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 HNAA2026020100107Adc · failedADC 1 FAILED IN FLIGHT FACT 01FEB26 17:47 ALB R&R'D ADC1 AT POS 100 IAW EMB145 AMM 34-15-01. PERFORMED LEAK CHECK IAW AMM 34-13-00. OPS CHECK DONE IAW AMM 34-15-00, SYSTEM TESTED SERVICEABLE, OK FOR SERVICE.SDR SCNA20260202052Smoke Detector · false activationRIGHT 2R LAV SMOKE DETECTOR ALARM 4 TIMES INFLIGHT, WHILE EMPTY. PERFORMED LAVATORY SMOKE DETECTOR TEST IAW AMM 26-14-00, NO DEFECTS NOTED, OKAY FOR SERVICE.SDR DALA2026020200749Strap · crackedCRACKED STRAP ASSY, HINGE FITTING 5 ON THE RT HORIZONTAL STAB. REPLACED THE STRAP ASSY AIW SRM 51-72-11, DWG D55181526, & AMM 55-16-42-400-001-A. MEASUREMENT OF CRACK: L= 0,7170 INCH. (LP 1430773)SDR DALA2026020200748Floor Support · corrodedCORRODED FLOOR SUPPORT -Y1162.5, BTWN FR 68 TO FR 69 AFT GALLEY. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND SRM 51-42-11, AND DWG D53472189, AND DWG D53472780. MEASUREMENT OF CORROSION: L= 0.850 INCH W= 0.668 INCH D= 0.036 INCH.SDR DALA2026020200747Seat Track · corrodedCORRODED SEAT TRACK +Y1292, FR 16 & 20 IN THE FWD GALLEY. REPLACED THE SEAT TRACK IAW SRM 51-72-11, SRM 51-42-11, DWG D53110920. & DWG D53112812. MEASUREMENT OF CORROSION: L= 3.640 IN W= 0.410 IN D= 0.035, (LP 1430750)SDR DALA2026020200746Window Frame · crackedCRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE RH SIDE POCKET INTERNAL AREA, AT LOWER INBOARD RADIUS, CRACK DIRECTION IS HORIZONTAL, CRACK LENGTH IS 0.375 INCH, AD 2020- 17-03 / WORKCARD 5311-0122 6-01. COMPLIED WITH ER/A 631326-14AD REV. ORIGISDR DALA2026020200745Fitting · not reportedPERFORM ER/A 596680-14AD CONTINUITY FITTINGS LT & RT SIDE REPLACEMENT. COMPLIED WITH ER/A 596680-14AD REV A. MATCHES WITH ALL STEPS ON PRI 596680-14AD REV 0, PRI 596680-14AD REV 1, PRI 596680-14AD REV2 AND PRI 596680-14AD REV 3. STEPS RELATED TO ITEMS OF ER/ASDR DALA2026020200741Fitting · corrodedCORROSION CENTER FITTING LOCATED BTW FR 66 TO FR 68 RH SIDE LOWER SILL AT AFT GALLEY AREA (SSI 534147). REPLACED CENTER FITTING LOC. BTW FR 66 TO FR 68 RH SIDE LOWER SILL AT AFT GALLEY AREA IAW SRM 51-42-11, A320 SRM51-72- 11, DWG D53480505, ISSUE: FE. MEASSDR AALA202602011242Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 ENTRY LOWER SILL INNER CHORD BETWEEN BS 294.50 AND BS 312.0. REPLACED INNER CHORD PER AARD 51-00-05-1 AND EA 366791.SDR IXXA20260201001Floorbeam · crackedBS 246 FLOORBEAM IN MEC LEFT TUNNEL HAD CRACKED VERTICAL STIFFENER LBL 26.SDR REXA2026073101352Acoustic Panel · crackedAFTER Z STIFFENER REMOVAL, CRACK WAS FOUND AT ACOUSTIC PANEL SKIN OF THE RH UPPER TRANSCOWL ACOUSTIC PANEL SKIN OF THE RH UPPER TRANSCOWL WAS REPAIRED PER EA CRJ954-21346 REV IRSDR SIMA20260131002Reinforcement · not reportedSTD-REQ EJ-53MA-077 OPS PTA DUE - REINFORCEMENT OF NLG BAY BULKHEAD WEB AND FRAME 8. TRANSFERRED FROM NRWC 770-ABI-02960 ITEM 1" (MAJOR ASLTERATION) PERFORMED REINFORCEMENT OF NLG BAY BULKHEAD WEB AND FRAME 8. IAW EJ-53MA-077 PT.A SEE NRTC F099251.SDR SIMA20260131001Reinforcement · not reportedSTD-REQ EJ-53MA-078 OPS PTA DUE - FORWARD PASSENGER AND SERVICE DOORS CUTOUT STRUCTURE REINFORCEMENT. TRANSFERRED FROM NRWC 770-ABI-02962 ITEM 1" (MAJOR ALTERATION) EO EJ-53MA-078 OPS PTA - FORWARD PASSENGER AND SERVICE DOORS CUTOUT STRUCTURE REINFORCEMENT C/SDR SIMA20260131003Reinforcement · not reportedSTD-REQ EJ-53MA-078 OPS PTB DUE - FORWARD PASSENGER AND SERVICE DOORS CUTOUT STRUCTURE REINFORCEMENT. TRANSFERRED FROM NRWC 770-ABI-02961 ITEM 1"(MAJOR ALTERATION) EO EJ-53MA-078 OPS PTB - FORWARD PASSENGER AND SERVICE DOORS CUTOUT STRUCTURE REINFORCEMENT X/WSDR COEA2026042314801Floorbeam · corrodedFLIGHT COMPARTMENT, FLOORBEAM 5 R/H HAS LEVEL 2 CORROSION UPPER SURFACE. REPAIR PER ATR72 SRM 51-25-01, 51-25-04 REV. 121.SDR SWIA202604175770Intercostal · corrodedPAX DOOR INTERCOSTAL DD6 MIDDLE HAS CORROSION. REMOVED, REPLACED AND INSTALLED NEW PASSENGER DOOR INTERCOSTAL DD6 MIDDLE IAW SRM 51-42-06, SRM 51-42-21, AND DWG 601R31702, REV-N. COMPLIED WITH SKY WEST TASK CARD 51-900-1003-SKY. MAJOR REPAIR.SDR AALA202603304166Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 43L AND BTW FR 59 TO FR 60 AFT CARGO COMPARTMEN (L= 0.542 IN W= 0.382 IN D= 0.025 IN). MAINTENANCE REPLACED STRINGERSDR VNAA20260329020Fitting · corrodedCORROSION FLOOR FITTING ON ACCESS 307 (2EAS) ON GALLEY 3. FLOOR FITTING ON ACCESS 307 (2EAS) ON GALLEY 3 WERE REPLACED PER CMM 25-33-13SDR VNAA20260329019Floorbeam · crackedCRACK ON ANGLE OF FLOORBEAM FS280 AND RBL12 AT PAX CABIN FLOOR. ANGLE OF FLOORBEAM FS280 AND RBL12 AT PAX CABIN FLOOR WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01.SDR SWAA2026030966576Floorbeam · corrodedCORRODED FLOORBEAM, BS 986.5, RBL 43, WL 208.1. REPAIRED THE FLOORBEAM IAW SRM-53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4, FIG 205.SDR SWAA2026030966425Floor Support · corrodedCORRODED FLOOR SUPPORT, BS 947.5 - 967, LBL 24, WL 208.1. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 147A5650, SHEET 5, REV E.SDR SWAA2026030966426Angle · corrodedCORRODED ANGLE, FLOOR STRUCTURE BS 992.8, RBL 31, WL 208.1. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 147A5700, SHEET 123, REV A.SDR SWAA2026030566543Angle · crackedCRACKED ANGLE, BS 400, STRINGER 26L. REPLACED THE ANGLE IAW SRM 51-40-02, & DWG 143A7505, SHEET 137, REV -. THE ANGLE WAS REPLACED DUE TO NO ALLOWABLE DAMAGE LIMITS IN SRM 53-00-53-1A-2.SDR SWAA2026030566537Angle · crackedCRACKED ANGLE, BS 500G, STRINGER 26L FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, & DWG 143A7505, SHEET 138, REV -.SDR SWAA2026030566548Angle · crackedCRACKED ANGLE, BS 500H, STRINGER 26R, FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, & DWG 143A7505, SHEET 139, REV -.SDR SWAA2026030566544Angle · crackedCRACKED ANGLE, BS 500G, STRINGER 26L, REPLACED THE ANGLE IAW SRM 51-40-02, & DWG 143A7505, SHEET 138, REV -.SDR SWAA2026030566545Angle · crackedCRACKED ANGLE, BS 500G, STRINGER 26R. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV -.SDR SWAA2026030566546Angle · crackedCRACKED ANGLE, BS 500H, STRINGER 26L. REPLACED THE ANGLE IAW SRM 51-40-02, & DWG 143A7505, SHEET 139, REV -.SDR SWAA2026030566549Support Bracket · crackedCRACKED SUPPORT BRACKET, BS 727. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 144A2600, SHEET 1084, REV-.SDR SWAA2026030566538Angle · crackedCRACKED ANGLE, BS 500H, STRINGER 26R. REPLACED THE ANGLE, IAW FASTENERS IAW SRM 51-40-02-0G, SRM-51-10-02-0G-0, ITEM 9, & DWG 143A7505, SHEET 138, REV-.SDR SWAA2026030566547Angle · crackedCRACKED ANGLE, BS 500H, STRINGER 26L. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02, & DWG 143A7505, SHEET 139, REV -.SDR SWAA2026030566536Sill Drain · corrodedCORRODED LOWER SILL DRAIN, BS 440 - 492.4, RBL 21, WL 156. REPLACED THE SILL DRAIN AND FASTENERS IAW SRM 51-40-02, AND DWG 143A8330, SHEET 30, REV -.SDR SWAA2026030566540Gusset · crackedCRACKED GUSSET ANGLE, BS 500I, STRINGER 19R. REPLACED THE GUSSET ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, AND DWG 143A7902, SHEET 256, REV B.SDR SWAA2026030566539Gusset · crackedCRACKED GUSSET ANGLE, BS 500I, STRINGER 21R, FWD CARGO BAY. REPLACED THE GUSSET ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7902, SHEET 257, REV B.SDR SWAA2026030566414Plate · crackedCRACKED CORRUGATED PLATE IRSS 216, LT WING T/E. REPLACED THE CORRUGATED PLATE IAW SRM 51-10-02-0G, ITEM 9, SRM 51-40-02-0G, AND DWG 115A2001, SHEET 78, REV: A.SDR SWAA2026030566417Angle · crackedCRACKED ANGLE ON ACCESS PANEL 551GB, LT WING. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.SDR SWAA2026030566418Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 561AB, LT WING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.SDR SWAA2026030566419Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 561CB, LT WING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.SDR VNAA20260304023Fitting · corrodedCORROSION FLOOR FITTING ACCESS 107. REPLACED IAW CMM 25-33-21.SDR HNAA2026030400183Floor Support · corroded00437 MID FLOOR GUSSET FROM FR 45 TO FR 47 HAS CORROSION. REMOVED AND REPLACED CENTER OMEGA BEAM FROM FR 46 - FR 53 (GUSSET P/N 145-30634-011) PER EMB 145 SRM 51-40-02-PR.SDR HNAA2026030400182Floor Support · corrodedMID FLOOR GUSSET FROM FR 38 TO FR 45 HAS CORROSION,. REMOVED AND REPLACED WITH NEW FROM STOCK MID FLOOR GUSSET FROM FR 38 TO FR 45 IAW EMB145 SRM 51-40-02-PR. REMOVED AND REPLACED WITH NEW FROM STOCK MID FLOOR GUSSET FROM FR 38 TO FR 45 IAW EMB 145 SRM 51-40SDR HNAA2026030400181Floor Support · corrodedFLOOR SILL FROM FR 35 TO FR 39, LH, HAS CORROSION. REMOVED AND REPLACED FLOOR SILL FROM FR 35 TO FR 39 LH. REF EMB145 SRM 51-40-02.SDR REXA2026030200154Door · cracked"LH FWD OVERWING EXIT DOOR HAS A SUSPECTED CRACK COMING OUT OF A PREVIOUS REPAIR STRIPPED THE FINISH OF THE SUSPECTED CRACK ON THE LH FWD OVER-WING EXIT DOOR IAW CRJ900 SRM 51-26-01-001-001-A01 RESTORED SURFACE FINISH AT REWORKED AREA IAW CRJ900 SRM 51-25-06-0SDR FDEA202601310110Computer · failedISSUE WITH FMS, AUTOPILOT & FLT DIRECTOR. CLIMBING OUT OF SCL, IN VNAV/LNAV, RECEIVED A CLIMB VIA CLEARANCE FROM ATC. ACFT LEVELED OFF AT 9000 AT SEKSE, IAW DONTI5B SID OFF OF 17L. ACFT WENT INTO VNAV PATH AS ANTICIPATED. ONCE PAST SEKSE, ACFT WENT INTO TO SDR IPXA2026022369212Skin · crackedLT WING FIXED L/E UPPER COMPOSITE SKIN HAS CRACKS UNDER SLAT NR 4. EVALUATED LT WING FIXED L/E UPPER COMPOSITE SKIN UNDER SLAT NR 4. FOUND OUT OF LIMITS, IAW SRM 57-41-01-1A-1, TABLE 1 FIGURE 101 ACCOMPLISHED REPAIR PER EO-96538-REQ1 AND VT-MAE EA 757-5741-SDR SWIA2026022375302Flap Track · damagedRIGHT FLAP TRACK 2A OTBD HAS MAX WIDTH REDUCTION DAMAGE OF 1.35MM WITH FLAPS EXTENDED. NOT WITHIN REPAIRABLE LIMITS. REMOVED AND REPLACED RT 2A OTBD FLAP TRACK IAW AMM 57-54-25.SDR SWIA2026013175301Flap Track · damagedRIGHT FLAP TRACK 1 OTBD HAS MAX WIDTH REDUCTION DAMAGE OF 1.12MM WITH FLAPS EXTENDED. NOT WITHIN REPAIRABLE LIMITS. REMOVED AND REPLACED RT FLAP TRACK 1 OTBD IAW AMM 57-54-25.SDR SWIA2026022375300Flap Track · damagedLEFT FLAP TRACK 2A OTBD HAS MAX WIDTH REDUCTION DAMAGE OF 1.26MM WITH FLAPS EXTENDED AND RETRACTED. NOT WITHIN REPAIRABLE LIMITS. REMOVED AND REPLACED LT 2A OTBD FLAP TRACK IAW AMM 57-54-25SDR REXA2026022300060Crossbeam · corrodedLEFT BS 280 CROSSBEAM CORRODED ON UPPER FLANGE BETWEEN BL 0 - LBL 11. REMOVED CORROSION ON THE CROSSBEAM IAW SRM 51-21-06-001-001-A01, DEEP PITTING IN ONE LOCATIONS WHERE UP TO 100% MATERIAL LOSS WAS FOUND. DUE TO THE EXTENT OF CORROSION, THE CROSSBEAM REQUIRESDR REXA2026022300058Crossbeam · corrodedRIGHT BS 280 CROSSBEAM CORRODED ON UPPER FLANGE BETWEEN BL 0 AND RBL 11. REMOVED SACRIFICIAL STRIP FROM FS 280 LB11 TO RBL11 TO GET ACCESS IAW SRM 51-42-06-001-001-A01. INSTALLED SAME SERVICEABLE SACRIFICIAL STRIP FROM FS 280 LBL 11 TO RBL 11 IAW SRM 51-42-06