N41104
Service difficulty reports · 66
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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' WHERE n_number = 'N41104' AND registry_match = 'registration' 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' WHERE n_number = 'N41104' AND registry_match = 'registration' 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 RAIA2019101590002Bracket · bindingDISCREPANT CONDITION: DURING A DEPARTMENT OF DEFENSE SCHEDULED AUDIT IT WAS FOUND THAT THE FORWARD LEFT HAND PORTABLE BREATHING EQUIPMENT CONTAINER WAS DIFFICULT TO REMOVE FROM ITS DESIGNED CASE MOUNTING BRACKET.THE BRACKET INSTALLED DIDN'T ALLOW FOR THE PBE TSDR RAIA2019082310001Light · inoperativeLEFT AFT WING TO FUSLAGE FAIRING EXTERIOR FLOOD LIGHT NR 5 WAS INOPERATIVE. R & R LEFT OVERWING EMERGENCY LIGHT. OPS CHECKED GOOD.SDR RAIA2019040850001O-Ring · failedBLEED 1 LEAK CLIMBING THROUGH 11K FT. NO VISIBLE MOISTURE... FOUND LEAKS AT SENSORS 15,17 AND 9. REPLACED O-RINGS AT LOCATIONS 15,17 AND 9. LEAK CHECK GOOD AT THIS TIMESDR RAIA201903260001O-Ring · damagedBLEED LEAK 1 IN FLIGHT. FOUND LEAKING DUCT AT AFT BULKHEAD FWD OF APU FIREWALL. R2 O-RING LEAK AND OPS CHECK GOOD.SDR RAIA201903170001Hydraulic Line · damagedENGINE 1 HYD SYSTEM FAILURE WITH ASSOCIATED MESSAGES. INSPECTED NR 1 EDP, HYD HOSE DAMAGED. R&R'D SYSTEM NR 1 PRESSURE(PUMP) HOSE OPS AND LEAK CHECK GOOD.SDR RAIA2018122200001A/C Pack · overtempPACK 2 OVERHEAT WITH BURING SMELL IN COCKPIT. COMPLIED WITH STEPS 5 BLOCK 1, 2, AND 12 OF EIM TGASK. COMPLED WITH BLOCK 2 STEPS 1 AND 2 WITH BOTH ENGINES AT TAKE OFF POWER. MESSAGE AND BURNING SMELL NOT DUPLICATED. TRANSITORY CONDITION PER BLOCK 12. OPS CHECKSDR RAIA201707110001Light · crackedEMERGENCY LIGHT STRIP IS CRACKED ACROSS FROM SEAT 2A. R & R THE LIGHT STRIP, OPS CHECK GOOD.SDR RAIA201602010001Light · inoperativePAX DOOR EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. R & R PAX DOOR EMERGENCY FLOOD LIGHT. OPS CHECKED GOOD.SDR RAIA201601060002Power Supply · inoperativeNR 11 MAIN DOOR EXIT MARKER LIGHT IS INOPERATIVE. R & R NR1 BATTERY POWER SUPPLY. OPS CHECK GOOD.SDR RAIA201601060001Power Supply · inoperativeNR 1 MAIN DOOR EXTERIOR FLOOD LIGHT ON BOTTOM SIDE OF THE PLUG DOOR HINGE IS INOPERATIVE. R & R NR 1 BATTERY POWER SUPPLY. OPS CHECK GOOD.SDR RAIA201512230001Proximity Switch · inoperativeNOSE GEAR DOOR DID NOT CLOSE AFTER GEAR RETRACTION, 1 MAIN GEAR POSSIBLY DOWN DURING CLIMB, RETURNED TO BLOCK. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR FWD DOOR PROXIMITY SWITCH, PERFORMED GEAR SWING AND OPS CHECK GOOD. RETURNED TO SERVICE.SDR RAIA201505270001Bleed Valve · failedAPU BLEED VALVE FAILED MESSAGE FOLLOWED BY APU FAILED MESSAGE ON EICAS, APU INDICATED 28V ON BUSS, ACFT RETURNED TO BLOCKS. REPLACED THE BLEED VALVE, OPS CHECKED GOOD.SDR ASOA20131231144RConnector · unsecureTHE CENTER OVERHEAD EMERGENCY EXIT LIGHT ABOVE ROW 18 WAS REPORTED INOPERATIVE. MX SECURED CONNECTOR ON SIGN AND OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20131230143Panel · inoperativeTHE CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT SIGN WAS REPORTED INOPERATIVE. MX R & R THE LIGHT PANEL ASSY WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20121003130Power Supply · inoperativeDURING MX INSPECTION, AN OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA11IA004Warning Message · false activationDURING CLIMB, THE CREW RECEIVED AN AUTOPILOT FAIL MESSAGE ON THE EICAS DISPLAY. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED SYS AND OPS CHECKS, HOWEVER THE CONDITION COULD NOT BE DUPLICATED NOR DID THE INDICATION ILLUMINASDR ASOA20111120004Aoa · burnedACFT WAS ENROUTE WHEN LIGHTNING STRUCK ACFT CAUSING A BURNING ODOR IN THE CABIN. THE CREW LANDED SAFELY. MX COMPLIED WITH A LIGHTNING STRIKE INSPECTION IAW AMM2 5-50-01. R & R THE NR 2 AOA VANE IAW AMM 27-36-01. OPS CHECKED GOOD AND WAS RELEASED.SDR C2XA11CL210Light · inoperativeCORRECTED SDR FOR A/C 41104 NEW NUMBER: DURING ROUTINE MAINTENANCE THE RIGHT EXTERNAL FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.SDR C2XA11CL209ALight · inoperativeDURING ROUTINE MAINTENANCE THE RIGHT EXTERNAL FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.SDR C2XA11TY016Engine · malfunctionedTYS - A/C WAS EN ROUTE FROM IAH TO IND WHEN THE CREW REPORTED A HAZY SMOKE IN CABIN, AFTER LANDING MOSTLY IN THE AFT CABIN. LANDING WAS NORMAL AND NO ICIAS INDICATIONS. A/C WAS FERRIED TO TYS WHERE THE NR 2 ENGINE WAS REMOVED AND REPLACED IAW EMB 145XR AMM-7SDR C2XA11CL032Engine · contaminatedMHT FLT 2635 - THE CREW REPORTED SMOKE IN THE CABIN, COCKPIT AFTER TAKEOFF. ALSO RECEIVED A LAV SMOKE MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO MHT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND RESIDUAL DEICE FLUID IN THE ENGINESSDR C2XA11SH031Attach Bracket · damagedSHV - DURING C-CHECK LT AILERON I/B HAT BUSHING OF O/B ATTACHMENT POINT OF PCA IS MIGRATED. REPLACED ATTACHMENT BRACKET IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11SH030Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 48-49. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-21-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11CL007Coffeemaker · contaminatedTHE CREW REPORTED A BURNING SMELL IN THE GALLEY. MAINTENANCE INSPECTED AND FOUND PLASTIC DEBRIS ON THE NR 2 COFFEE POT. REMOVED DEBRIS AND OPERATIONAL CHECKS WERE GOOD.SDR C2XA10RI130Panel · inoperativeFLIGHT 3009 - EWR - FLIGHT CREW REPORTED LAV SMOKE TEST INOPERATIVE. EWR MX REMOVED AND REPLACED LAV SMOKE PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA10IA249Switch · defectiveIAH - FLIGHT 2020, THE CREW REPORTED A BLEED ONE OVERTEMP IN ICING CONDITIONS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TEMP SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WASDR C2XA10CL041Smoke Detector · failedDURING ROUTINE MAINTENANCE THE AFT CARGO SMOKE DETECTOR FAILED THE TASK CARD 26-15-01-212-001-A00 OPERATIONAL CHECKS. MAINTENANCE REPLACED THE SMOKE DETECTOR AND OPERATIONAL CHECKS WERE GOOD.SDR C2XA09IA288AProximity Switch · inoperativeIAH - FLIGHT 2365, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL AND E1-2 TR DISAGREE MESSAGES IN CRUISE. WHEN EXTENDING THE LANDING GEAR ON APPROACH, ALL MESSAGES CLEARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RESDR C2XA09TY165Sill · corrodedSERVICE DOOR SILL CORRODED AT SCREW HOLES. BLENDED MINOR CORROSION IAW SRM 51-10-03, RESTORED FINISH.SDR C2XA09TY164Skin · dented2 DENTS, LT FUSELAGE BETWEEN FR 19 AND 20. REPAIRED DAMAGE IAW IC2009-145/04712. REFINISHED SURFACE IAW CPM51-21-07, EC5330-01937.SDR C2XA09TY162Floor Support · corrodedACFT IN C-CHECK WHEN THE INBD SIDE OF THE LT OMEGA BEAM WAS FOUND CORRODED AT FR 54 THRU FR 58. MX BLENDED THE SURFACE CORROSION IAW SRM 51-10-03 AND ALODINED, PRIMED AND PAINTED IAW CPM 51-21-07. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF SDR C2XA09TY160Sill · corrodedACFT IN C-CHECK AND THE RT FLOOR SILL AT FR 36 THRU FR 42 WAS FOUND CORRODED. MX REMOVED AND REPLACED THE FLOOR SILL IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR C2XA09TY159Sill · corrodedACFT IN C-CHECK AND THE RT FLOOR SILL FROM FR 42 THRU FR 48 WAS FOUND CORRODED. MX REMOVED AND REPLACED THE FLOOR SILL IAW SRM 51-40-02 AND CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR C2XA09TY158Sill · corrodedACFT IN C-CHECK AND THE RT FLOOR SILL AT FRAME 33 THRU FRAME 34 WAS FOUND CORRODED. MX BLENDED OUT THE CORROSION, FOUND TO BE WITHIN LIMITS. ALLODINED, PRIMED AND PAINTED IAW SRM 51-10-03 AND SRM 51-21--04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASSDR C2XA09TY157Sill · corrodedAIRCRAFT IN C-CHECK STATUS AND THE LT FLOOR SILL AT FRAME 32 THRU FRAME 33 WAS FOUND CORRODED. MX REMOVED AND REPLACED THE FLOOR SILL IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR C2XA09TY155Skin · gougedACFT CURRENTLY IN A C-CHECK STATUS WHEN INSP FOUND A GOUGE ON THE PAX DOOR AFT SIDE LWR EDGE. MX MEASURED, BLENDED AND INSTALL A DOUBLER OVER THE DAMAGED AREA. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR C2XA09TY166Sill · corrodedRT FLOOR SILL CORRODED AT FRM 50. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-23-10, RESTORED FINISH.SDR C2XA09TY154Sill · corrodedLT FLOOR SILL CORRODED AT FRM 47. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02.SDR C2XA09TY153Sill · corrodedLT FLOOR SILL AT FRM 32-33 HAS CORROSION. REMOVED AND REPLACED SILL IAW SRM 51-40-02.SDR C2XA09TY151Shear Tie · crackedSHEAR CLIP HAS A CRACK AT FR 81 AND STR 10L. REMOVED AND REPLACED CRACKED SHEAR CLIP IAW SRM 51-40-02.SDR C2XA09TY138Skin · dentedFUSELAGE DENTED AT FRM 28, STR 13R. REPAIRED BY CUTTING OUT DAMAGED AREA, FABRICATED FILLER AND INSTALLED DOUBLER IAW EC5330-01936. AIRCRAFT STILL IN C-CHECK.SDR C2XA09TY137Sill · corrodedLT FLOOR SILL CORRODED AT FRAME 47. REMOVED AND REPLACED FLOOR SILL.SDR C2XA09TY136Sill · corrodedLT FLOOR SILL IS CORRODED AT FRM 49. REMOVED AND REPLACED FLOOR SILL.SDR C2XA09TY135Sill · corrodedAFT GUSSET IN GALLEY AREA CORRODED. THE AFT GUSSET WAS REMOVED AND REPLACED.SDR C2XA09TY133Sill · corrodedTYS - AIRCRAFT CURRENTLY IN A C-CHECK STATUS AND INSPECTION FOUND THE RT FLOOR SILL FROM FR 53 TO FR 59 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB 145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RETURNED TO SERVICE AT THE END OSDR C2XA09TY134Sill · corrodedTYS - AIRCRAFT IN C-CHECK STATUS AND INSPECTION FOUND THE LT FLOOR SILL AT FR 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB 145XR SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR C2XA09IA145AController · inoperativeTHE CREW REPORTED A WINDSHIELD HEAT FAIL MESSAGE ON EICAS. THE ACFT DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. MX PLACEDTHE WINDSHIELD HEAT ON MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. ON 06/05/09 MX REMOVED AND REPLACED THE NR 2 WINDSHIELD HEAT CSDR C2XA09TY104Warning System · malfunctionedTYS - AIRCRAFT EN ROUTE FROM IAH TO ORF WHEN THE WINDSHIELD HEAT FAIL. AIRCRAFT DIVERTED TO BNA AND SWAPPED AIRCRAFT TO 192. MAINTENANCE COULDN'T DUPLICATE PROBLEM ON GROUND WHEN PRESSURIZED. PLACED ON MEL. MEL 2473864.SDR C2XA08IA251Engine · smokeIAH - FLIGHT 2160, THE FLIGHT ATTENDANT REPORTED THAT A HAZE DEVELOPED IN THE CABIN FOLLOWED BY A MOMENTARY LAV SMOKE INDICATION. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX R&R THE NR 2 ENGINE, OPS CHECKED WITH NO DEFECTS, AND THE ACFT WASSDR C2XA08RI177Control Panel · defectiveFLIGHT 2966 - EWR - FLIGHT CREW REPORTED LAVATORY SMOKE INDICATION ON EICAS DURING CLIMBING WITH A SLIGHT SMELL OF SMOKE. CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR PANEL AND PERFORMED OPERATION
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