40-02.Jul 12, 2026 · N942LL · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026081400689Floor Support · corrodedLAV L/H FLOOR SILL HAS CORROSION AROUND NUT-PLATE HOLE. REMOVED AND REPLACED LAV L/H FLOOR SILL IAW EMB145 SRM 51-40-02.Jul 12, 2026 · N942LL · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026081400688Support Fitting · corrodedLAV FLOOR POTABLE WATER FITTING SUPPORT HAS CORROSION ON UNDERNEATH SURFACE. REMOVED AND REPLACED LAV FLOOR POTABLE WATER FITTING SUPPORT IAW EMB 145 SRM 51-40-02.Jul 12, 2026 · N942LL · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026081400674Floor Support · corrodedF139046 L/H FLOOR OMEGA BEAM GUSSET #6 IN MULTIPLE AREAS HAVE CORROSION. REMOVED AND REPLACED L/H FLOOR OMEGA BEAM GUSSET #6 IAW EMB 145 SRM 51-40-02Jul 12, 2026 · N942LL · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026081400673Floor Support · corrodedRIGHT FLOOR SILL NR 3 HAVE CORROSION IN MULTIPLE AREAS. BLENDED AREAS ON RH FLOOR SILL NR 3 IAW SRM 51-10-03 BLENDED AREAS FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-23-10AD. REMOVED AND REPLACED RT FLOOR SILL NR 3 IAW SRM 51-40-02 & 51-40-09.Jul 12, 2026 · N942LL · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026081400672Floor Support · corrodedR/H FLOOR SILL #5 HAVE CORROSION IN MULTIPLE AREAS. REMOVED AND REPLACED R/H FLOOR SILL #5 IAW EMB 145 SRM 51-40-02 AND 51-40-09.Jul 12, 2026 · N942LL · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026081400671Floor Support · corrodedLEFT FLOOR SILL #5 HAVE CORROSION IN MULTIPLE AREAS. RAR LH FLOOR SILL #5 IAW EMB 145 SRM 51-40-02Jul 12, 2026 · N942LL · Emb EMB145LR · Fuselage Miscellaneous StructureSDR AALA202608138635Slide Raft · deformedAIRCRAFT IN BASE MAINTENANCE: DURING EPAS OPERATIONAL TEST FOUND DOOR 3R SLIDE RAFT WITH DEFORMATION. SLIDE MUST BE REPLACED. MAINTENANCE ESCAPE SLIDE PACK ASSEMBLY ON DOOR R3 PER JOB CARD 72L80025005.Jul 12, 2026 · N751AN · Boeing 777223 · Escape SlideSDR SWAA2026081224942Thrust Reverser · delaminatedDELAMINATED OTBD THRUST REVERSER, AFT LOWER AREA, NR 1 ENGINE. REPAIRED THE OTBD THRUST REVERSER IAW SRM 51-70-05-2R-1, REPAIR 1.Jul 12, 2026 · N7732A · Boeing 7377BD · Engine Thrust ReverserSDR SWAA2026081253425Angle · crackedCRACKED SEAL PLATE, ACCESS PANEL 333AT ANGLE, LT HORIZONTAL STAB. REPLACED THE SEAL PLATE ANGLE IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.Jul 12, 2026 · N7732A · Boeing 7377BD · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026073025374Retainer · crackedNR 1 ENG, FWD CIRCUNFERENTIAL LATCH (ENGINE SIDE), RT ATTACHMENT BROKEN. DOT 73-022. REPLACE RETAINER ON FITTING AT NR 1 ENG, FWD CIRCUNFERENTIAL LATCH RT ENGINE SIDE IAW SRM 51-40-21. INSTALLED NR 1 ENGINE FWD CIRCUMFERENTIAL LATCH ATTACHMENT BRACKET FITTING Jul 12, 2026 · N136UP · Airbus A300F4622R · Engine Thrust ReverserSDR SWIA2026071276735Seat Track · gougedFORWARD FUSELAGE WET AREA- RT INBD SEAT TRACK SECTION 1, GOUGED BETWEEN FRAMES 20 - 21. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08. O.E.M. PART INSTALLED.Jul 12, 2026 · N146SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026080401482Window Frame · damagedDURING INSPECTION OF LT WINDSHIELD STRUCTURE FOR INSTALL OF LT WINDSHIELD, FOUND 3 ELONGATED HOLES. NO LIMITS NOTED IN SRM HOLE MEASUREMENTS ARE .372 .353 .323. COMPLIED WITH STEP 1 AND 3 IAW REO 690-53-11-2232, REV. --(P2). COMPLIED WITH ALL STEPS OF REO 690Jul 12, 2026 · N923XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR DALA2026073004398Strut · corrodedCORROSION INTERCONNECTING STRUT IB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED STRUT PER A321 AMM 27-51-44. (1695840) AIRCRAFT WAS GROUNDED.Jul 12, 2026 · N106DN · Airbus A321211 · Trailing Edge FlapsSDR AALA202607289715Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AFT CORNER SHAPE FITTING AT FR 68 AND S23R. REPLACED CORNER SHAPE FITTING PER SRM 51-42-11.Jul 12, 2026 · N9016 · Airbus A319115 · Fuselage Miscellaneous StructureSDR SIMA20260712005Seat Track · corrodedRIGHT CENTER SEAT TRACK HAS CORROSION BTWN FR 84-85 JUST AFT OF SEAT TRACK AFT END. (MAJOR REPAIR) (LEVEL 2 CORROSION). ACCOMPLISHED A PERMANENT REPAIR ON RT CENTER SEAT TRACK LOCATED BETWEEN FR84 AND FR85 JUST AFT OF SEAT TRACK AFT END AND RT INBD SEAT TRACKJul 12, 2026 · N302RN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20260712003Floor Support · corrodedRIGHT CENTER FLOOR BEAM HAS CORROSION LOCATED BETWEEN FR 90-91. (LEVEL 2 CORROSION) R & R RT CENTER FLOOR BEAM LOCATED BETWEEN FR90 AND FR91 IAW SRM 51-40-08Jul 12, 2026 · N302RN · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SIMA20260712004Shear Panel · corrodedSSI 53-23-005 RH SHEAR PANEL LOCATED BETWEEN FR 87-88 IS CORRODED. (LEVEL 2 CORROSION) RAR RH SHEAR PANEL LOCATED BETWEEN FR87 AND FR88 IAW ERJ 175 SRM 51-40-08Jul 12, 2026 · N302RN · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SIMA20260712002Floor Support · corrodedSSI 53-23-005 RH CENTER FLOOR BEAM HAS CORROSION LOCATED BETWEEN FR 89-90, (LEVEL 2 CORROSION) RAR RH CENTER FLOOR BEAM AT FR89-90 IAW ERJ175 SRM 51-40-08Jul 12, 2026 · N302RN · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR DALA2026072304313Skin · missingLEFT INBD FLAP MISSING LOWER SKIN, JUST OTBD OF INBOARD FLAP FAIRING MEASURING, 31IN BY 13 IN FLAP. R & R T/E WEDGE PANEL (SSE 664006) IAW AMM 27-51. ACFT OK FOR SVC. (8402931) AIRCRAFT WAS GROUNDED.Jul 12, 2026 · N963DZ · Boeing 7379GPER · Trailing Edge FlapsSDR SWAA2026072207566Plate · crackedRIGHT WING LOWER INBD FIXED TRAILING EDGE PANEL 651GB AREA WIGGLE PLATE CRACKED. R & R RT WING LOWER INBORD FIXED TRAILING EDGE PANEL 651 GB WINGGLE PLATE IAW SRM 51-40-02-0G-0, AND DWG -115A2001, REV-.Jul 12, 2026 · N7847A · Boeing 737752 · Wing Main, Frame StructureSDR SWAA2026071670216Girt Bar · stuckFWD SERVICE DOOR GIRT BAR RETAINER OUT OF PLACE AND STUCK. SECURED GIRT BAR RELEASE STOP ASSEMBLY ON FWD SERVICE DOOR PER AMM 25-66-01. OPS CK NML.Jul 12, 2026 · N910WN · Boeing 7377H4 · Emergency EquipmentSDR CALA2026072217942Beam · crackedPERFORM AN INSPECTION OF THE REPAIRS ON THE FORWARD CARGO DOOR UPPER FRAME AND BEAM IAW THE PART TWO OF THE LATEST REVISION OF ECRA 5230-02326INITIATED A DIP TO INSPECT REPAIRS ON THE FORWARD CARGO DOOR UPPER FRAME AND BEAM. INTERIM REPAIR ACCOMPLISH ON THE Jul 12, 2026 · N37521 · Boeing 7379 · Fuselage Main, StructureSDR CALA2026072217940Door Frame · crackedCONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS ON THE FORWARD CARGO DOOR UPPER FRAME AND BEAM REPAIRS IAW PART TWO OF THE LATEST REVISION OF ECRA 5230-02326INITIATED A DIP TO HAVE PLANNING CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS ON THE FORWARDJul 12, 2026 · N37521 · Boeing 7379 · Fuselage Main, Structure