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.
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 AALA202607015986Wire · looseAIRCRAFT WAS NOT GROUNDED: SEAT 15C LOWER ASSEMBLY EMERGENCY LIGHT FOUND INOPERATIVE. MAINTENANCE FOUND CONNECTOR WIRES LOOSE, RECONNECTED CONNECTOR WIRES PER ESPM 20-48-21 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING WITH NO ISSSDR DALA2026070103877Coalescer Bag · odorBURNING SMELL WITH APU ON AND PACKS, R & R COALESCER BAGS PER B717 AMM 21-54-08. (6688572) (AIRCRAFT GROUNDED).SDR JR2R20260701783Angle · crackedLH STABILIZER MIDDLE SPAR RIB 10 I/B ANGLE IS CRACKED. REPLACEDSDR R61A2026070100178Skin · crackedCRACKED LEFT WING FWD WHEEL WELL EDGE AT RIB 3A. PERFORMED DOUBLER REPAIR IAW ETD2026-170-010629-A.SDR JR2R20260701868Fitting · crackedRIGHT MLG W/W, AILERON QUADRANT CRACKED ON THE O/B SIDE. REPLACEDSDR SIMA20260701001Fitting · lack of lubeFA CAN'T GET 2L DOOR TO OPEN AND DISARM. VISUALLY INSP L2 DOOR EVACUATING SLIDE/GIRT BAR FLAP AND FITTING AS PER AMM 53-23-21 AND AMM 52-12-41. CLEANED AND LUBE STICKY FITTINGS. OPENED AND CLOSED L2 DOOR. ARMED AND DISARMED DOOR OPS CHECK GOOD. REF SDS 52-12-0SDR JR2R20260701891Seat Track · corrodedFWD WET AREA SEAT TRACK BEAM RBL11 BETWEEN FR12 - FR14 AROUND GALLEY ATTACH POINT CORRODED. REPAIRED.SDR 2026FA0000553Fuel Line · crackedWHILE PERFORMING FUEL SET UP FOUND FUEL LINE FROM THROTTLE BODY TO FUEL DISTRIBUTION MANIFOLD B-NUT FERRULE TO BE CRACKED.SDR JR2R20260701962Rib · crackedLEFT HORIZONTAL TIP RIB 14 CRACKED. REPAIREDSDR DALA2026070103873Servo Valve · faultedDE - DUE TO BRAKES AUTO BRK FAULT ECAM WARNING. REPLACED NORMAL BRAKE SERVO VALVE (15GG) AND BSCU (10GG). (LP: 8749444, AIRCRAFT WAS GROUNDED).SDR JR2R20260701872Beam · corrodedFWD PASSENGER DOOR LOWER BEAM AFT GIRT BAR FITTING CUTOUT HAS DAMAGED. REPLACED.SDR SWIA2026063077734Intercostal · corrodedCORROSION ON PAX DOOR MID DD3 INTERCOSTAL. REPLACED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, & DWG 601R31702, REV N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. PRESSURE LEAK CHECKED GOOD.SDR SWIA2026063077733Former · corrodedCORROSION ON PAX DOOR FORMER BS 323.936 AND CLEAT BETWEEN MID DD3 AND MID DD4 INTERCOSTALS. REPLACED THE FORMER IAW SRM 51-42-06-001-001-A01, REV 38, & DWG 601R31702, REV N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. PRESSURE LEAK CHECKED GOOD.SDR SWIA2026063077732Former · corrodedCORROSION ON PAX DOOR FORMER BS 335.163 BETWEEN MID DD3 AND MID DD4 INTERCOSTALS. REPLACED WITH NEW, PASSENGER DOOR FORMER IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702, REV N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. PRESSURE LEAK CHECKED GOOD.SDR SWIA2026063077674Former · corrodedPAX DOOR FORMER FS32941 BETWEEN DD4 AND DD5 INTERCOSTAL IS CORRODED MX 32541370 C-CHECK RO 10132026REPLACED WITH NEW, PASSENGER DOOR FORMER FS32941 BETWEEN DD4 AND DD5 INTERCOSTAL IAW CRJ 900 SRM 51-42-06-001-001-A01, CRJ 900 SRM 51-42-21-001-001-A01 AND DWSDR VNAA202609010001Skin · corrodedLIGHTNING STRIKES (14 EA) FROM BS 594 - 661+32.00, BTW STRS 19L TO 26R AT FUSELAGE EXTERNAL SKIN. LIGHTNING STRIKES (14 EA) FROM BS 594 - 661.00+32, BTW STRS 19L TO 26R AT FUSELAGE EXTERNAL SKIN WERE REPAIRED PER REO 690-53-31-1159 REV -.SDR DALA2026082504828Longeron · corrodedER/A 635349-14; A220-100 / FWD & CNTR WING TO BODY FAIRING / MULTIPLE LONGERON / CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 635349-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 FLIGHT HOURS FROM 12,873 TOTAL AIRCRAFT FLIGHT HOURSSDR REXA2026082401628Support · crackedAFTER SEAL RETAINERS SUPPORTS REMOVAL, CRACKED FORWARD LOWER SKIN ANGLE (SUPPORT OF SEAL RETAINERS) WAS FOUND AT RH WING. FORWARD LOWER SKIN ANGLE WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 PAR. 8 C AND SRM CRJ 900 SRM 51-42-21-001-001-A01 PAR 6. C.SDR REXA2026082401624Frame · corrodedCORROSION ON ANGLE OF FRAME FS 1015 STGR 20L CORROSION ON ANGLE OF FRAME FS 1015 STGR 20L WAS REOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND IT WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01SDR REXA2026082401623Frame · corrodedCORROSION ON FRAME FS 1015 STGR 26R TO STGR 23L REPAIR PER EA NO. CRJ953-22686 REV. IRSDR REXA2026082401622Window Frame · crackedCRACK ON BOTTOM ANGLE POST (2 EAS) LH/RH ON INTERNAL STRUCTURE BTWN WINDSHIELD AND SIDE WINDOWS. ANGLE POST (2 EAS) LH/RH ON INTERNAL STRUCTURE BTWN WINDSHIELD AND SIDE WINDOWS WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01SDR REXA2026082401621Window Frame · crackedCRACK ON BOTTOM ANGLE POST (2 EAS) LH/RH ON INTERNAL STRUCTURE BTWN WINDSHIELD AND SIDE WINDOWS. ANGLE POST (2 EAS) LH/RH ON INTERNAL STRUCTURE BTWN WINDSHIELD AND SIDE WINDOWS WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01SDR REXA2026082401620Floorbeam · crackedCRACK ON FLOOR BEAM RBL12 ON FS280 AT FLIGHT COMPARTMENT FLOOR STRUCTURE. FLOOR BEAM RBL12 ON FS280 AT FLIGHT COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-11-2225 REV - -SDR REXA2026082401619Intercostal · corrodedCORROSION ON INTERCOSTAL BTW FS=866 TO 861/ STGR 21R AT INTERNAL FUSELAGE STRUCTURE DUE TO EXCESSIVE CORROSION ON INTERCOSTAL BTW FS=866 TO 861/ STGR 21R AT INTERNAL FUSELAGE STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-A01SDR REXA2026082401618Support Angle · crackedCRACK ANGLE SUPPORT INSIDE OF ACCESS PANEL 122CR ANGLE SUPPORT INSIDE OF ACCESS PANEL 122CR WAS FABRICATED AND REPLACED PER EA NO CRJ953-22677 REV. IR AND CRJ-900 SRM 51-42-21-001-001-A01SDR REXA2026082401617Frame · crackedCORROSION ON FRAME FS 661+46 BTW STGR25R TO STGR 23R, FRAME 661+32 BTW STGR 27 TO STGR 25R, FRAME FS 661 BTW STGR 27R TO STGR 26R, FRAME FS 597 BTW STGR 27 TO STGR 26R. FRAME FS 661 BTW STGR 27R TO STGR 26R WAS REPAIRED PER CRJ 900 SRM 53-00-06-201-001-A03SDR REXA2026082401614Web · corrodedCORROSION ON WEB BTW 1LBL TO 27LBL BTW FS 1088 TO FS 1098 CORROSION ON WEB BTW 1LBL TO 27LBL BTW FS 1088 TO FS 1098 WAS EA NO. REPAIRED PER CRJ953-22801 REV. BSDR REXA2026082401600Hinge Fitting · corrodedCORROSION WAS FOUND ON BORE LUGS OF AILERON HINGES 2, 3 AND 4, ALSO CORROSION ON INB LUG FACE OF HINGE 4 AT RH WING REAR SPAR. BORE LUGS OF AILERON HINGES 2, 3 AND 4, ALSO INB LUG FACE OF HINGE 4 AT RH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-552 REV. - SDR REXA2026082401599Hinge Fitting · corrodedCORROSION WAS FOUND ON BORE LUGS OF AILERON HINGES 2, 3 AND 4, ALSO CORROSION ON INB LUG FACE OF HINGE 4 AT RH WING REAR SPAR. BORE LUGS OF AILERON HINGES 2, 3 AND 4, ALSO INB LUG FACE OF HINGE 4 AT RH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-552 REV. - SDR REXA2026082401598Hinge Fitting · corrodedCORROSION WAS FOUND ON BORE LUGS OF AILERON HINGES 2, 3 AND 4, ALSO CORROSION ON INB LUG FACE OF HINGE 4 AT RH WING REAR SPAR. BORE LUGS OF AILERON HINGES 2, 3 AND 4, ALSO INB LUG FACE OF HINGE 4 AT RH WING REAR SPAR WERE REPAIRED PER REO 690-57-51-552 REV. - SDR REXA2026082401597Support Beam · chafedWEAR ON BEAM SUPPORT OF BUNGE MECHANISM NEXT TO AFT PULLEY AT AFT BAGGAGE COMPARTMENT. WEAR ON BEAM SUPPORT OF BUNGE MECHANISM NEXT TO AFT PULLEY AT AFT BAGGAGE COMPARTMENT WAS REPAIRED PER EA NO. CRJ953-22738 REV. IRSDR REXA2026082401596Stringer · corrodedCORROSION ON STRINGER 21R FROM FS319 TO FS333 AND FROM FS394 TO FS453 AT E/E COMPARTMENT DUE TO EXCESSIVE CORROSION ON STRINGER 21R FROM FS394 TO FS477 AT E/E COMPARTMENT WAS REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01, SRM 53-21-03-101-002-A04, SRM 51-42-06SDR REXA2026082401595Stringer · corrodedCORROSION ON STRINGER 21R FROM FS319 TO FS333 AND FROM FS394 TO FS453 AT E/E COMPARTMENT DUE TO EXCESSIVE CORROSION ON STRINGER 21R FROM FS280 TO FS333 AT E/E COMPARTMENT WAS REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01, SRM 53-21-03-101-002-A04, SRM 51-42-06SDR REXA2026082401594Stringer · corrodedCORROSION ON STRINGER 19R FROM FS310 TO FS319 AND FROM FS437 TO FS477 AT E/E COMPARTMENT. DUE TO EXCESSIVE CORROSION ON STRINGER FS437 TO FS477 AT E/E COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-00-03-201-001-A02SDR REXA2026082401593Doubler · corrodedCORROSION ON INTERNAL ANTENNA DOUBLER BTW FS295 AND FS310 BTW STGR26L AND STGR26R AT E/E COMPARTMENT. INTERNAL ANTENNA DOUBLER BTW FS295 AND FS310 BTW STGR26L AND STGR26R AT E/E COMPARTMENT WAS REPAIRED PER EA NO. CRJ953-22769 REV. IRSDR REXA2026082401592Stringer Splice · corrodedDUE TO EXCESSIVE CORROSION ON STRINGER SPLICES (3E/A) ON FS333 ON STGR21R, STGR22R AND STGR23R AT E/E COMPARTMENT WERE REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01 DUE TO EXCESSIVE CORROSION ON STRINGER SSDR REXA2026082401591Stringer Splice · corrodedDUE TO EXCESSIVE CORROSION ON STRINGER SPLICES (3E/A) ON FS333 ON STGR21R, STGR22R AND STGR23R AT E/E COMPARTMENT WERE REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01 DUE TO EXCESSIVE CORROSION ON STRINGER SSDR REXA2026082401590Stringer Splice · corrodedDUE TO EXCESSIVE CORROSION ON STRINGER SPLICES (3E/A) ON FS333 ON STGR21R, STGR22R AND STGR23R AT E/E COMPARTMENT WERE REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01 DUE TO EXCESSIVE CORROSION ON STRINGER SSDR REXA2026082401589Frame · corrodedCORROSION ON FRAMES BTW FS=847+16/STGR26L TO 26R, FS=847+32/STGR26L TO 26R AT INTERNAL FUSELAGE STRUCTURE CORROSION ON FRAMES BTW FS=847+16/STGR26L TO 26R WAS REPAIRED PER EA NO. CRJ953-22764 REV. IRSDR REXA2026082401559Structure · crackedCRACK EXTERNAL POWER BOX INSIDE OF ACCESS PANEL 122DR. EXTERNAL POWER BOX INSIDE OF ACCESS PANEL 122DR WAS REPLACED IAW SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01.SDR REXA2026082401558Seat Track · corrodedCORROSION ON SIDE SEAT TRACKS BTW BS 744 - 768 RT SIDE AND BTW BS 785 - 847+16 LT SIDE IN PAX CABIN. CORROSION ON SIDE SEAT TRACKS WAS EVALUATED OUT LIMITS IAW SRM 53-41-49-101-001-A02. REPLACED IAW AMM 53-00-49.SDR REXA2026082401557Seat Track · corrodedCORROSION ON SIDE SEAT TRACK BTW BS 744 - 768 RT SIDE & BTW BS 785 - 847+16 LT SIDE AT PAX CABIN CORROSION ON SIDE SEAT TRACK LT SIDE EVALUATED OUT LIMITS IAW SRM 53-41-49-101-001-A02. REPLACED IAW AMM 53-00-49.SDR REXA2026082401552Frame · corrodedCORRODED FRAME, FS 1000, STR 25R - 23L. THE FRAME WAS REPAIRED IAW EA CRJ953-22813, REV IR.SDR REXA2026082401549Rib · corrodedCRACK ON RIB WS=14.50 AT RH MLG WHEEL WELL AREA. THE RIB WAS REPLACED IAW SRM 51-42-21-001-001-A01, PAR 6.C, SRM 51-42-22-001-001-A01, PAR. 6.& AMM 32-32-06.SDR AALA202608185979Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER BETWEEN FR 59 AND FR 60 AND S43L - REPAIRED STRINGER PER EA 377430SDR SWAA2026081136726Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 194E AT LOWER FUSELAGE. REPAIRED THE ACCESS PANEL 194E IAW SRM 51-70-05-2R-8, REPAIR 8.SDR SWAA2026081125967Panel · crackedCRACKED LT WING INBD FIXED TRAILING EDGE SHELF PANEL. REPLACED THE LT WING SHELF PANEL IAW SRM 51-40-02, AND DWG 115A2200, SHEET 2, REV D.SDR SWIA2026063076792Angle · corrodedUPON REMOVAL OF THE INNER SKIN FOUND DD7 FS311 ANGLE CORRODED. REMOVED AND INSTALLED NEW PAX DOOR DD7 FS311 ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702, REV N. PERFORMED PRESSURE LEAK TEST OF THE REPAIR AREA IAW AMM 21-31-00-910-801-A01. LEAK TEST GSDR SWIA2026063076788Intercostal · corrodedUPON REMOVAL OF THE INNER SKIN FOUND PAX DOOR DD5 BS 311 ANGLE CORRODED. REMOVED & INSTALLED NEW PAX DOOR DD5 BS 311 ANGLE IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702, REV N. PERFORMED PRESSURE LEAK TEST OF THE REPAIR AREA IAW AMM 21-31-00-910-801-A01. LESDR SWIA2026063076771Intercostal · corrodedUPON REMOVAL OF INNER SKIN FOUND PAX DOOR AFT INTERCOSTAL DD4 CORRODED. REMOVED AND INSTALLED A NEW PAX DOOR AFT INTERCOSTAL DD4 IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702 REV N. PERFORMED PRESSURE LEAK TEST OF THE REPAIR AREA IAW AMM 21-31-00-910-801-A0