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 IXXA2026020601Skin · damagedDURING REPAIR ON NR 187303-0100-0192 IT WAS DISCOVERED THAT THERE IS A SCRIBE JUST FWD OF THE REPAIR AREA AT STA 740 STR 19L COMMON TO THE SKIN LAP.Feb 6, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR CALA2026092319699Bulkhead Web · crackedFOUND SMALL CRACK AT PANEL P-18 BULKHEAD AFT FACE WEB S13L BS 259.5. PERFORMED A REPAIR AT P-18 BULKHEAD AFT FACE WEB PANEL BETWEEN S-11L TO S-13L STA 259.5 IAW SRM 51-40-02-0G-0, AND ESR-WI 95-14588.Feb 5, 2026 · N35236 · Boeing 737824 · Fuselage Main, BulkheadSDR SWIA2026020576882Skin · dentedDENT 28.5" FROM RT WING IBD FLAP OTBD EDGE & 5.75" FROM TE ON UPPER SKIN. DENT FOUND TO BE 1.2" X 1" AT A DEPTH OF 0.028". REPAIRED THE RT WING INBD FLAP OTBD EDGE AND 5.75 FROM TE ON UPPER SKIN IAW REO 601R-57-52-2555, REV--. APPLIED SURFACE FINISH IAW SFeb 5, 2026 · N207PS · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2026080301389Angle · crackedCRACK ON LH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER LH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER WERE REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01Feb 5, 2026 · N398CA · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous StructureSDR REXA2026080301384Landing · cracked"CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS MANUFACTURED PER EA NO: CRJ953-21561 REV IR, DWG CC670-33151-6 REV ""D"", AND REPLACED PER CRJ 900 SRM 51-42-0Feb 5, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR DALA2026071504167Stringer · damagedSTRINGER 1L, FR 60 TO FR 64, TOOLING DAMAGE. COMPLIED WITH ERA 631889-14. (1437525) AIRCRAFT WAS GROUNDED.Feb 5, 2026 · N861NW · Airbus A330223 · Fuselage Main, Longeron/StringerSDR SWIA2026020576088Frame · fomREMOVE AND SPLICE FRAME AT FS319 FROM STR25R AND STR25L TO FOM. (C-CHECK RO 05/22/2026)REMOVED AND SPLICED FRAME FS319 FROM STR25R AND STR25L, REF CRJ900 SRM 53-00-06-201-006-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY AND FORM M-337. SEE CONTIFeb 5, 2026 · N899SK · Cndair CL6002D24 · Standard Practices/StructuresSDR SWIA2026020576049Stringer · corrodedCORROSION FOUND ON STRINGER 25R, BS 280 - 333. REPLACED STRINGER 25R FS280 - FS333 REF. DWG SH670-31630 REV: K AND SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS.Feb 5, 2026 · N899SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR VNAA20260511010Door Frame · corrodedCOCKPIT DOOR POST IS CORRODED AT RBL 11 W.L.72.5. REPAIRED RBL 11 COCKPIT DOOR POST IAW BOMBARDIER GREO 670-53-11-745 REV -A DATED 2016-10-28.Feb 5, 2026 · N512AE · Cndair CL6002C10 · Fuselage Main, StructureSDR AALA202604287088Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND LOCATED ON UPPER TENSION BOLT, WINDSHIELD CENTER POST LH SIDE. CRACK DIRECTION: 1 OCLOCK (VIEW ON LH SIDE), CRACK LEN GHT= 0.200 INCH APPROX, AD-2020-17-03. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INSTFeb 5, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202604284966Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND LOCATED ON UPPER TENSION BOLT, WINDSHIELD CENTER POST LH SIDE. CRACK DIRECTION: 1 OCLOCK (VIEW ON LH SIDE), CRACK LEN GHT= 0.200 INCH APPROX, AD-2020-17-03. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INSFeb 5, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR SWIA2026020575870Intercostal · corrodedPAX DOOR DD4 MID INTERCOSTAL IS CORRODED. REMOVED AND INSTALLED NEW PASSENGER DOOR DD4 MID INTERCOSTAL. IAW SRM 51-42-06-00 AND SRM 51-42-21. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026020575867Frame · corrodedPAX DOOR FS320.163 FRAME BETWEEN DD5 INTERCOSTAL AND LOWER CHANNEL IS CORRODED. INSTALLED NEW PAX DOOR FS320.163 FRAME . IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKYFeb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026020575860Intercostal · corrodedPAX DOOR DD1A MID INTERCOSTAL IS CORRODED. INSTALLED NEW PAX DOOR DD1A MID INTERCOSTAL. IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026020575856Cleat · corrodedPAX DOOR DD5 FS347.25 CLEAT IS CORRODED. INSTALLED NEW PAX FS347.25 DD5 CLEAT. IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026020575853Intercostal · corrodedPAX DOOR DD3 MID INTERCOSTAL IS CORRODED. INSTALLED NEW PASSENGER DOOR DD3 MID INTERCOSTAL IAW SRM 51-42-06-00 AND SRM 51-42-21-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026020575850Intercostal · corrodedPAX DOOR DD1A AFT INTERCOSTAL IS CORRODED. INSTALLED NEW PAX DOOR AFT INTERCOSTAL DD1A . IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKYFeb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026020575847Cleat · corrodedPAX DOOR DD7 FS347.25 CLEAT IS CORRODED. INSTALLED NEW PAX FS347.25 DD7 CLEAT. IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026020575839Intercostal · corrodedPAX DOOR DD2 MID INTERCOSTAL IS CORRODED. INSTALLED NEW PASSENGER DOOR DD2 MID INTERCOSTAL. IAW SRM 51-42-06-00 AND CRJ200 SRM 51-42-21-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026020575838Cleat · corrodedPAX DOOR DD7A FS327.763 CLEAT IS CORRODED. PAX DOOR FS327.763 DD7A 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 52-00-00 PERFORMED LOCATE AND DRILL NEW PASSENGER DOOR FS327.7Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026020575836Retainer · corrodedPAX DOOR FWD LOWER CORNER SEAL RETAINER IS CORRODED. INSTALLED NEW PASSENGER DOOR LOWER FWD CORNER SEAL RETAINER. IAW SRM 51-42-06-00 AND DWG 601R31871 REV D. COMPLIED WITH TASK CARD 51-900-1003-SKY.Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026020575833Intercostal · corrodedPAX DOOR DD1 MID INTERCOSTAL IS CORRODED. INSTALLED NEW PAX DOOR DD1 MID INTERCOSTAL. IAW SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.Feb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026020575830Cleat · corrodedPAX DOOR DD1A FS338.963 INBD CLEAT IS CORRODED. PAX DOOR DD1A FS338.963 INBD CLEAT, ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00 CORROSION ON MORE THAN ONE ELEMENT AT A GIVEN CROSS-SECTION, PAX DOOR DD1A FS338.963 INBD CLEAT IS OUT OF LIMITS, IAWFeb 5, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026020575829Channel · corroded(MX 31663791) PAX DOOR FS327.763 FRAME BETWEEN DD6 INTERCOSTAL AND LOWER CHANNEL IS CORRODED. (C-CHECK RO 04/19/2026)INSTALLED NEW PAX DOOR FS327.763 FRAME. IAW. CRJ200 SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.Feb 5, 2026 · N959SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026020575712Skin · dentedDENT ON BOTTOM SIDE OF LT INBOARD FLAP INBOARD SIDE. REPAIRED LT INBD FLAP BOTTOM INDB SIDE DENT IAW CRJ 200 SRM 57-52-00-02 REPAIR 3 COMPLETED TASK CARD 51-900-1003-SKY.Feb 5, 2026 · N915EV · Cndair CL6002B19 · Trailing Edge FlapsSDR VNAA2026041500009Skin · damagedPERM REPAIR BEFORE 49,272.65 FH - LH IB SLAT WITHIN 6474.88 FHS FROM IR (BEFORE 49,272.65 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. DURING VISUAL INSPECTION OF IB SLAT EDGE OF PREVIOUS TEMP REPAIR REF: EA 23-C7-57-00Feb 5, 2026 · N521AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA2026041500001Bracket · crackedAFT BAGGAGE BAY DOOR INTERNAL HARNESS BRACKET IS CRACKED.Feb 5, 2026 · N521AE · Cndair CL6002C10 · Cargo/Baggage DoorsSDR REXA2026032700274Landing · crackedCRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS MANUFACTURED PER EA NO: CRJ953-21561 REV IR, DWG CC670-33151-6 REV ""D"", AND REPLACED PER CRJ 900 SRM 51-42-06Feb 5, 2026 · N918XJ · Cndair CL6002D24 · Service DoorsSDR REXA2026032700260Support · crackedCRACKED INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE WAS REPLACED PER CRJ900 SRM 51-41-10-001-001-A01 AND SRM 51-42-06-001-001-A01Feb 5, 2026 · N918XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR AALA202603209599Bellcrank · out of adjustAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 TORSION BAR BELL-CRANK OF THE COMPENSATION MECHANISM IS OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED PASSENGER / CREW DOOR 832 TORSION BAR BELL-CRANK OF THE COMPENSATION MECHANISM PER AMM 52-10-00.Feb 5, 2026 · N9006 · Airbus A319115 · Passenger/Crew DoorsSDR SWAA2026031368021Web · crackedCRACKED WEB, BS 312 - 328, LBL 47.5, WL 208.1. REPLACED THE WEB IAW SRM 51-40-02-0G-0, & DWG 141A5400, SHEET 26, REV-.Feb 5, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031368022Floor Support · crackedCRACKED FLOOR SUPPORT, BS 344 - 360, BL 0, WL 208.1. REPLACED INTERCOSTAL AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 141A5400, SHEET 32, REV -.Feb 5, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031368195Angle · crackedCRACKED ANGLE, BS 500H, STR 26R. REPLACED THE ANGLE, IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7505, SHEET 137, & 138, REV-.Feb 5, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031368196Angle · crackedCRACKED ANGLE, BS 500H, STR 26R. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7505, SHEET 137, & 138, REV - .Feb 5, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031368198Angle · crackedCRACKED ANGLE, BS 500G, STR 26R. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-10-02, & DWG 143A7505, SHEET 137, REV-.Feb 5, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031368199Angle · crackedCRACKED ANGLE, BS 500G, STR 26R. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7505, SHEET 137, & 138, REV - .Feb 5, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031368201Angle · crackedCRACKED ANGLE, BS 500H, STR 26L. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7505, SHEET 137, & 138, REV -.Feb 5, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031368202Angle · crackedCRACKED ANGLE, BS 500H, STR 26L. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 143A7505, SHEET 137, REV-.Feb 5, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031368204Angle · crackedCRACKED ANGLE, BS 400, STR 26L. REPLACED THE ANGLE IAW SRM 51-40-02-0G, & DWG 143A7505, SHEET 137, REV-.Feb 5, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031368200Angle · crackedCRACKED GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 21L IN THE FWD CARGO COMPARTMENT. REPLACED THE GUSSET ANGLE AND FASTENERS LOCATED IAW SRM 51-40-02, AND DWG 143A7902, SHEET 256, REV B.Feb 5, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031368197Support Angle · crackedCRACK GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 19R IN THE FWD CARGO BAY. INSTALLED A NEW GUSSET SUPPORT AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 143A7902, SHEET 257, REV B.Feb 5, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031368027Support · crackedCRACK INNER CHORD LOCATED BS 303.9 LBL 55 WL 208.1 AT FWD GALLEY AND LAV. REPLACED INNER CHORD & FASTENERS AT FORWARD GALLEY AREA BETWEEN BS 270 - 360, STR 17L, WL 208.1, & LBL 55 IAW SRM 51-40-02-0G-0, DWG 141A8110, SHEET 9, REV A, DWG 140A9810, SHEET 53, Feb 5, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031268203Angle · crackedCRACKED ANGLE, BS 500G, STRINGER 26L IN THE FWD CARGO BAY. REPLACED ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 143A7505, SHEET 137, REV-.Feb 5, 2026 · N8629A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026031168018Shield · corrodedCORRODED FWD CARGO FWD SHIELD, BS 420+1 - 420+19, RBL 22, WL 156 HAD MULTIPLE AREAS AROUND NUT PLATE HOLES. REMOVED AND REPLACED THE SHIELD IAW SRM 51-40-02, & DWG 143A0080, REV-Feb 5, 2026 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026031170227Mount · corrodedNR 2 ENGINE AFT MOUNT HAS EVIDENCE OF FRETTING ON THE OUTBOARD LINK AT TRF ATTACHMENT. REMOVED AND INSTALLED NEW AFT ENGINE MOUNT IAW MT 771-021-00-03.Feb 5, 2026 · N8525S · Boeing 7378H4 · Engine Mount SectionSDR SWAA2026031068180Scuff Plate · crackedFWD SERVICE DOOR SCUFF PLATE CRACKED ON THE AFT EDGE. REMOVED THE COATINGS AND UNWANTED MATERIALS FROM THE SCUFF PLATE BEFORE WELDING IAW SRM 53-10-15-2R-2, STEP 4.B.(3). WELDED THE DAMAGED AREA OF SCUFF PLATE IAW SRM 53-10-15-2R-2, STEP 4.B.(4). THE SCUFFFeb 5, 2026 · N246LV · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026030968011Door Frame · crackedCRACKED DOOR FRAME, BS 312, STR 5L - STR 6L. PERFORMED A REPAIR ON THE DOOR FRAME IAW EA NM-22-153-01244, REV B.Feb 5, 2026 · N8628A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2026030968012Angle · crackedCRACKED ANGLE, BS 500I, LBL 7. REPLACED THE ANGLE IAW SRM 51-40-02-0G, & DWG 143A7902, SHEET 320, REV -.Feb 5, 2026 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026030968013Angle · crackedCRACKED ANGLE, DOOR CUT OUT, BS 309, STR 8L. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 141A8220, SHEET 21, REV A.Feb 5, 2026 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026030968014Angle · crackedCRACKED ANGLE, BS 500I, RBL 7. REPLACED THE ANGLE IAW SRM 51-40-02-0G, & DRAWING 143A7902, SHEET 320, REV -.Feb 5, 2026 · N8628A · Boeing 7378H4 · Fuselage Miscellaneous Structure