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 AALA202602054807Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: CIDS PANEL CAUTION. MAINTENANCE SERVICED THE R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.SDR AALA202602054678Bottle · low pressureAIRCRAFT WAS GROUNDED: CIDS PANEL DISPLAYS CHECK DOOR PRESSURE MESSAGE FOR DOOR 1L. MAINTENANCE SERVICED THE L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AND THE MESSAGE EXTINGUISHED.SDR FDEA202602040132Repair · no discrepancyEXISTING REPAIR ON MDCC CROSSBEAM AT FR55 BETWEEN Y1456 AND Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR55 BETWEEN Y1456 AND Y1959 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5310-70959 A. THE REPAIR IS CATEGORY SDR FDEA202602040129Bulb · failedDURING MX PRE-FLIGHT, FOUND L1 OVERHEAD EMERGENCY EXIT SIGN DIM. AMM: 33-51-01-2 REMOVED AND REPLACED 12 FAULTY BULBS IN THE L1 OVERHEAD EMERGENCY EXIT SIGN AS PER ABOVE REF. OPS CHECK GOOD. A/C OK FOR SERVICE.SDR FDEA202602040128Valve · faultedWHILE PERFORMING OPS CHECK OF ELCTROHYDRAULIC VALVE 3GA REPLACEMENT WRI 5-25/4268. THE NOSE GEAR RETRACTED.SDR CALA2026020513592Skin · damagedNR 10 L/E SLAT UPPER SURFACE DISBONDED & MISSING, CAT 2, METALLIC PARTS BETWEEN 15 & 150 SQ/IN, SLAT REMOVAL COMPLETE UP TO PART E SECT 8 IAW AMM 27-81-15-000-801. SLAT REMOVAL COMPLETE AS IAW AMM 27-81-15-000-801, NR 10 SLAT INSTALLATION CARRIED OUT IAW AMM RSDR CALA2026020413586Battery · no testCIDS1 EPSU SYS TEST FAILED. CLASS 1, BAT/EPSU(16WL) OWD R. REMOVED AND REPLACED 16WL EPSU BATTERY REF AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS TESTS GOOD. FAULT NO LONGER PRESENT.SDR ASAA2026020464113Battery Pack · no testOUTBOARD AFT LEFT HAND OVERWING AND LOWER AFT WING LIGHTS FAILED CAPACITY TEST. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK M1670 AT LEFT SIDEWALL CARPET RISER, OPS TESTED GOOD IAW AMM 33-51-06-960-805.SDR ASAA2026020464112Battery Pack · no testOUTBOARD OVERWING AFT RIGHT AND LOWER AFT WING LIGHTS FAILED CAPACITY TEST. GROUNDED - YES. REPLACED BATTERY PACK (M1671) AND OPS CHECKED GOOD IAW 33-51-06-960-805.SDR IXXA2026020400001Skin · delaminatedRIGHT WING O/B FLAP LOWER SURFACE TRAILING EDGE HAS A DENT AND DELAMINATION THAT REQUIRES COMPOSIT REPAIR.SDR DALA2026020400822Seat Track · corrodedSEAT TRACK, MID CABIN FOUND CORRODED AT -Y1552.5, FR 35-37. REPAIRED IAW ERA 631636-14, REV ORIGINAL. (1434900)SDR DALA2026020400821Seat Track · corrodedSEAT TRACK, LT AFT CABIN FOUND CORRODED AT FR 74, Y794.3. REPAIRED IAW ERA 631634-14, REV ORIGINAL. (1434888)SDR DALA2026020400820Seat Track · corrodedSEAT TRACK, AFT CABIN AT FR 74 - 75, - Y794.3 FOUND CORRODED. REPAIRED IAW ERA 631644-14, REV ORIGINAL. (1434808)SDR DALA2026020400819Seat Track · corrodedSEAT TRACK, AFT CABIN FOUND WITH CORROSION AT FR 74 -Y1137.1. REPAIRED IAW ERA 631637-14, REV ORIGINAL. (1434795)SDR DALA2026020400818Seat Track · corrodedLEFT AFT CABIN SEAT TRACK FOUND WITH CORROSION AT FR 74 Y1137.1. REPAIRED IAW ERA 631635-14, REV ORIGINAL. (1434784)SDR JR2R20260204409Shear Tie · corrodedWHILE PREPPING FOR OK TO CLOSE BULHEAD FOUND SHEAR TIE AT FR85 BETWEEN STRI28R TO STR27R CORRODED. REMOVED AND REPLACEDSDR AALA202602041150Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: R3 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.SDR AALA202602041031Slide · defectiveAIRCRAFT WAS NOT GROUNDED: DURING A SCHEDULED REPLACEMENT OF THE L4 DOOR SLIDE, MAINTENANCE FOUND THE REPLACEMENT SLIDE WAS BAD FROM STOCK, ROUTED THE DEFECTIVE SLIDE TO BE SENT OUT FOR REPAIR AND RE-INSTALLED THE ORIGINAL SLIDE PER AMM 25-62-44.SDR IXXA2026020404Bracket · corrodedLEFT WING T/E FRONT SECTION OF LANDING GEAR SUPPORT BEAM HAS CORRODED PANEL SUPPORT BRACKETSDR IXXA2026020403Bracket · corrodedLOWER FUSELAGE WING TO BODY PANEL SUPPORT BRACKET HAS CORROSION AT WIRING CLAMP HOOKUP BETWEEN LEFT WHEEL WELL AND GEARSDR IXXA20260204003Support · brokenLW T/E PANEL SUPPORT BROKEN. FOR 561ABSDR 4GIA8G9R0106201Angle · crackedRIGHT WING IN PNL 841-20 DOUBLER BEHIND VERTICAL ANGLE HAS 3/4 INCH LONG CRACK FS 434 BL 51SDR DALA2026020400815Oil System · leakingMULTI EVENTS OF SMOKE/FUMES-ON ARRIVAL INTO AUA THROUGHOUT AC, ON DEPT AUA IN BACK OF AC, ON ARRIVAL BOS FRONT OF AC. ROWS 17-25 MOST PREDOMINANT. FA'S REPORT HARSH CHEMICAL SMELL, IRRITATION, HEADACHE. PILOTS DID NOT HAVE ANY CONTACT. FOUND OIL INSIDE #2 ENSDR FDEA202602040127Stringer · damagedREMOVE EXISTING REPAIR AT STA 1656 ON STRINGER 26L REPAIRED STRINGER SECTION AT BS 1640 11" TO BS1660 10" STR 26L, IAW B757 SRM 53-00-03-2R, FIG 201, DETAIL I AND B757 SRM 51-40-02-0GSDR FDEA202602040126Floor Panel · damagedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 241WFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 241WFF, MPN: 145T5876-51, RBL 11- LBL 11, STA 1114.82-984.95 IN REF. TO BOEING DWG 145T5876-51, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MSDR FDEA202602040125Controller · faultedAT FLIGHT LEVEL 370 GOT AN ECAM DUE TO HIGH CABIN PRESSURE, SHORTLY AFTER THAT THE NR 2 PRESSURE REGULATOR FAULTED, DONED OXYGEN MASKS STARTED A DECENT AND RAN THE ECAM. ALL PRESSURE REGULATING VALVES SHOWED CLOSED ON ECAM. THE CABIN PRESSURE CONTINUED TO CLISDR FDEA202602040124Floorboard · damagedFLOORBOARD 241AGF IS DAMAGED. FABRICATED NEW FLOOR PANEL 241AGF, MPN: 145T5874-31, RBL 77.50 - RBL 89.50, STA 984.95-1087 IN REF. TO BOEING DWG 145T5874-31, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR.SDR FDEA202602040123Floor Panel · damagedFLOOR PANEL 242MFF IS DAMAGED. FABRICATED NEW FLOOR PANEL 242MFF, RBL 74.25"- RBL 86.25", STA 933- 984.95 IN REF. TO BOEING DWG 145T5876-21. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PANEL WILL BE ACCOMPLISHED ON WO# SDR FDEA202602040122Floorboard · damagedFLOORBOARD 241QFF IS DAMAGED. FABRICATED NEW FLOOR PANEL 241QFF, LBL 77.50"- LBL 89.50", STA 933- 984.95 IN REF. TO BOEING DWG 145T5876-15. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PANEL WILL BE ACCOMPLISHED ON WO# SDR FDEA202602040121Floor Panel · damagedFLOORBOARD 242LFA IS DAMAGED. FABRICATED NEW FLOOR PANEL 242LFA, MPN: 145T5874-18, RBL 54.75- RBL 74.25, STA 930-972 IN REF. TO BOEING DWG 145T5874-18. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PANEL WILL BE ACCOMPLISSDR FDEA202602040120Slide · brokenR1 DOOR SLIDE ASSEMBLY HAS BROKEN BATTERY HARD SHELL. RELEASED FOR SERVICE PER MEL: 52-11-01-01, CATEGORY: C. R1 DOOR ESCAPE SLIDE INOP. SLIDE REMAINS INSTALLED ON DOOR. REMOVED AND REPLACED R1 DOOR SLIDE IAW AMM 25-61-22-04-01. OPS CHECKS GOODSDR IXXA20260204001Support Angle · crackedMCD AFT SEAL SUPPORT ANGLE CRACKED.SDR ABXA20260204048Heater · inoperativeDURING TAXI OUT, RT WINDOW HEAT INOPERATIVE. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED RT SIDE WINDOW NR 2 HEAT SYS EPR MEL ABX-30-41-1-2. PLACRAD INSTALLED. ACFT REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.SDR DALA2026020400812Clamp · looseATB - DUE TO ENG 2 FIRE LOOP B FAULT FOLLOWED BY ENG 2 FIRE ECAM WARNING. FOUND HP AND IP VALVE CLAMPS LOOSE. RESECURED CLAMPS.(LP: 77020558)SDR DALA2026020400811Actuator · failedDIV - TO JFK DUE TO A L/G GEAR NOT UPLOCKED AND L/G DOORS NOT CLOSED ECAM WARNINGS DURING GEAR RETRACTION. MAINTENANCE STILL IN PROGRESS. (LP: 8182810)SDR IXXA2026020402Skin Splice · crackedLW LE SKIN SPLICE PLATE IS CRACKED AT OFSS 500SDR IXXA2026020401Frame · crackedNUMBER 2 ENGINE OUTBOARD CORE COWL INTERNAL UPPER L/E STRUCTURE HAS CRACKSDR 2026FA0000082Skin · not reportedCENTER WING, UPPER SKIN ,AT STR-U17, LBL 90.SDR 2026FA0000081Window Frame · corrodedRIGHT WINDOW FRAME BETWEEN BS 544 AND 566, CORRODED.SDR 2026FA0000080Window Frame · corrodedRIGHT WINDOW FRAME BETWEEN BS 522 AND 544, CORRODED.SDR 2026FA0000079Window Frame · corrodedRIGHT WINDOW FRAME BETWEEN BS 500 AND 520, CORRODED,SDR 2026FA0000078Bear Strap · not reportedUPPER BEAR STRAP, FWD LARGE CARGO DOOR, BS 478, S20R,SDR 2026FA0000077Skin · not reportedCENTER WING, UPPER SKIN BETWEEN STR1C AND AT BS 955 AND BETWEEN BL 0 - BL 11.06,SDR 2026FA0000076Failsafe · crackedBS 955, S22L, LT FAIL SAFE STRAP ,SB 767-53A0100, A CRACK WAS FOUND ON THE LOWER HOLE OF THE LT FAIL SAFE STRAP.SDR 2026FA0000075Failsafe · crackedSEC 45 BS 955 S22R, RIGHT FAIL SAFE STRAP, SB 767-53A0100, CRACK FOUND ON THE LOWER HOLE OF THE RIGHT FAIL SAFE STRAP.SDR SWIA2026020376869Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA94171-670-53-11-2025 MXCODEID104885-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 94171TEMP REPAIR FOR DENT DAMAGE TO CANOPY SKIN PANEL BETWEEN FS247.30-FS254.68 STR1R-STR2R (ON RH SIDE) IS VALID FOR 2700 FH FROM THE TIMSDR 2026FA0000483Door Latch · bentRCP LH DOOR HANDLE PUSH ROD IS BENT. REMOVED AND REPLACED RCP L/H DOOR HANDLE PUSH ROD. NO DEFECTS NOTED.SDR VNAA20260511011Floorbeam · corrodedF.S.280 LOWER WEB IS CORRODED ON EDGE AT LBL 11 BETWEEN CORROSION CAP AND DOOR POST. REPLACED LH FS 280 CROSS BEAM WITH NEW, P/N CC670-34094-1S IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01.SDR SWIA2026020375885Floor Support · damagedDURING FLOOR SUPPORT REPAIR AT RBL 9 BETWEEN BS 409.5 & 409 + 32 FOUND UNDERLYING DAMAGE ON FLOOR. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06 AND SRM 53-00-43. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR VNAA202603130002Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DAT