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 DALA2026030401511Charger · inoperativeFOUND 4L AND 4R DOORS WITH ONE EACH EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED M736 BATTERY CHARGER AND BATTERY PER B 757 AMM 33-51.MFG PN ON/OFF 2012-1. (8242701)SDR DALA2026030401510Indicator · inoperative4R DOOR KNUCKLE BUSTER NOT ARMING. RESEATED KNUCKLE BUSTER & CLEANED DEBRIS OK FOR SVC 4R DOOR PER B757 AMM 52-11. (8584738)SDR DALA2026030401507Fuse · failedINTERIOR SEAT MOUNTED EMERGENCY LIGHTS INOP ROWS 1-4. FOUND & REPLACED 1 BAD FUSE ON M731 POWER SUPPLY PER B757 AMM 33-51 REPLACED M731 POWER SUPPLY. DISCREPANCY CORRECTED. (8584735)SDR DALA2026030401506Angle · brokenBROKEN FWD CLIP OF GIRT BAR L4. FWD CLIP OF GIRT BAR L4 WAS REPLACED PER ER/A 622462-14 REV. A SECTION II. (1477554)SDR DALA2026030401505Snubber · out of toleranceOUT OF LIMITS PIN EXTENSION ON ROTARY SNUBBER AT 4 RH DOOR. THE ROTARY SNUBBER WAS REMOVED PER AMM 52-11-10 AND INSTALL SERVICEABLE ROTARY SNUBBER UNDER AMDS 5211-6005-4R. (1477637)SDR DALA2026030401503Power Supply · inoperativeROW 30AB-37AB EMERGENCY LIGHTS INOP. T/S & FOUND ESPU (15WL) FAULTS. R/R ESPU REF A330 AMM 33-51. OK FOR SERVICE. (8351622)SDR DALA2026030401495Door Sill · corrodedFWD CARGO DOOR LOWER SILL SURFACE COVERED BY PLATES, FOUND SURFACE CORROSION NEAR 4 ATTACH SCREWS. (M/P) REF AMDS CARD 5321 -2015 FIG 2 AREA 4. SSI 53-21-25-02. NO PREVIOUS REPAIRS IN AREA NOTED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ASDR DALA2026030401494Skin · corrodedAFT SERVICE DOOR SKIN UNDER SCUFF PLATE, COUNTERSINK HOLES 2OL, 3OL, 4OL, 5OL, 8OL, 9OL, 10OL, 11OL, 12OL AND 13OL HAVE CORROSION IN COUNTERSINKS AND ADJACENT TO COUNTERSINKS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATIOSDR DALA2026030401493Floor Panel · corrodedCORRODED FLOOR PANEL SUPPORT BETWEEN RBL 23 AND RBL 43.2 AT FR 76. REMOVED DAMAGED SUPPORT AND INSTALLED NEW FLOOR SUPPORT AT FR 76 -78 RBL 39" IAW BOMBARDIER DRAWING# PL C01342700 AND A220ASRP BD500-A-J51-42-06-00AAA-078A-A. (LP# 1477333)SDR UIEA2026030300076Cooling Fan · failedE/E COOLING SUPPLY FAN STATUS MSG, ACCOMPANIED WITH ELECTRICAL BURNING ODOR IN THE FLT DECK. R & R THE E/E COOLING SUPPLY FAN IAW AMM 21-58-01 & IPC 21-58-01-01, ITEM 200. E & E COOLING GROUND TEST PASSED IAW AMM 21-58-00.SDR AALA202603041519Fan · seizedAIRCRAFT WAS GROUNDED: VENT BLOWER FAULT ECAM CAME ON DURING CLIMB, 25 MINUTES AFTER TAKE OFF. FLIGHT CREW ACCOMPLISHED ECAM PROCEDURE-BLOWER TO OVERRIDE-ECAM CLEARED, NO STATUS MESSAGES OTHER THAN PREVIOUS MEL MESSAGES. FLIGHT CREW REPORTED THEY NOTICED SLIGSDR AALA202603049998Smoke Detector · false activationAIRCRAFT WAS NOT GROUNDED: THE FLIGHT CREW REPORTED THAT WHILE AT CRUISE THEY RECEIVED AN AFT LAVATORY SMOKE WARNING ECAM THAT ONLY LASTED FOR ABOUT 2 SECONDS AND DISAPPEARED. THE FLIGHT ATTENDANTS INVESTIGATED AND FOUND ALL LAVATORIES WERE FREE OF SMOKE. THESDR AALA202603046214Fitting · lack of lubeAIRCRAFT WAS NOT GROUNDED: L4 ARMING DOOR LEVER DOES NOT STAY DISARMED (UP). SLOWLY FALLS DOWN. MAINTENANCE REPOSITIONED GIRT BAR INTO FLOOR FITTING & LUBRICATED FLOOR FITTINGS IAW AMM 25-62-44. A SATISFACTORY OPS CHECK OF THE L4 DOOR ARMING SYSTEM ACCOMPLISSDR AALA202603041528Elec Connector · disconnectedAIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT ON SEAT 22C IS INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR FOR THE EMERGENCY LIGHT UNPLUGGED AT THE LIGHT HOUSING, CONNECTED THE ELECTRICAL CONNECTOR AND ACCOMPLISHED A SATISFACTORY OPS CHECK OF THE EMERGENCY LIGHTINSDR SCNA20260304108Fitting · crackedLOWER FUSELAGE, MAIN WHEEL WELL, BS 727, LBL 16 - 49, FUEL LINE FITTING CRACKED, FOUND DURING PERFORMANCE OF ITEM 1-23. REPLACED FUEL FEED LINESHROUD DRAIN AT LOWER FUSELOAGE MAIN WHEEL WELL STA 727 FROM LBL16 TO LBL 49 IAW B737-/00 AMM TASK 20-50-11-910-81SDR DALA2026030401482Wire Harness · damagedSEAT ROW 24 A/B EMERGENCY LIGHTS INOPERATIVE. WIRE GOING FROM SIDEWALL TO LIGHT ASSY CONNECTOR SEPARATED. RE-TERMINATED THE SEAT 24 AB WIRE HARNESS AT WALL IAW ESPM 20-10-13. OPS CKD GOOD. (8257974)SDR DXTA2026030407101Wire Splice · damagedWHILE CLOSING THE MAIN CABIN DOOR, THE HANDLE MOVES FREELY DOESN'T FEEL LIKE THE CAMS ARE ENGAGING. THE HANDLE ALSO WILL MOVE TO THE OPEN POSITION WITHOUT PRESSING THE RED BUTTON. AND THE DOOR OPEN LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED FAULTY MED CLSDR DXTA2026030407103Latch Pin · lack of lubeMAIN PASSENGER DOOR, RED EICAS MESSAGE DISPLAYED. THE VISUAL TWO TOP GREEN LINES DO NOT LINE UP. PIC'S INCLUDED. ALSO NOTED, AOG MAIN CABIN DOOR NOT ALIGNING TO SHUT. CLEANED AND LUBRICATED THE LATCH PINS. COMPLIED WITH MUTIPLE MAINENTRANCE DOOR OPS CHECKSSDR EVCA202603030002Unknown · odorCREW SMELLED ELECTRICAL BURNING WHEN HEATER WAS TURNED ON. COULD NOT DUPLICATE ON GROUNDSDR QR9R2026030300001Sensor · fluctuatesIN FLIGHT, GENERATOR AMP NR 1 AT 30-35 %, GEN AMP NR 2 FLUCTUATES 10-25 %. REMOVED AND REPLACED NR 2 CURRENT SENSOR IAW AMM 24-30-00, 4-6.SDR AALA202603036865Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL AT STA 727J AND RBL 30. REPAIRED PER SRM 53-00-53-2R-5.SDR FDEA202603030306Light · inoperativeWHEN ARMING THE SLIDES FOR DEPARTURE, RT SLIDE LIGHT DID NOT ILLUMINATE. RELEASED FOR SERVICE IAW MEL 25-66-04-B, CATEGORY C. VERIFIED SLIDE ARMED LT DOES NOT ILLUMINATE WHEN R1 DOOR SLIDE IS ARMED. PERFORMED GVI OF R1 DOOR ESCAPE SLIDE GIRT BAR, SKIRT & LSDR JR2R20260303391Fitting · crackedRH W/W AILERON QUADRANT FITTING CRACKED. REPLACEDSDR 2026F00020Skin · crackedEXTERIOR FUSELAGE SKIN ONLY IS CRACKED AT ONE FASTENER HOLE LOCATED L1 DOOR CUT OUT AFT CORNER STA 335 JUST ABOVE STR 20L(VERIFIED WITH HFEC).REPAIRED EXTERIOR FUSELAGE SKIN CRACK AT ONE FASTENER HOLE LOCATED L1 DOOR CUT OUT, AFT CORNER, STA 335 JUST ABOVE STRSDR SIMA20260303001Seat Track · corrodedDURING PASSENGER SEAT REMOVAL FOR HEAVY CHECK INSPECTION, FOUND LEFT INBOARD SEAT TRACK TO BE CORRODED BETWEEN FRAMES 19-20. (MAJOR REPAIR) (LEVEL 2 CORROSION). REPAIRED SEAT TRACK IAW ERS EJ-53MR-5374.SDR DALA2026030301442Bracket · damagedTOOLING DAMAGE ON BRACKET FWD SIDE OF C 23 P3 TO P4. REPAIRED PER ERA 632611-14 REV ORIG. (1476403)SDR DALA2026030301441Skin · dentedFUSELAGE SKIN BETWEEN FR 34-35, BELOW S31R DENTED. PERFORMED THE PERMANENT DOUBLER REPAIR ON DENTED AREA. AT EXTERNAL FUSELAGE SKIN C34-C35A AND S30R -S33R IAW ER/A 625812-14, REV B. (1476731)SDR DALA2026030301438Selector Valve · faultedDE - DUE TO NLG STEERING ECAM MSG WITH ASSOCIATED FAULT LIGHT. REPLACED NWS SELECTOR VALVE. OK FOR SERVICE. (8491487)SDR AALA202603032590Skin · crackedAIRCRAFT IN BASE MAINTENANCE. CRACK IN THE FUSELAGE SKIN AT APU DOOR FWD HINGE POINT, BS 1104. ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-80-01-2R-1.SDR SWIA2026030277336Skin · damagedREPAIR RT INBOARD FLAP LOWER SKIN DUE TO MULTIPLE DISCREPANCIES. C-CHECK RO 9302026RH IB FLAP LOWER SKIN HAS BEEN REPAIRED REF SRM 57-52-01-201-005-A01 REFER TO CONTINUATION SHEET FOR DETAILS COMPLIED WITH TASK CARD 51-900-1002-SKYSDR 2026FA0000774Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.SDR 2026FA0000773Bushing · defectiveTHE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.SDR CALA2026090119129Frame · dentedDENT ON FRAME AT BS 1340 NEAR S26R IN AFT CARGO BAY. ACCOMPLISHED INTERIM REPAIR IAW ECRA5360-02110 AND 757-5360-13-A4284, PART 1, STEP 1.SDR COEA2026072226803Channel · corrodedRT AILERON, MOVEABLE TRIM TAB CLOSEOUT CHANNEL HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED CHANNEL PER ATR72 SRM 51-25-03 REV. 122.SDR SWIA2026030275989Intercostal · mechanic errorINTERCOSTAL AT FS 533 BETWEEN STGR 26L-27 FOUND TO HAVE DOUBLE DRILLED HOLE. PERFOMED MAJOR REPAIR OF INTERCOSTAL AT FS 533 BETWEEN STGR 26L-27 IAW SRM 531-42-06-001-001-A01 REV. 38D AND REO 670-53-32-174 REV.--SDR U2RA202604280010Tension Tie · crackedOPEN-HOLE NDI INSPECTION FOUND DEFECT SIGNALS WHILE PERFORMING BS 1180LT - 1140 RT.SDR VNAA202604110012Skin · crackedCRACK AT AFT AREA OF PAX DOOR SKIN PANEL BELOW TOP STOW STEP. AFT AREA OF PAX DOOR SKIN PANEL BELOW TOP STOW STEP WAS REPAIRED PER CRJ-900 SRM 52-11-04-201-006-A01.SDR VNAA202604110011Door Frame · corrodedCORROSION ON MIDCAP OF PASSENGER DOOR SURROUND STRUCTURE BTW FS310.00 TO FS349.00 AND STGR 18LH. MIDCAP OF PASSENGER DOOR SURROUND STRUCTURE BTW FS310.00 TO FS349.00 AND STGR 18LH WAS EVALUATED AND THEREFORE IS OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-001-ASDR VNAA202604110009Insert · damagedCARGO PIT TAPE APPLIED - AFT LAV TOILET SHROUD RH POTTED INSERT DAMAGE 1. WITHIN 835 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. AFT LAV TOILET SHROUD AFT INSERT DAMAGSDR VNAA202604110008Inlet · wornWEAR ON AFT EDGE OF INLET COWL IN SETLEMENT AREA OF FAN COWL 3:00 O' CLOCK POSITION AT LH ENGINE. ON AFT EDGE OF INLET COWL IN SETLEMENT AREA OF FAN COWL 3:00 O' CLOCK POSITION AT LH ENG WAS REPAIRED PER REO 690-54-11-607 REV. - -SDR VNAA202604110007Insert · damagedCARGO PIT TAPE APPLIED - FWD LAV TOILET SHROUD FWD INSERT DAMAGE 1. WITHIN 1591 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT LOCATION IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. FWD LAV TOILET SHROUD FWD INSERT DAMAGESDR VNAA202604110006Bracket · brokenBROKEN UPPER BRACKET OF PYLON TIE-BAR APROX FS1069.75 AT RH PYLON INSTERNAL STRUCTURE. BRACKET OF PYLON TIE-BAR APROX FS1069.75 AT RH PYLON INSTERNAL STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 PAR. 6.C.SDR VNAA202604110005Skin · damagedLIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BETWEEN FS202.75 - FS613.00 WITHIN 6500FH, PERFORM A PERMANENT REPAIR IAW APPROVED PROCEDURES. LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BETWEEN FS202.75 - FS613.00 WERE REPAIRED PER CRJ-900 SRM 53-00-00-201-003-A03 ANDSDR U2RA2020405000005Web · crackedCRACK FOUND ON FORWARD FUSELAGE WEB OF NOSE GEAR WELL AT STRINGER S-26 STA 140-160 WL 205 R&R WEB PART NUMBER 65B01870U243 IAW SRM 51-40-02SDR SWAA2026033175992Crossbeam · crackedCRACKED CROSSBEAM, BS 540, LBL 44, WL 208. REMOVED AND REPLACED CROSSBEAM, BS 540, LBL24 - 45, WL 208, IAW SRM 51-40-02, & DWG 143A5240, REV -.SDR SWAA2026033175999Seat Track · corrodedCORROSION ON SEAT TRACK LBL 45, BS 480+17, BS 500+8, BS 500A+8, BS 500B+18. THE SEAT TRACK WILL BE REPLACED ON FAULT TTG8Q01AR96P.SDR SWAA2026033075902Floor Support · crackedCRACKED INTERCOSTAL AT BS 380-400 RBL 8 WL 208. REMOVED AND REPLACED INTERCOSTAL AT BS 380-400 RBL 8 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 143A5400 SHEET 38 REV A.SDR SWAA2026033075893Strap · corrodedCORROSION ON STRAP AT BS 1018 RBL3 WL 208<[01] REMOVED; FABRICATED AND INSTALLED NEW TENSION STRAP BS 1006 - BS11028 RBL3 WL 208 I.A.W SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND BOEING DWGS 147A5730 REV: C; 147A5744 REV: B; PL 147A5744 REV: E.SDR SWAA2026033075903Intercostal · crackedCRACKED INTERCOSTAL AT BS 380-400 LBL 13 WL 208. NOT ALLOWABLE LIMITS FOUND THEREFORE SRM 51-10-02-0G-0 PAR 9.C REMOVE AND REPLACEMENT OF THE PART IS APPLICABLE; REMOVED CRACKED INTERCOSTAL AT BS 380-400 LBL 13 WL 208 PER SRM 51-40-02; OK TO INSTALL NEW INTESDR SWAA2026033075904Intercostal · crackedCRACKED INTERCOSTAL AT BS 380-400 BL 0 WL 208. NOT ALLOWABLE LIMITS FOUND THEREFORE SRM 51-10-02-0G-0 PAR 9.C REMOVE AND REPLACEMENT OF THE PART IS APPLICABLE; REMOVED CRACKED INTERCOSTAL AT BS 380-400 BL 0 WL 208 PER SRM 51-40-02; LOCATED AND DRILLED NEW IN