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 NX422026022700009Crankcase · gougedUPON DISASSEMBLY FOR ITS FIRST OVERHAUL, DAMAGE WAS FOUND ON THE LEFT HAND CRANCASE TO ONE THRU STUD LOCATION. THE DAMAGE APPEARS TO BE A GOUGE WITH DISPLACED METAL JUST UNDER THE CYLINDER PAD INSIDE THE THRU STUD BORE. SIMILAR DAMAGE ON OTHER ENGINES WAS PREVSDR FDEA202602240286Slider · dirtyL FWD ENTRY DOOR SLIDE LIGHT WILL NOT ILLUMINATE AND PLASTIC COMPONENT FELL OUT OF DOOR. RELEASED FOR SERVICE PER MEL 52-11-01-A, CATEGORY B. REMOVED LOWER SLIDE COVER AND PERFORMED OPS CHECK OF GIRT BAR...FOUND GIRT BAR SLIDER FILTHY, CONTAMINATED WITH EXSDR DALA2026022701386Oxygen Mask · deployedCREW DEPLOYED O2 MASKS AND ALL O2 GENERATORS DEPLOYED WITH THE EXCEPTION OF LAVATORIES. FWD TO 46 EA NON-ROUTINES FOR GEN REPLACEMENT, MASK CLEANING AND REINSTALL. (LP# 8036172, MSI# 2026-00141)SDR AALA202602274497Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN SEAT TRACK AT FR 43 AND -Y1292. REPLACED SEAT TRACK PER SRM 51-42-11-801.SDR AALA202602270238Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN SEAT TRACK BETWEEN FR 45 AND FR 46 AT Y1292. REPLACED SEAT TRACK PER SRM 51-42-11-801.SDR SWAA2026022673941Flashlight Assy · no testAFT LEFT FLASHLIGHT WILL NOT TEST. REMOVED AND REPLACED AFT LEFT EMERGENCY FLASHLIGHT, BATTERY, AND MOUNTING BRACKET. OPS CHECKED GOOD. ALL WORK PERFORMED IAW AMM 25-64-00.SDR SWAA2026022673555Door · crackedLEFT MLG CENTER DOOR CRACKED AT FWD SUPPORT ROD FITTING, REMOVED CENTER AND INNER DOOR IAW MM 32-13-11, OK TO CONT REF AUTH 307366. OK TO CONT PER CDL 32-10-3XC SP1B. INSTALLED L/H MLG CENTER DOOR PER AMM 32-13-11.SDR SWAA2026022673937Sign · brokenCREW REPORTS CEILING EMERGENCY EXIT SIGN BROKEN. REMOVED & REPLACED CEILING EMERGENCY EXIT SIGN ASSY IAW AMM 33-51-01.SDR SWAA2026022673797Battery Pack · inoperativeLEFT MID EMERGENCY LIGHTS AISLE, OVERWING ESCAPE LIGHT, & OVERWING ESCAPE GROUND ILLUMINATION LIGHT INOPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-06-960-805.SDR SWAA2026022673795Light · inoperativeL/H EXTERIOR AFT SLIDE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-04-960-801.SDR SWAA2026022673942Skin · delaminatedLEFT WING INBOARD FLAP APPEARS TO BE DELAMINATED. C/W EA 26-157-00528SDR ANCF202602264006Switch · abnormalHYD Y RSR LO LV - IAW AMM 29-13-41-000/400-004-A, REV 76, THE LOW LEVEL SWITCH OF THE YELLOW HYDRAULIC RESERVOIR WAS REPLACED, TEST SATISFACTORY WITH ENGINE RUN-UP AMM 71-00-00-710-003-B REV.SDR DALA2026022601375Rib · damagedDURING REPAIR OF LOG 8456712 FOUND HINGE RIB 1, HINGE RIB 2,AND LWR CLOSURE RIB DAMAGED. WILL REQUIRE REPLACEMENT. REPAIR WORK COMPLIED WITH PRI 632577-14 REV 2. FINAL ERA 632577- 14 REV, ORIGINAL MATCHES. ALL RII'S COMPLIED WITH LEAK CK + OPS CK GOOD. (LP# 84SDR ASAA2026022463555Lamp · inoperativeFWD FLIGHT ATTENDANT LAV SMOKE RED LIGHT ON THE CEILING IS INOP. GROUNDED - YES. RELAMPED FWD FA LAV SMOKE LIGHT OPS CHECK GOOD. OK FOR SVC.SDR IPXA2026022667301Flap · damagedNR 17 LEFI DAMAGED. PERFORMED GVI ON #17 LEADING EDGE FLAP. QUALITY CONTROL IS OKAY TO INSTALL AT THE DISCRETION OF MAINTENANCE.SDR DALA2026022601368Engine · odorON TAXI OUT AFTER BOTH ENGINES RUNNING PILOTS NOTIFIED AN ODOR THEN CONFIRMED WITH FLIGHT CREW THROUGH THE AIRCRAFT. PERFORMED T/S PER TSM A350 21-21-XX-54001-421A-A. UPON RUNNING THE NBR 1 ENG, AN OIL ODOR WAS DETECTED. INSPECTED ENG AND AREA NO LEAK NOTED. PSDR AALA202602261905Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO VERTICAL STABILIZER AFT DRAG BRACE FITTING AT WL 301, RBL 10. REPLACED FITTING PER SRM 53-80-90-0I.SDR AALA202602265928Seat Track · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN SEAT TRACK AT FR 39 AND +Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.SDR DALA2026022601360Oxygen Mask · unwanted deployOXYGEN PANEL MASK DEPLOYED / LOCATION:207: R & R LATCH ASSY OF OXY CONTAINER AT LAV 207 REF A330 CMM 35-22-40 AND A330 35-21. OPS CHECK GOOD. (1465051)SDR CALA2026022614114Mount · unsecureR1 WINDOW, LOUD WIND NOISE & WHISTLE FROM TAKEOFF ROLL TO 5000 FT AND 250. DEBRIEFED FLT CREW, LOUD SOUND STARTED AT 100 KNOTS & GREW LOUDER UNTIL 5000FT, STOPPED IN CLIMB. ACFT PRESSURIZED TO A DELTA P OF 2, FOUND TOO LOUD TO CONTINUE FLT. CREW COULDN`TSDR CALA2026022614101Floor Support · crackedMAIN CABIN BS 328-400 BL-0 FLOOR SUPPORT CRACKED. REMOVED AND REPLACED CRACKED FLOOR SUPPORT IAW DWG 143A5300, REV - AND SRM 51-40-02.SDR CALA2026022614099Floorbeam · corrodedCORROSION - FWD WET AREA FLOORBEAM TEE WITH SURFACE CORROSION SPOTS AT BS 294.5 RBL 18 & RBL 28. AT BS 294.5 UPPER CHORD CORROSION BETWEEN RBL 18 AND RBL 28 FOUND OUT OF LIMITS, REPAIR MAIN CABIN FWD WET AREA FLOOR BS 294.5 BETWEEN RBL25 - LBL21 IAW SRM 53-10SDR CALA2026022614098Adiru · faultedON CLIMBOUT CAPTS PFD LOST AIRSPEED.ALTITUDE. AND HDG. STAYED GONE FOR 10-15 MINS THEN RETURNED. AFTER LRU HISTORY REVIEW, LT AOA SENSOR HAS NUMEROUS REMOVALS FOR THE SAME ISSUES, ACCOMPLISHED WIRE CHECKS IN FUP 8025635, REF SSM 34-21-13-102.1, 34-21-14-101SDR CALA2026022614096Battery Pack · no testPOWER SUPPLY M1670 BATTERY FAILED TEST REMOVED AND REPLACED EMERGENCY BATTERY PACK M1670 IAW BOEING AMM 33-51-06-960-805. OPS CHECK SATISFACTORY.SDR CALA2026022614094Floorbeam · corrodedMAIN CABIN LEFT AFT WET AREA FLOOR BEAM UPPER FLANGE CORRODED AROUND LAV MOUNT AT BS 947 LBL23. ALL MAINTENANCE COMPLETED UP TO SFR INPUT. PERFORMED PERMANENT REPAIR AT FLOOR BEAM UPPER FLANGE BS 947 IAW SRM 53-70-51-2R-5.SDR CALA2026022614092Tie Down · corrodedL1 DOOR TIE DOWN FITTING AT STA 312 HAS EXFOLIATING CORROSION REF AAR N/R 100007609. REMOVED AND REPLACED FITTING L1 DOOR FWD AT STA 312 IAW SRM 51-40-02-0G -0, AND AIPC 53-42-00-29. LOGPAGE 8010828 ESFR ENTERED. REMOVED AND REPLACED FITTING L1 DOOR FWD AT SDR CALA2026022614090Intercostal · corrodedAFT CARGO COMP, BTW STA 1360-1380, S27R, INTERCOSTAL ANGLE WITH CORROSION.REF NR 1336679. PARTS FABRICATED PER DWG 146N4512-4, 146N5213-1, 146N5213-1, AND 654N0244-226. REMOVED (1) INTERCOSTAL, (1) FITTING (1) CHORD (1) CLIP, (2) SHE ANTIE, (3) FILLERS, IAW SRSDR CALA2026022614088Floorbeam · corrodedFLOORBEAM BTW BL 0 - RBL 24.75, BS 333.45, CORRODED. REPAIR FABRICATED IAW DWG 141N5160, REV D. REMOVED AND REPLACED, REMOVED 100%, EXFOLIATED BS 333.45 BTW BL 0 - RBL 24.75, APPLIED TREAT AND PRIMER IAW IAW SRM 51-20-01 ; APPLIED TOP COAT IAW AMM 51-21-15SDR CALA2026022614086Closeout Panel · corrodedMAIN CABIN,FLOOR STRUCTURE RH AFT WET AREA, CLOSE OUT WEB UPPER SKIN HAS CORROSION AT SEVERAL SPOTS AND RUNNING UNDER AFT GALLEY FLOOR SUPPORT FITTINGS (2EA), BS987-BS1006. REMOVED AND REPLACED CLOSE OUT WEB IAW DWG 147A5701, REV A, AND SRM 51-40-02.SDR CALA2026022614084Closeout Panel · corrodedMAIN CABIN LEFT AFT WET AREA CLOSE OUT WEB UPPER SURFACE CORRODED AT BS 1006 TO 986 BETWEEN LBL 23 AND LBL 37. REMOVED AND REPLACED THE CLOSE OUT WEB AT MAIN CABIN LH AFT WET AREA.SDR CALA2026022614082Light · failedEMERGENCY FLOOR LIGHTS FROM 30FED TO 35FED ALL DIM WITH A BURNING ODOR IN SURROUNDING AREA. 31F - FLOOR PROXIMITY EMERGENCY LIGHT FOUND TO BE DAMAGED AND BURNED OUT AND EXPLAINS BURNING ODOR IN SURROUNDING AREA. LIGHT ASSY REPLACED IAW CMM 25-23-52. OPS TEST CSDR CALA2026022614080Battery · no testDURING CIDS EMERGENCY LIGHT TEST. PERFORMED BITE OF 13WL IAW 33-51-00-810-802-A, BATTERY FAULT ACTIVATED. R & R THE BATTERY AT 13WL, OPS TEST PASSED IAW TSM 33-51-00-810-802A, AMM33-51-38-000-002.SDR CALA2026022614070Power Supply · no testDURING TEST OF THE EMERGENCY LIGHTS, EPSU UNIT FWD L MESSAGE WAS SHOWN ON PROGRAMMING AND TEST PANEL. REMOVED AND REPLACED THE ESPU & BATTERY IAW AMM 33-51-38-400-002-A, AND 33-51-38-400-001-A. TEST PASSED.SDR ASAA2026022464529Elec Connector · disconnectedWHILE PERFORMING T/C 32-010-00, FOUND EMERGENCY LIGHT OVERHEAD OF ROW 1 INOPERATIVE. GROUNDED - YES. FOUND EMERGENCY AISLE LIGHT CONNECTOR DISCONNECTED, PERFORMED GVI OF CONNECTORS FOUND NO DAMAGE OR BROKEN PARTS. RECONNECTED CONNECTORS PERFORMED OP CHECK, OP SDR SWAA2026022573948Counter · odorELECTRICAL ODOR COMING FROM FO YOKE TRIP COUNTER. REMOVED AND REPLACED FO'S TRIP COUNTER IAW MM 33-11-00.SDR DALA2026022501352Camshaft · wornL2 DOOR DIFFICULT TO OPEN. REMOVED THE DOOR LINER & NOTICE OVER CENTER IS OFF. REMOVED LINER, DOOR HANDLE & COVER. FOUND LOWER GUIDE ARM ROLLER WORN. REMOVED IAW AMM 52-11. FOUND COUNTERBALANCE ROLLER WORN, REMOVED IAW AMM 52-11. R & R ROLLER YOKE IAW AMSDR DALA2026022501347Skin · corrodedFUSELAGE EXTERNAL SKIN & INTERNAL SKIN DOUBLER AT THE WASTE SERVICE PANEL CUTOUT, BS 1540 - 1560, S27 - 29R CORRODED. REPAIRED IAW ERA 632028-14. (1465593)SDR DALA2026022501346Frame · corrodedAFTER WASTE PANEL REMOVAL. CORROSION WAS FOUND ON FUSELAGE FRAME, BTW S29R - 28R, BS 1540, OUT OF LIMITS IAW SRM 53-00-07-1A, PROCEDURE 1, AD 1 NOTE B, DETAIL II, NDT MANUAL PART. 4 51-00-10 PROCEDURE 2. THE FRAME WEB AT BS 1540, S28 - 29R REPAIRED IAW ESDR DALA2026022501344Skin · dentedDENT ON EXTERNAL SKIN LOCATED AT FR 3 & 19 INCHES BELOW RH STRINGER, LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON THE SKIN IAW SRM 53-11-11-300-041, STEP 2.A, FIGURE 001.SDR AALA202602252538Flashlight · no testAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT FORWARD CABIN FLASHLIGHT BLINKING RED. REMOVED AND REPLACED BATTERY IN FORWARD FLIGHT ATTENDANT FLASHLIGHT. PER AMM 25-64-00.SDR AALA202602256389Handle · inoperativeAIRCRAFT WAS NOT GROUNDED: LAVATORY-D DOOR DOES NOT OPEN PROPERLY. REMOVED AND REPLACED DOOR HANDLE ON LAVATORY-D DOOR OPS CK GOOD. PER CMM 25-40-64.SDR AALA202602256738Screw · looseAIRCRAFT WAS NOT GROUNDED: LAVATORY-D DOOR WILL NOT OPEN ALL THE WAY. SECURED UPPER TRACK SCREWS. OPS CHECK NORMAL.SDR AALA202602256504Flap System · stuckAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: WHEN EXTENDING THE FLAPS, TRAILING EDGE FLAPS STUCK ASYMMETRICAL BETWEEN 0 AND 1 WITH LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO AND LANDED SAFELY AT TPA. (OPEN).SDR AALA202602250435Circuit Breaker · trippedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: AFTER TAKEOFF BOTH SPAR VALVE CLOSED LIGHTS ILLUMINATED BRIGHT AND CIRCUIT BREAKERS B3 AND B4 BEHIND FO SEAT BOTH POPPED. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT ORD. FOUND CIRCUIT BREASDR FDEA202602240277Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231NFF MDC FLOOR PANEL 231NFF MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 93.SDR FDEA202602240276Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231QFF MDC FLOOR PANEL 231QFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 93.SDR FDEA202602240275Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 251QFF MDC FLOOR PANEL 251QFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 93.SDR FDEA202602240274Floor Panel · puncturedPUNCTURE ON 251PFF FLOOR PANEL OF MAIN CARGO COMPARTMENT FLOOR PANEL 251PFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 SHEET 2 REV. 93 AUG 15-2025SDR FDEA202602240273Skin · delaminatedDELAMINATION IN LEADING EDGE AT 69" INNER END ON OUTBOARD FLAP, RH WING LEADING EDGE AT 69 " INNER END ON OUTBOARD FLAP, RH WING WAS REPAIRED IAW B767 SRM 57-53-01-2R FIGURE 201 SHEET 5 PAG 5 AND B767 SRM 51-70-17-0G PAR 4 A FIGURE 10 SHEET 1, REV 93.SDR FDEA202602240272Skin · delaminatedDELAMINATION IN LEADING EDGE AT 50" OF INBOARD FLAP SUPPORT FAIRING ON OUTBOARD FLAP, RH WING LEADING EDGE AT 50" OF INBOARD FLAP SUPPORT FAIRING ON OUTBOARD FLAP RH WING WAS REPAIRED IAW B767 SRM 57-53-01-2R FIGURE 201 SHEET 5 PAG 5 AND B767 SRM 51-70-17-