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 DALA2026051603027Fairing · damagedDIV - DUE TO LOUD POPPING NOISE FROM THE LEFT OVERWING EMERGENCY EXIT DOOR. NO PRESSURIZATION ISSUES REPORTED. UPPER WING TO BODY FAIRING PANEL 191DT WAS FOUND DAMAGED WITH LARGE CHUNKS MISSING, BUT NOT A TOTAL PANEL LOSS. : MAINTENANCE IN PROGRESS. (LP: 86488May 15, 2026 · N366NW · Airbus A320212 · Aerodynamic FairingsSDR DALA2026051603025Sensor · faultedDECLARED EMERGENCY DUE TO A NOSE WHEEL STEERING FAULT DURING APPROACH. AIRCRAFT TOWED TO THE GATE. REPLACED NWS FEEDBACK SENSOR 3GC AND ADJUSTED OUT OF RANGE NWS SENSOR 4GC. (LP: 8934419). AIRCRAFT WAS GROUNDEDMay 15, 2026 · N301NB · Airbus A319114 · Landing Gear Steering SystemSDR F3LA202605160413Power Supply · faultedDURING HEAVY CHECK EPSU TEST FOUND AFT EPSU (13WL) FAULTING FOR INTERIOR AND EXTERIOR LIGHTS. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED R4 DOOR SLIDE IAW AMM 25-62-44-400-803-A. OPS TEST GOOD. RE-TESTED EPSU BATTERY TEST IAW AMM 33-51-38-400-002-A. OPS TESMay 15, 2026 · N373FR · Airbus A320251N · Emergency LightingSDR ABXA20260515201Warning Light · illuminatedMAIN DECK CARGO FIRE PANEL POSITION A2 HAS FAULT LIGHT ILLUMINATED. MTX GROUNDED A/C MTX C/W AFOLTS TEST IAW B767 AMM 26-10-00 OPS CHECK GOOD NO MSG AT THIS TIME. AND RETURNED A/C TO SERVICE.May 15, 2026 · N227CY · Boeing 767316 · Smoke DetectionSDR ABXA20260515163Skin · ground damageDURING LINE OPS IN CVG, A GROUND CREW TOWED STAIRS UNDER THE RIGHT WING AND SCRAPED THE ENTIRE LOWER WING SKIN FROM FRONT SPAR TO REAR SPAR AT APPROXIMATELY WS 962. THE AIRCRAFT WAS MOVED TO A HANGAR AND IS CURRENTLY IN A-CHK IN CVG. BOEING WAS CONTACTED FOR AMay 15, 2026 · N362CM · Boeing 767338 · Wing, Plate/SkinSDR DALA2026051603021Power Supply · failedDURING EMERGENCY BATTERY PACK REPLACEMENT WORKCARD # FOUND EPSU L3 BAD. REPLACED 3L EPSU ASSY REF A321 AMM 33-51. (LP 8237573 - AIRCRAFT WAS GROUNDED)May 15, 2026 · N124DX · Airbus A321211 · Emergency LightingSDR FDEA202605150611Floor Panel · puncturedFOUR PUNCTURES ON FLOOR PANEL 231VFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 231VFF ON MAIN CARGO COMPARTMENT. WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025May 15, 2026 · N289FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202605150610Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 252RFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 252RFF ON MAIN CARGO COMPARTMENT. WAS REPAIRED IAW SRM 57-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025May 15, 2026 · N289FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202605150609Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 242TFA ON MAIN CARGO COMPARTMENT. FLOOR PANEL 242TFA ON MAIN CARGO COMPARTMENT. WAS REPAIRED IAW SRM 57-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025May 15, 2026 · N289FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202605150608Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 232NFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 232 NFF ON MAIN CARGO COMPARTMENT. WAS REPAIRED IAW SRM 57-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025May 15, 2026 · N289FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202605150607Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 241AFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 241AFF ON MAIN CARGO COMPARTMENT. WAS REPAIRED IAW SRM 57-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025May 15, 2026 · N289FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202605150606Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 241AFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 241AFF ON MAIN CARGO COMPARTMENT. WAS REPAIRED IAW SRM 57-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025May 15, 2026 · N289FE · Boeing 767300 · Fuselage Floor PanelSDR FDEA202605150605Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 241WFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 241 WFF ON MAIN CARGO COMPARTMENT. WAS REPAIRED IAW SRM 57-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025May 15, 2026 · N289FE · Boeing 767300 · Fuselage Floor PanelSDR FDEA202605150604Floor Panel · puncturedTWO PUNCTURES ON FLOOR PANEL 241ZFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 241ZFF ON MAIN CARGO COMPARTMENT. WAS REPAIRED IAW SRM 57-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025May 15, 2026 · N289FE · Boeing 767300 · Fuselage Floor PanelSDR FDEA202605150603Floor Panel · puncturedFOUR PUNCTURES ON FLOOR PANEL 241AGF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 241AGF ON MAIN CARGO COMPARTMENT. WAS REPAIRED IAW SRM 57-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025May 15, 2026 · N289FE · Boeing 767300 · Fuselage Floor PanelSDR FDEA202605150602Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 241DFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 241DFF ON MAIN CARGO COMPARTMENT. WAS REPAIRED IAW SRM 57-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025May 15, 2026 · N289FE · Boeing 767300 · Fuselage Floor PanelSDR FDEA202605150601Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 241KFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 241KFF ON MAIN CARGO COMPARTMENT. WAS REPAIRED IAW SRM 57-00-50-2R PAR 4 B FIG 201 SHEET 2 REV 94 DEC 15/2025May 15, 2026 · N289FE · Boeing 767300 · Fuselage Floor PanelSDR FDEA202605150600Floor Panel · puncturedFIVE PUNCTURES ON FLOOR PANEL 231LFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 231LFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW SRM 57-00-50-2R PAR 4-B FIG.201 SHEET 2 REV 94 DEC 15/2025.May 15, 2026 · N289FE · Boeing 767300 · Fuselage Floor PanelSDR FDEA202605150599Bottle · low pressureMAIN CABIN DOOR 2R EMERGENCY OPERATION CYLINDER REQUIRES SERVICING. SERVICED R1 FORWARD DOOR EMERGENCY OPERATION CYLINDER IAW AMM 52-10-14-03-02. ACFT OK TO CONTINUE.May 15, 2026 · N673FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA202605150598Iru · failedDURING INITIAL TAKEOFF, APPROXIMATELY 60 KIAS, MASTER WARNING CHIME AND IRS 3 FAULT, REJECTED TAKEOFF. RELEASED FOR SERVICE PER MEL : 34-25-01. R & R IRU 3 IAW 34-25-34-04. OPS CHKD NORMAL.May 15, 2026 · N657FE · Airbus A300F4605R · Integrated Flight SystemSDR WX0A2026051532816Epsu · no test(AIRCRAFT NOT GROUNDED) EPSU 11 WL FAILS EPSU BATTERY TEST. REMOVED AND REPLACED EPSU BATTERY SUPPLY REF AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-AMay 15, 2026 · N327NV · Airbus A319111 · Emergency LightingSDR KY7A202605150106Warning Light · illuminatedCARGO DOOR PRIMARY & SECONDARY LIGHTS ILLUMINATED IN TAKEOFF ROLL; ON WORK ORDER # 40582, WAITING FOR FINAL REPAIR REPORT DUE ON 05/17/2026May 15, 2026 · N971DC · Emb EMB145LR · Door Warning SystemSDR ABXA20260515206Module · faultedDURING TAXI, (L) PACK OFF CAUTION MSG. CREW RETURNED TO THE GATE (BTB). PERFORMED BITE TEST AND RESET OF BLEED SUPPLY MODULE FOR PER FIM 21-51 FT 844 NO FAULTS NOTED. PERFORMED ENG RUN PER AMM 71-00-00 ALL OPS CKS GOOD AT THIS TIME. AIRCRAFT REMAINS ETOPS 180.May 15, 2026 · N1709A · Boeing 767375 · Engine Bleed Air SystemSDR ABXA20260515205Module · faultedDURING TAXI, (L) ENGINE BLEED OFF MSG. CREW RETURNED TO THE GATE (BTB). PERFORMED BITE TEST AND RESET OF BLEED SUPPLY MODULE PER FIM 36-10 FT 847 NO FAULT NOTED, PERFORMED ENG RUN PER AMM 71-00-00 ALL OPS CKS GOOD AT THIS TIME. AIRCRAFT REMAINS ETOPS 180. A/C May 15, 2026 · N1709A · Boeing 767375 · Engine Bleed Air SystemSDR ABXA20260515203Fire Loop · warning messageDURING PREDEPARTURE CHECK, LH ENG OH LP 2 STATUS MESSAGE SHOWN. DEFERRED LH ENG OH LP2 STATUS MESSAGE IAW MEL 26-11-2-1 C/W MX PROCEDURES MBCB 05/25/26 PLACARD INSTALLED A/C RELEASE ETOPS 120. A/C RETURNED TO SERVICE.May 15, 2026 · N371CM · Boeing 767338 · Smoke DetectionSDR JR2R20260515014Skin · crackedL/H ELEVATOR #2 HINGE UPPER SKIN CUTOUT AROUND HINGE FITTING HAS COMPOSITE DAMAGE ON CORNER. REPAIRED PER ETD.May 15, 2026 · N86347 · Emb ERJ170200LL · Elevator, Plate/SkinSDR DALA2026051503015Battery Pack · inoperativeDURING SVC CHECK FOUND MID CABIN EMEGENCY LIGHTS OUT/INOP. REPLACED EPSU & BATTERY (14WL) IAW AMM 32-51. OPS CHECK OF EMERGENCY LIGHTS GOOD. (LP 8637951 - AIRCRAFT WAS GROUNDED)May 15, 2026 · N338DN · Airbus A321213 · Emergency LightingSDR JGVR20260515204Skin · corrodedMECHANICALLY REMOVED 1 AREA OF CORROSION ON THE UPPER AFT CORNER OF THE CUT OUT OF THE E-EXIT ON FUSELAGE SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.May 15, 2026 · N313QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR JGVR20260515203Spar · corrodedMECHANICALLY REMOVED CORROSION LOCATED ON RH WING AFT SPAR, AFT FACE OF SPAR WEB BELOW SPOILER PANEL #9 AROUND PRESSURE AND RETURN HYDRAULIC LINE CARRY THROUGH FITTINGS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS PER May 15, 2026 · N313QS · Cessna 680CE · Wing SparSDR JGVR20260515202Spar Cap · corrodedMECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED INSIDE LH HORIZONTAL STAB ELEVATOR COVE, LOWER SPAR CLIP BETWEEN INBOARD AND MIDDLE ELEVATOR HINGE ATTACHMENTS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS PER NETJETS May 15, 2026 · N313QS · Cessna 680CE · Horizontal Stabilizer, Spar/RibSDR JGVR20260515001Skin · corrodedMECHANICALLY REMOVED 1 AREA OF CORROSION AND 1 AREA OF BARE METAL LOCATED ON LH HORIZONTAL STAB UPPER SKIN NEAR INBOARD ELEVATOR HINGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLERS PER NETJETS REQUEST FOR TECHNICAMay 15, 2026 · N313QS · Cessna 680CE · Horizontal Stabilizer, Plate/SkinSDR JGVR20260515201Skin · corrodedMECHANICALLY REMOVED 1 AREA OF CORROSION AND 1 AREA OF BARE METAL LOCATED ON LH HORIZONTAL STAB UPPER SKIN NEAR INBOARD ELEVATOR HINGE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLERS PER NETJETS REQUEST FOR TECHNICAMay 15, 2026 · N313QS · Cessna 680CE · Horizontal Stabilizer, Plate/SkinSDR QR9R2026051500001Control Lever · out of limitsRECEIVED CONTROL LEVER ASSY FROM AIRBUS UNSERVICEABLE. MEASURED .026" AROUND SLIP BUSHING, MAX ALLOWED IS .019".May 15, 2026 · Bolkms BK117C2 · Main Rotor HeadSDR ICRR202605150001Link · crackedCRACK DISCOVERED DURING ULTRASONIC INSPECTION.May 15, 2026 · Cndair CL6002B19 · Engine Mount SectionSDR 2026FA0000386Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKED.May 15, 2026 · N61803 · Cessna 172M · Wing Miscellaneous StructureSDR SWIA2026051477294Hinge · damagedPAX DOOR PIANO HINGE FUSELAGE SIDE FWD AND AFT LUGS INNER SURFACE ARE ELONGATED OUT OF LIMITS REQUIRE REPLACEMENT. REMOVED PAX DOOR PIANO HINGE FUSELAGE SIDE IAW SRM 53-21-23 4 PROCEDURE A, B, C. INSTALLED A NEW PAX DOOR PIANO HINGE FUSELAGE SIDE IAW 53-21-2May 14, 2026 · N936SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2026051477207Intercostal · corrodedPAX DOOR , AFT INTERCOSTAL DD5 IS CORRODED. PAX DOOR , AFT INTERCOSTAL DD5 WAS REMOVED AND REPLACED IAW SRM 51-42-06-00.May 14, 2026 · N455SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051477202Former · corrodedPAX DOOR, FORMER AT BS 311. 75 IS CORRODED. REMOVED AND REPLACED PAX DOOR FWD FORMER AT BS 311.75 IAW SRM 51-42-06-00. COMPLETED TASK CARD 51-900-1003-SKY, NO WEIGHT CHANGE. REF CONTINUATION CARD FOR WORK PERFORMED.May 14, 2026 · N455SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051477180Bracket · corrodedPAX DOOR, AFT INTERCOSTAL BRACKET AT DD6 IS CORRODED. AFT INTERCOSTAL BRACKET AT DD6 WAS REMOVED & REPLACED IAW SRM 51-42-06-00. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE.May 14, 2026 · N455SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051477177Skin · dentedLEFT INBD FLAP HAD A DENT ON LOWER SKIN TRAILING EDGE, WS 104. DENT MEASURES APPROX 15L X 15W X 0030D. REPAIRED LT INBD FLAP SKIN IAW SNIEO 601R14008 S16, SRM 51-23-00 & SRM 51-42-13. COMPLETED SKYCARD 51-900-1003-SKY. NO WEIGHT CHANGE SEE CONTINUE CARD FOMay 14, 2026 · N455SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2026051477176Intercostal · corrodedPAX DOOR, AFT INTERCOSTAL DD4 IS CORRODED. REMOVED AND REPLACED PAX DOOR DD4 AFT INTERCOSTAL IAW SRM 51-42-06-00. COMPLETED TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE. REF CONTINUATION CARD FOR WORK PERFORMED.May 14, 2026 · N455SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051477175Door Frame · damagedPAX DOOR, FRAME AT BS 327. 763 BETWEEN DD6 AND DD8. PAX DOOR, FRAME AT BS 327.763 BETWEEN DD6 AND DD8 WAS R & R BY A NEW ONE IAW SRM 51-40-11-00, SRM 51-42-06-00 AND SRM 51-42-21-00 COMPLETED TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE. REF CONTINUATION CAMay 14, 2026 · N455SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026051477169Door Frame · corrodedPAX DOOR, FRAME AT BS 338.963 WAS CORRODED. THE DOOR FRAME WAS REMOVED & REPLACED IAW SRM 51-42-06-00, AND SRM 51-42-21-00.May 14, 2026 · N455SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026051477166Spar · gougedRIGHT INBD FLAP HAS A GOUGE ON THE FWD FACE OF THE FRONT SPAR LOCATED AT WS 127.25. REMOVED GOUGE DAMAGE AND REPAIRED RT INBD FLAP IAW REO 601R-57-52-2557, REV-.May 14, 2026 · N455SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2026051477164Intercostal · corrodedPAX DOOR, MID INTERCOSTAL AT DD1 BTWN BS 335. 763 & 323.363 IS CORRODED. PAX DOOR, MID INTERCOSTAL AT DD1 WAS REMOVED AND REPLACED IAW SRM 51-42-06-00 AND SRM 51-42-21-00.May 14, 2026 · N455SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051477162Intercostal · corrodedPAX DOOR, AFT INTERCOSTAL AT DD2 IS CORRODED. REMOVED AND REPLACED PAX DOOR DD2 AFT INTERCOSTAL IAW AMM 51-42-06-00.May 14, 2026 · N455SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026051477157Intercostal · damagedPAX DOOR, INTERCOSTAL DD7A BETWEEN FS 332.763 AND 320. 163. PAX DOOR, INTERCOSTAL DD7A REMOVED AND REPLACED FOR A NEW ONE IAW SRM 51-42-06-00.May 14, 2026 · N455SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR 4VAA202605140027Skin · corrodedDURING INSPECTION, CORROSION AND CHAFING WAS FOUND ON THE RIGHT NACELLE INSIDE SKIN. THE SKIN WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060709.May 14, 2026 · N749SA · Saab 2000SAAB · Nacelle/Pylon, Plate/SkinSDR 4VAA202605140008Splice · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT HORIZONTAL STAB UPPER FINGER SPLICE AT Y1595B-1500. IT WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060673.May 14, 2026 · N749SA · Saab 2000SAAB · Horizontal Stabilizer StructureSDR SWIA2026051477018Stringer · crackedSTGR 3L IS CRACKED AT F.S. 280. (C-CHECK RO 08/28/2026)REMOVED CRACKED STGR3L TO FS280 ATTACH ANGLES AND LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE ATTACH ANGLES PN# 600-31057-19 & 600-31057-20 AT SAME LOCATION IAW CRJ200 SRM 51-42-21, 51-42-06, & 51-40-May 14, 2026 · N477CA · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer