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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2026FA0000121Structure · crackedHORIZONTAL STABILIZER CRACKED BEYOND REPAIR. LEADING CENTER AT FORWARD SPAR.SDR DALA2026021201028Floor Support · corrodedCORRODED FLOOR SUPPORT, +Y765, BTW FR 66 - 70 IN THE AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, SRM 51-42-11, & DWG 10N01036. (LP 1447191)SDR DALA2026021201027Seat Track · corrodedCORRODED SEAT TRACK, +Y1292, BTWN FR 64 - 65 IN THE AFT GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-42-11, SRM 51-72-11, AND DWG 10N01036. (LP 1447183)SDR DALA2026021201026Seat Track · corrodedCORRODED SEAT TRACK, -Y765, BTW FR 64 - 66 IN THE AFT GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-72-11, & SRM 51-42-11, AND DWG 10N01036. (LP 1447149)SDR DALA2026021201025Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT, -Y254, AROUND HOLES BTW FR 16 - 20 IN THE FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11, AND DWG D53111462.SDR 2026FA0000120Stiffener · crackedR/H WING FWD WING WALK CRACKED. REPLACED WITH NEW ASSYSDR 2026FA0000119Stiffener · crackedRIGHT WING FWD WING WALK CRACKED. REPLACED WITH NEW ASSY.SDR 2026FA0000118Stiffener · crackedR/H WING AFT WING WALK CRACKED. REPLACED WITH NEW ASSYSDR 2026FA0000117Stiffener · crackedRIGHT WING AFT WING WALK CRACKED. REPLACED WITH NEW ASSY.SDR 2026FA0000116Stiffener · crackedRIGHT WING FWD WING WALK CRACKED. REPLACED WITH NEW ASSYSDR 2026FA0000115Stiffener · crackedRIGHT WING INBD FWD LWR SKIN, AFT STIFFENER CRACKED, REPLACED WITH NEWSDR 2026FA0000114Stiffener · crackedRT WING INBD FWD LWR SKIN, FWD STIFFENER CRACKED, REPLACED WITH NEWSDR 2026FA0000113Stiffener · crackedLH WING TOP I/B FWD SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEWSDR 2026FA0000112Stiffener · crackedLH WING TOP I/B FWD SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR 2026FA0000111Stiffener · crackedLH WING LWR I/B FWD SKIN, BOTTOM FWD STIFFENER CRACKED. REPLACED WITH NEWSDR 2026FA0000110Stiffener · crackedRIGHT WING LWR INBD FWD SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR 2026FA0000108Stiffener · crackedRIGHT WING LWR INBD FWD SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR AALA202602129327Light · no testAIRCRAFT WAS GROUNDED: DURING R1 SLIDE REPLACEMENT EMERGENCY LIGHT TEST 33-51-00-710-001 FAILED. MAINTENANCE REPLACED EMERGENCY LIGHT AND TESTED OK IAW 33-51-00.SDR 2026FA0000107Stiffener · crackedRIGHT WING LWR INBD FWD SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEW.SDR QR9R2026021200002Bolt · crackedNDI INSPECTION REVEALED HEX BOLT WAS CRACKED.SDR GTIA2025021239279Flashlight · inoperativeFWD GALLEY FLASHLIGHT INOP -INSTALLED NEW FLASHLIGHT PER SPIRIT A320 EMERGENCY DRAWING LAYOUT TEST . OK THIS CLOSES DMI PLC RMVD, MOC NOTIFIED DMI LOG UPDATEDSDR QR9R2026021200001Bolt · crackedNDI INSPECTION REVEALED HEX BOLT WAS CRACKED.SDR TSAA2026021200001Indicator · failedFIRST OFFICER'S AIRSPEED INDICATOR FAILED WITH A RED FLAG. NEEDLE FROZEN AT 296 KTS.SDR FDEA202602120191Seat Track · corrodedMAIN CABIN SEAT TRACK BETWEEN BS 1620 - 1420, LBL 58.22 MULTIPLE SPOTS OF CORROSION. REMOVED THE SEAT TRACK IAW SRM 51-40-02-0G, TRIMMED, LOCATED, & DRILLED A NEW SEAT TRACK SECTION IAW SRM 51-40-05-0G, SRM 51-40-08-0G, & DWG 657N3332, REV A. INSTALLED THSDR FDEA202602120190Skin · delaminatedDELAMINATION IN LEADING EDGE ON OTBD FLAP AT 9.5" INBD END. RT WING LEADING EDGE FLAP WAS REPAIRED IAW SRM 51-70-03-0G, PARA 5.A., FIG 5, SHEET 1, REV 93 AND SRM 57-53-01-2R TABLE I FIG. 201 (SHEET 5) REV 93.SDR FDEA202602120189Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 241ZFF OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, PAR 4-B, FIG 201, SHEET 2, REV 93.SDR FDEA202602120188Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 242TFA OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, REPAIR GENERAL, PARA 4.B, FIG 201, SHEET 2, REV 93.SDR FDEA202602120187Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 241YFA OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, REPAIR GENERAL, PARA 4.B, FIG 201, SHEET 2, REV 93.SDR FDEA202602120186Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 242MFF OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R, REPAIR, GENERAL PARA. 4.B, FIG. 201, SHEET 2, REV 93.SDR FDEA202602120185Floor Panel · crackedSEVERAL CRACKS ON FLOOR PANEL 242VFF OF MAIN DECK CARGO. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4.B, FIG 201, SHEET 2, REPAIR GENERAL, REV 93.SDR FDEA202602120184Floor Panel · dentedMAIN DECK, AT APROX. BS 870, FLOOR PANEL 241GFF UPPER SKIN DENTED. REPAIRED THE TOP SKIN THE FLOOR PANEL IAW SRM 53-00-50-2R 4.B. INSTALLATION OF THE FLOOR PANEL WILL BE ACCOMPLISHED ON WO 91257, SEQ 149. MAJOR REPAIR.SDR FDEA202602120183Wire · wrong partFOUND BREAKAWAY WIRE THAT SECURES THE RELEASE MECHANISM NOT TO BE CLAD-PLATED COPPER WIRE. REMOVED LT DOOR SLIDE IAW MM 25-66-01-4. REMOVED STAINLESS SAFETY WIRE AND INSTALLED CORRECT WIRE IAW FEA G-2560-F0386282C. REINSTALLED DOOR SLIDE IAW 25-66-01-4. DOSDR FDEA202602120182Smoke Detector · no testAFT CARGO SMOKE LOOP A WILL NOT TEST. LIKELY FAILED COMPONENT IS THE 50WU3, ELECTRONIC SMOKE DETECTION UNIT. TROUBLESHOT IAW TSM 26-19-01 STANDARDS. AMM: 26-19-34-04 PERFORMED BITE TEST ON MAIN CARGO SMOKE DETECTOR CONTROL UNITS, 50WU1, 50WU2 AND 50WU3. FASDR COEA2026021202946Bolt · brokenFLT 7692/PDX: LEFT BRAKE SEIZED UP ON TAXI OFF RUNWAY. MAINTENANCE DISCOVERED THE WHEEL HALF BOLT ON THE LT MAIN WHEEL BROKEN. REPLACED THE L/H MAIN WHEEL ASSY. AND L/H BRAKE ASSY. OPS CHECK GOOD.SDR DALA2026021201015Light · inoperativeCEILING EMERGENCY LIGHT OUT. R & R CEILING EMERGENCY LIGHT IAW AMM 33-51, OPS CHECKED GOOD.SDR CALA2026021213745Probe · faultyFUEL IMBALANCE ON TANK 1 DECREASING RAPIDLY. PERFORMED NR 1 TANK FQIS DRY RESISTANCE AND CAPACITANCE CHECK IAW AMM 28-41-21-710-801, FOUND F15, F1, F2, F3, F4, F5, F6 FQIS TANK UNITS OUT OF LIMITS. R & R NR 1 FQIS TANK UNITS OUT OF LIMITS F15, F1, F2, F3, FSDR REXA2026080301406Strap · corrodedINITIAL INSPECTION: CORROSION ON JOINT STRAP, SETTLEMENT Ï¿½REA OF FAIRING ACCESS PANEL 194AB & 193AB JOINT STRAP (FRAME ASSY) SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB & 193AB WAS REPAIRED PER REO 670-53-82-733. REV. --SDR REXA2026080301390Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM RBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT CENTER COCKPIT FLOOR BEAM RBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 670-53-11-2278REV. --SDR REXA2026080301385Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT RH WING CRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT RH WING WAS REPAIRED PER REO 670-57-41-681 REV - -.SDR DALA2026080604540Stringer · damagedSTRINGER 3R. FRAME 61 - 62, TOOLING DAMAGE. COMPLIED WITH ERA 631894-14. (1446780) AIRCRAFT WAS GROUNDED.SDR SWIA2026021176063Door Frame · crackedSUSPECT OF CRACK ON DOOR LANDING LH ON UPPER ELECTRIC ACCESS DOOR SURROUND STRUCTURE FS173.00 TO FS193.00. REMOVED AND REPLACED WITH 1 EA OF NEW LANDING. REF. CRJ900 SRM 51-42-06-001-001-A01 AND DWG CC670-33040 REV -G. COMPLIED WITH ALL STEPS OF TASK CARD 5SDR SWIA2026021176042Pressure Blkhd · chafedUPON REMOVAL OF LT AILERON REAR QUADRANT, FOUND CHAFE ON AFT PRESSURE BULKHEAD FS847. REPAIRED LH AFT PRESSURE BULKHEAD FS847 PER REO 690-53-41-579. REV -. SEE CONTINUATION CARD FOR DETAILSCOMPLIED WITH 51-900-1002. PRESSURE CHECKED GOOD.SDR 2026FA0000412Actuator · separatedWHEN FRONT COCKPIT PILOT ACTUATED THE FLAP SWITCH, BOTH SIDES DROPPED TO FULL DOWN IMMEDIATELY AND THE FLAP SWITCH WAS UNABLE TO MOVE THE FLAPS ON EITHER SIDE. MAINTENANCE FOUND THAT THE FLAP ACTUATOR HAD SEPARATED FROM THE FLAP MOTOR/GEARBOX. REMOVED AND REPSDR VNAA20260508002Skin · dentedPER CUSTOMER REQUEST WORK REO 670-53-61-2676 REV (P1) DATED 2026-02-09 ( REPAIR TO DENTS ON FUSELAGE SKIN BETWEEN FS1000.00-FS1051.30 AND STR24R-STR26L) COMPLIED WITH MHIRJ REO 670-53-61-2676 REV -- DATED 2026-03-04 (REPAIR TO DENTS ON FUSELAGE SKIN BETWEEN SDR SWIA2026021175746Rib · corrodedLEFT WHEEL WELL BATTERY RIB AT WS58.8 HAS FWD CHANNEL CORRODED. REMOVED AND REPLACED FWD CHANNEL IAW SRM 51-42-21 AND DWG. 601R10205 REV. -F. LEAK CHECKED GOOD.SDR SWIA2026021175721Hinge · damagedPAX DOOR HINGE ON THE PAX DOOR ROLL PIN HOLE IS ELONGATED. PERFORMED A MAJOR REPAIR TO THE PAX DOOR PIANO HINGE HALF (DOOR SIDE) BY INSTALLING A LARGER SPRING PIN IAW MHIRJ REO 601R-52-11-3094 REV-. COMPLETED SKYWEST RII MAJOR REPAIR TASK CARD 51-900-1003-SKSDR SWIA2026021175704Floor Support · corrodedRIGHT FLOOR SUPPORT CORRODED AT BS 559 FOUND TO BE OUT OF LIMITS IAW REO 601R-53-41-666, REV-C. REPAIRED RT FLOOR SUPPORT IAW REO 601R53-41-3408, REV -. 6 AND SKY CARD 51-900-1003-SKY.SDR REXA2026032700248Hinge · corrodedCORROSION WAS FOUND ON FITTINGS LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). DUE TO EXCESSIVE CORROSION PER CRJ 900 SRM 51-10-06-001-001-A01 ON FITTINGS (4EAS) LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSESDR REXA2026032700247Fitting · corrodedCORROSION WAS FOUND ON FITTINGS LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). DUE TO EXCESSIVE CORROSION PER CRJ 900 SRM 51-10-06-001-001-A01 ON FITTINGS (4EAS) LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSESDR REXA2026032700246Fitting · corrodedCORROSION WAS FOUND ON FITTINGS LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). DUE TO EXCESSIVE CORROSION PER CRJ 900 SRM 51-10-06-001-001-A01 ON FITTINGS (4EAS) LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSE