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 SWIA2026051876877Drag Angle · crackedVERT STAB LH AFT DRAG ANGLE IS CRACKED (C-CHECK RO 08/17/2026)PERFORMED REPAIR AT VERT STAB LH AFT DRAG ANGLE IAW BOMBARDIER REO 670-55-31-018, REV -A, DATE: 2016-11-10.May 18, 2026 · N796SK · Cndair CL6002C11 · Fuselage, Stabilizer Attach FittingsSDR SWIA2026051876876Drag Angle · crackedVERT STAB RH AFT DRAG ANGLE IS CRACKED (C-CHECK RO 08/17/2026)PERFORMED REPAIR AFT DRAG ANGLE AT RH VERT STAB IAW BOMBARDIER REO 670-55-31-018 DATE: 2016-11-10, CRJ550 SRM 51-26-01, NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S072326-2 DATE INSMay 18, 2026 · N796SK · Cndair CL6002C11 · Fuselage, Stabilizer Attach FittingsSDR VNAA202607300009Skin · corrodedSEVERAL CORROSION ON INTERNAL FUSELAGE SKIN BTW VERTICAL STAB 55.625% TO VERTICAL STAB 67.5% AND BTW STR 22L TO STR 22R THROUGH ACCESS PANEL 362AR. CORROSION ON INTERNAL FUSELAGE SKIN BTW VERTICAL STAB 55.625% TO VERTICAL STAB 67.5% & BTW STR 22L TO STR 22R TMay 18, 2026 · N644NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202607300008Skin · corrodedSEVERAL CORROSION ON INTERNAL FUSELAGE SKIN BTW VERTICAL STAB 55.625% TO VERTICAL STAB 67.5% AND BTW STR 22L - STR 22R THROUGH ACCESS PANEL 362AR. CORROSION ON INTERNAL FUSELAGE SKIN BTW VERTICAL STAB 55.625% TO VERTICAL STAB 67.5% AND BTW STR 22L TO STR 22R May 18, 2026 · N644NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202607300007Angle · corrodedSEVERAL CORROSION ON INTERNAL FUSELAJE SKIN BTW VERTICAL STABILIZER 55.625% TO VERTICAL STABILIZER67.5% AND BTW SGTR 22L TO SGTR 22R THROUTHG ACCES PANEL 362AR. CORROSION ON INTERNAL FUSELAJE SKIN BTW VERTICAL STAB 55.625% TO VERTICAL STAB 67.5% AND BTW STR 2May 18, 2026 · N644NN · Cndair CL6002D24 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026061504197Attach Angle · crackedRIGHT BS 663, A CRACK FOUND ON VAPOR BARRIER UPPER ATTACH ANGLE AT RBL 25, WL 167.68. REMOVED DAMAGE AND REPAIRED IAW SRM 57-10-10-2R-5.May 18, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026061504198Attach Angle · crackedLEFT BS 663, CRACK FOUND ON VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 25, WL 167.68. REMOVED DAMAGE AND REPAIRED IAW SRM 57-10-10-2R-5.May 18, 2026 · N925WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR 2026FA0000582Pitot Tube · blockedWHILE OPERATING IN THE CLOUDS AT 28,000 FEET MSL IN THE VICINITY OF CONVECTIVE WEATHER (TAT -3) THE AIRCRAFT EXPERIENCED 3 VERY BRIEF ERRATIC AIRSPEED ENCOUNTERS EFFECTING BOTH THE NR 1 & 2 AIRSPEED INDICATION SYSTEMS. THE NR 3 (STANDBY) SYSTEM WAS NOT OBSERVMay 18, 2026 · N571CH · Gulstm G280 · Pitot/Static SystemSDR SWIA2026051876427Intercostal · corrodedCLIP INTERCOSTAL DD7 IS CORRODED. REMOVED PASSENGER DOOR CLIP INTERCOSTAL DD7 IAW SRM 51-42-06-001-001-A01 & INSTALLED PASSENGER DOOR CLIP INTERCOSTAL DD7 REF SRM 51-42-06-001-001-A01 REV 38, & DWG 601R31702, REV -N. & COMPLIED WITH SKYWEST TASK CARD 51-900-May 18, 2026 · N770SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026051876419Door Frame · corrodedFRAME, FS313.56, DD4 AND DD5 IS CORRODED. REMOVED AND REPLACED CORRODED FRAME AT FS313.56 WITH NEW PASSENGER DOOR FRAME AT FS313.56 USING NEW FASTENERS, REF. SRM 51-42-06-001-001-A01 REV 38 AND BOMBARDIER DWG 601R31702 REV -N. SEE CONITNUATION STEPS FOR MORE May 18, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2026051876403Door Frame · corrodedCLEAT COMMON FRAME BS 338.963 IS CORRODED. REMOVED PASSENGER DOOR CLEAT COMMON FRAME BS 338.963 IAW SRM 51-42-06-001-001-A01 & INSTALLED NEW PASSENGER DOOR CLEAT COMMON FRAME BS 338.963 IAW SRM 51-42-06-001-001-A01 REV 38, AND DWG 601R31702 REV -N, & COMPLMay 18, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2026051876402Angle · corrodedCLIP INTERCOSTAL DD6 IS CORRODED. REMOVED PASSENGER DOOR CLIP INTERCOSTAL DD6 REF. SRM 51-42-06-001-001-A01 & INSTALLED NEW PASSENGER DOOR CLIP INTERCOSTAL DD6 REF. SRM 51-42-06-001-001-A01 REV 38 AND DWG 601R31702 REV -N. & COMPLIED WITH SKYWEST TASK CARD May 18, 2026 · N770SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026051876399Cleat · corrodedCLEAT COMMON INTERCOSTAL DD6 IS CORRODED. REMOVED AND REPLACED WITH 1 EA OF NEW CLEAT COMMON INTERCOSTAL DD6 REF. SRM 51-42-06-001-001-A01.May 18, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA2026051876384Intercostal · corrodedINTERCOSTAL, DD4 IS CORRODED MX#32277118 (C-CHECK RO 07/01/2026)REMOVED AND REPLACED CORRODED INTERCOSTAL AT DD4 WITH NEW PASSENGER DOOR INTERCOSTAL DD4 USING ALL NEW FASTENERS, REF. CRJ700 SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020 AND BOMBARDIER DWG 60May 18, 2026 · N770SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026051876381Intercostal · corrodedPASSENGER DOOR INTERCOSTAL COMMON WITH FORMER BS 347.25 CORRODED. REMOVED AND INSTALLED NEW PASSENGER DOOR AFT DD4 INTERCOSTAL COMMON WITH FORMER BS 347.25 IAW SRM 51-42-06-001-001-A01 REV 38, AND DWG 601R31702 REV -N.May 18, 2026 · N770SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026070276372Intercostal · corrodedCLIP INTERCOSTAL COMMON INTERCOSTAL AND FORMER 347.25 IS CORRODED. REMOVED PASSENGER DOOR CLIP INTERCOSTAL COMMON INTERCOSTAL AND FORMER BS 347.25 IAW SRM 51-42-06-001-001-A01 & INSTALLED NEW PASSENGER DOOR CLIP INTERCOSTAL COMMON INTERCOSTAL AND FORMER BS 34May 18, 2026 · N770SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2026051876367Intercostal · corrodedPASSENGER DOOR INTERCOSTAL, DD2 IS CORRODED. REMOVED AND REPLACED CORRODED INTERCOSTAL AT DD2 WITH NEW NEW PASSENGER DOOR INTERCOSTAL AT DD2 USING NEW FASTENERS, REF. SRM 51-42-06-001-001-A01 REV 38 AND DWG 601R31702 REV -N. SEE CONTINUATION STEPS FOR MORE DMay 18, 2026 · N770SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWAA2026063004259Seat Track · corrodedCORROSION IN WELL ON PASSENGER CABIN SEAT TRACKS AT BS 480+15- BS 500+8, BS 500A+6 - BS 500A+18, BS 500D+8 - BS 500D+19. ON CROWN BS 500A+18 AT LBL 25 WL 208. SEAT TRACK FOUND TO BE OUT OF LIMITS, & WILL BE REPLACED ON TASK CARD TTG8Q01C933B.May 18, 2026 · N929WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026063004261Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACKS IN WELL AT BS 480+14 - BS 480+19, BS 500A+4 - BS 500A+16, BS 500D+9 - BS 500D+13. ON CROWN BS 480+8 - BS 480+13, LBL 45, WL 208. THE SEAT TRACK FOUND TO BE OUT OF LIMITS; WILL BE REPLACED ON TASK CARD TTG8Q01C9N0.May 18, 2026 · N929WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR AALA202606288625Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.May 18, 2026 · N152UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR AALA202606248095Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT RIGHT DOOR AFT HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER CMM 52-82-32.May 18, 2026 · N104NN · Airbus A321231 · Fuselage, Door HingeSDR AALA202606247676Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT LEFT DOOR AFT HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER CMM 52-82-32.May 18, 2026 · N104NN · Airbus A321231 · Fuselage, Door HingeSDR AALA202606247736Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT LEFT DOOR FORWARD HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER CMM 52-82-32.May 18, 2026 · N104NN · Airbus A321231 · Fuselage, Door HingeSDR AALA202606249592Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR AFT RIGHT DOOR FORWARD HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER CMM 52-82-32.May 18, 2026 · N104NN · Airbus A321231 · Fuselage, Door HingeSDR SWAA2026062204121Floorbeam · corrodedCORROSION ON BS 947 FLOORBEAM UPPER FLANGE, LBL 49 AND LBL 53, WL 208. PERFORMED REPAIR ON THE FLOORBEAM IAW SRM 53-70-51-2R-5, REPAIR 5.May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2026062204124Floorbeam · corrodedCORROSION ON BS 986.5 FLOORBEAM UPPER FLANGE AT NUTPLATE HOLE LBL 43, WL 208. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6, FIG 205.May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Main, Floor BeamSDR SWAA2026062204122Support Angle · corrodedCORROSION ON RT ZEE SUPPORT ANGLE AT BS 986.5+6, RBL 37, WL 208. REMOVED AND REPLACED RT ZEE SUPPORT ANGLE AT BS 986.5, RBL 37, WL 208 IAW SRM 51-40-02-0G-0, AND DWG 147A5700, REV A.May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026062204270Support Angle · corrodedCORROSION ON RT ZEE SUPPORT ANGLE AT BS 986.5+6, RBL 32, WL 208. REMOVED AND REPLACED RT ZEE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 147A5700, REV A.May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026062204271Sill Drain · corrodedCORROSION ON ASD MOP SILL AT BS 947+8, RBL 56, WL 208. REMOVED & INSTALLED NEW AFT SERVICE DOOR MOP SILL FROM 887+10 -1006 IAW SRM 51-40-02; DWG 147A8501 REV:A,; & DWG 147A0000 REV A.May 18, 2026 · N8646B · Boeing 7378H4 · Emergency ExitsSDR SWAA2026062204268Support Strap · corrodedCORROSION ON SHEAR WEB SUPPORT STRAP AT BS 1016+3, RBL 3, WL 208. REMOVED AND REPLACED SHEAR WEB SUPPORT STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5700, REV A.May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026062204272Support Strap · corrodedCORROSION ON SHEAR WEB SUPPORT STRAP AT BS 1016+3 AND 1016+12, LBL 3, WL 208. REMOVED AND REPLACED THE SHEAR WEB STRAP IAW SRM 51-40-02-0G-0, AND DWG 147A5700, REV A.May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026062204281Support Bracket · crackedLOWER BULKHEAD SUPPORT BRACKET AT BS 867, LBL 3, WL 156 CRACKED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02-0G-0.May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026062204273Support Bracket · crackedACB FWD BULKHEAD SUPPORT BRACKET AT BS 731, BL 0, WL 160 IS CRACKED. REMOVED AND REPLACED ACB FWD BULKHEAD BRACKET ASSY IAW SRM 51-40-02 AND DWG 144A2600, REV -.May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026062204297Access Panel · debondedACCESS PANEL 191FL L/E IS DISBONDED. REPAIRED DISBONDED L/E ON ACCESS PANEL 191FL IAW SRM 53-30-70-2R-1 AND SRM 51-70-05-2R-6.May 18, 2026 · N8646B · Boeing 7378H4 · Aerodynamic FairingsSDR SWAA2026062204269Support Angle · corrodedCORROSION ON LT ZEE SUPPORT ANGLE AT BS 986.5+6, LBL 37, WL 208. REMOVED AND REPLACED RT ZEE SUPPORT ANGLE BS 986.5+6, LBL 37, WL 208 IAW SRM 51-40-02, SRM 51-40-02-0G-0, AND DWG 147A5700, REV A;May 18, 2026 · N8646B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWIA2026051876269Door Sill · corrodedGALLEY SERVICE DOOR LOWER SILL IS CORRODED JUST FORWARD OF THE FORWARD DOOR FITTING. REPLACED ANGLE LOWER SILL REF DWG SH670-31950 REV Y & SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKYMay 18, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, StructureSDR SWAA2026061804099Floor Panel · delaminatedDELAMINATED FLOOR PANEL 241EF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 241EF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL.May 18, 2026 · N500WR · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026061804100Floor Panel · delaminatedDELAMINATED FLOOR PANEL 241KF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 241KF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL.May 18, 2026 · N500WR · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026061804101Floor Panel · delaminatedDELAMINATED FLOOR PANEL 242HF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 242HF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL.May 18, 2026 · N500WR · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026061804094Support Angle · crackedCRACKED SUPPORT ANGLE, BS 867, S26L IN THE AFT CARGO BAY. REPLACED THE SUPPORT ANGLE LOCATED BS 867 AND S-26L AFT CARGO COMPARTMENT IAW SRM 51-10-02; SRM 51-40-02 AND DWG 149A8102 SHEET 19 REV A.May 18, 2026 · N500WR · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061808029Floor Panel · delaminatedDELAMINATED ACCESS PANEL 232 RF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 232RF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL.May 18, 2026 · N500WR · Boeing 7378H4 · Fuselage Floor PanelSDR SWAA2026061804204Support Bracket · crackedCRACKED SUPPORT BRACKET ON ACCESS PANEL 834DZ ON THE AFT ENTRY DOOR. REPLACED SUPPORT BRACKET LOCATED ON ACCESS PANEL 834DZ AT AFT ENTRY DOOR IAW SRM 51-10-02-0G ITEM 9, SRM 51-40-02-0G, AND DWG 411A2119, SHEET 72, REV -. EVALUATED CRACK ON SUPPORT BRACKET AMay 18, 2026 · N500WR · Boeing 7378H4 · Passenger/Crew DoorsSDR SWAA2026061804096Rib · crackedCRACKED LEADING EDGE RIB ACCESS PANEL 331B LE STA 105.26 AT LT HORIZONTAL STABILIZER. REPLACED RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 186A1001 SHEET 19 REV -.May 18, 2026 · N500WR · Boeing 7378H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2026061804095Rib · crackedCRACKED LEADING EDGE RIB ACCESS PANEL 331B LE STA 114.55 AT LT HORIZONTAL STABILIZER. REPLACED RIB LOCATED LE STA 114.55 AT LT HORIZONTAL STABILIZER IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 186A1001 SHEET 19 REV-.May 18, 2026 · N500WR · Boeing 7378H4 · Horizontal Stabilizer, Spar/RibSDR HNAA2026061700544Floor Support · corroded00619 MID OMEGA BEAM FR 24 TO 25 AREA FOUND TO BE OUT OF LIMITS REQUIRES REPAIR. REPAIRED OUT OF LIMITS CORROSION ON MID OMEGA BEAM AT FR 24 TO FR 25 WITH A DOUBLER IAW EMB 145 SRM 53-22-10-RE SECTION 4 SEE PIEDMONT MAJOR EO1-53-26-0251May 18, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SWIA2026051876229Stringer · crackedCENTER FUSELAGE III, STRINGER 9L CRACKED ON MOST AFT EDGE AT FR 90. (BEHIND WASTE TANK) REMOVED AND REPLACED CENTER FUSELAGE III, LT STRINGER 9A AT FR 90 IAW SRM 51-40-08. WEIGHT AND BALANCE NOT AFFECTED BY REPAIR, NO FURTHER ACTION REQUIRED.May 18, 2026 · N141SY · Emb ERJ170200LR · Fuselage Main, Longeron/StringerSDR AALA202606169775Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.May 18, 2026 · N152UW · Airbus A321211 · Fuselage Miscellaneous StructureSDR ASAA2026051866731Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN IS CRACKED TWO LOCATIONS INBD OF RIB 7. GROUNDED - YES. REPAIRED LT HORIZONTAL STAB LOWER SKIN AT TWO LOCATIONS IB OF RIB 7 IAW SRM 55-10-01-2R-11 STEP 4A-R THIS REPAIR HAVE SUPPLEMENTAL INSPECTION REQUIREMENTS INSPECTION THRESHMay 18, 2026 · N548AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR AALA202606157958Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM-SEAT TRACK AT FR 66 AND -Y765. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.May 18, 2026 · N152UW · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202606136211Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOORBEAM AT FR 67 AND -Y765, REPLACED FLOORBEAM IAW SRM 51-42-11.May 18, 2026 · N152UW · Airbus A321211 · Fuselage Main, Floor Beam