# Service difficulty reports: N41104 A list on [N41104](https://openairdocs.org/aircraft/N41104.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 66 reports - [SDR RAIA2019101590002](https://openairdocs.org/sdr/RAIA2019101590002.md): Bracket · binding · Oct 9, 2019 · N41104 · Emb EMB145XR · Emergency Equipment > DISCREPANT 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 T - [SDR RAIA2019082310001](https://openairdocs.org/sdr/RAIA2019082310001.md): Light · inoperative · Aug 21, 2019 · N41104 · Emb EMB145XR · Emergency Lighting > LEFT AFT WING TO FUSLAGE FAIRING EXTERIOR FLOOD LIGHT NR 5 WAS INOPERATIVE. R & R LEFT OVERWING EMERGENCY LIGHT. OPS CHECKED GOOD. - [SDR RAIA2019040850001](https://openairdocs.org/sdr/RAIA2019040850001.md): O-Ring · failed · Apr 5, 2019 · N41104 · Emb EMB145XR · Pneumatic Distribution System > BLEED 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 TIME - [SDR RAIA201903260001](https://openairdocs.org/sdr/RAIA201903260001.md): O-Ring · damaged · Mar 26, 2019 · N41104 · Emb EMB145XR · Pneumatic Distribution System > BLEED LEAK 1 IN FLIGHT. FOUND LEAKING DUCT AT AFT BULKHEAD FWD OF APU FIREWALL. R2 O-RING LEAK AND OPS CHECK GOOD. - [SDR RAIA201903170001](https://openairdocs.org/sdr/RAIA201903170001.md): Hydraulic Line · damaged · Mar 17, 2019 · N41104 · Emb EMB145XR · Hydraulic System, Main > ENGINE 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 RAIA2018122200001](https://openairdocs.org/sdr/RAIA2018122200001.md): A/C Pack · overtemp · Dec 20, 2018 · N41104 · Emb EMB145XR · Cabin Cooling System > PACK 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 CHECK - [SDR RAIA201707110001](https://openairdocs.org/sdr/RAIA201707110001.md): Light · cracked · Jul 11, 2017 · N41104 · Emb EMB145XR · Emergency Lighting > EMERGENCY LIGHT STRIP IS CRACKED ACROSS FROM SEAT 2A. R & R THE LIGHT STRIP, OPS CHECK GOOD. - [SDR RAIA201602010001](https://openairdocs.org/sdr/RAIA201602010001.md): Light · inoperative · Feb 1, 2016 · N41104 · Emb EMB145XR · Emergency Lighting > PAX DOOR EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. R & R PAX DOOR EMERGENCY FLOOD LIGHT. OPS CHECKED GOOD. - [SDR RAIA201601060002](https://openairdocs.org/sdr/RAIA201601060002.md): Power Supply · inoperative · Jan 6, 2016 · N41104 · Emb EMB145XR · Emergency Lighting > NR 11 MAIN DOOR EXIT MARKER LIGHT IS INOPERATIVE. R & R NR1 BATTERY POWER SUPPLY. OPS CHECK GOOD. - [SDR RAIA201601060001](https://openairdocs.org/sdr/RAIA201601060001.md): Power Supply · inoperative · Jan 6, 2016 · N41104 · Emb EMB145XR · Emergency Lighting > NR 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 RAIA201512230001](https://openairdocs.org/sdr/RAIA201512230001.md): Proximity Switch · inoperative · Dec 23, 2015 · N41104 · Emb EMB145XR · Landing Gear Position and Warning > NOSE 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 RAIA201505270001](https://openairdocs.org/sdr/RAIA201505270001.md): Bleed Valve · failed · May 27, 2015 · N41104 · Emb EMB145XR · APU Bleed Air System > APU 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 ASOA20131231144R](https://openairdocs.org/sdr/ASOA20131231144R.md): Connector · unsecure · Dec 31, 2013 · N41104 · Emb EMB145XR · Light System Wiring > THE 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 ASOA20131230143](https://openairdocs.org/sdr/ASOA20131230143.md): Panel · inoperative · Dec 30, 2013 · N41104 · Emb EMB145XR · Emergency Lighting > THE 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 ASOA20121003130](https://openairdocs.org/sdr/ASOA20121003130.md): Power Supply · inoperative · Oct 3, 2012 · N41104 · Emb EMB145XR · Emergency Lighting > DURING 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 ASOA11IA004](https://openairdocs.org/sdr/ASOA11IA004.md): Warning Message · false activation · Nov 22, 2011 · N41104 · Emb EMB145XR · Autopilot System > DURING 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 ILLUMINA - [SDR ASOA20111120004](https://openairdocs.org/sdr/ASOA20111120004.md): Aoa · burned · Nov 20, 2011 · N41104 · Emb EMB145XR · Stall Warning System > ACFT 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 C2XA11CL210](https://openairdocs.org/sdr/C2XA11CL210.md): Light · inoperative · Sep 18, 2011 · N41104 · Emb EMB145XR · Emergency Lighting > CORRECTED 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 C2XA11CL209A](https://openairdocs.org/sdr/C2XA11CL209A.md): Light · inoperative · Sep 18, 2011 · N41104 · Emb EMB145XR · Emergency Lighting > 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 C2XA11TY016](https://openairdocs.org/sdr/C2XA11TY016.md): Engine · malfunctioned · Feb 16, 2011 · N41104 · Emb EMB145XR · Engine (Turbine/Turboprop) > TYS - 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-7 - [SDR C2XA11CL032](https://openairdocs.org/sdr/C2XA11CL032.md): Engine · contaminated · Feb 2, 2011 · N41104 · Emb EMB145XR · Engine (Turbine/Turboprop) > MHT 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 ENGINES - [SDR C2XA11SH031](https://openairdocs.org/sdr/C2XA11SH031.md): Attach Bracket · damaged · Jan 30, 2011 · N41104 · Emb EMB145XR · Ailerons > SHV - 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 C2XA11SH030](https://openairdocs.org/sdr/C2XA11SH030.md): Floor Support · corroded · Jan 30, 2011 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > SHV - 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 C2XA11CL007](https://openairdocs.org/sdr/C2XA11CL007.md): Coffeemaker · contaminated · Jan 7, 2011 · N41104 · Emb EMB145XR · Buffet/Galleys > THE 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 C2XA10RI130](https://openairdocs.org/sdr/C2XA10RI130.md): Panel · inoperative · Oct 15, 2010 · N41104 · Emb EMB145XR · Smoke Detection > FLIGHT 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 C2XA10IA249](https://openairdocs.org/sdr/C2XA10IA249.md): Switch · defective · Sep 8, 2010 · N41104 · Emb EMB145XR · Pneumatic Indicating System > IAH - 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 WA - [SDR C2XA10CL041](https://openairdocs.org/sdr/C2XA10CL041.md): Smoke Detector · failed · Mar 3, 2010 · N41104 · Emb EMB145XR · Smoke Detection > DURING 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 C2XA09IA288A](https://openairdocs.org/sdr/C2XA09IA288A.md): Proximity Switch · inoperative · Nov 10, 2009 · N41104 · Emb EMB145XR · Landing Gear Position and Warning > IAH - 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 RE - [SDR C2XA09TY165](https://openairdocs.org/sdr/C2XA09TY165.md): Sill · corroded · Jul 15, 2009 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > SERVICE DOOR SILL CORRODED AT SCREW HOLES. BLENDED MINOR CORROSION IAW SRM 51-10-03, RESTORED FINISH. - [SDR C2XA09TY164](https://openairdocs.org/sdr/C2XA09TY164.md): Skin · dented · Jul 15, 2009 · N41104 · Emb EMB145XR · Fuselage Main, Plate/Skin > 2 DENTS, LT FUSELAGE BETWEEN FR 19 AND 20. REPAIRED DAMAGE IAW IC2009-145/04712. REFINISHED SURFACE IAW CPM51-21-07, EC5330-01937. - [SDR C2XA09TY162](https://openairdocs.org/sdr/C2XA09TY162.md): Floor Support · corroded · Jul 15, 2009 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > ACFT 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 C2XA09TY160](https://openairdocs.org/sdr/C2XA09TY160.md): Sill · corroded · Jul 15, 2009 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > ACFT 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 C2XA09TY159](https://openairdocs.org/sdr/C2XA09TY159.md): Sill · corroded · Jul 15, 2009 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > ACFT 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 C2XA09TY158](https://openairdocs.org/sdr/C2XA09TY158.md): Sill · corroded · Jul 15, 2009 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > ACFT 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 RELEAS - [SDR C2XA09TY157](https://openairdocs.org/sdr/C2XA09TY157.md): Sill · corroded · Jul 15, 2009 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > AIRCRAFT 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 C2XA09TY155](https://openairdocs.org/sdr/C2XA09TY155.md): Skin · gouged · Jul 14, 2009 · N41104 · Emb EMB145XR · Passenger/Crew Doors > ACFT 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 C2XA09TY166](https://openairdocs.org/sdr/C2XA09TY166.md): Sill · corroded · Jul 13, 2009 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > RT FLOOR SILL CORRODED AT FRM 50. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-23-10, RESTORED FINISH. - [SDR C2XA09TY154](https://openairdocs.org/sdr/C2XA09TY154.md): Sill · corroded · Jul 13, 2009 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > LT FLOOR SILL CORRODED AT FRM 47. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02. - [SDR C2XA09TY153](https://openairdocs.org/sdr/C2XA09TY153.md): Sill · corroded · Jul 13, 2009 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > LT FLOOR SILL AT FRM 32-33 HAS CORROSION. REMOVED AND REPLACED SILL IAW SRM 51-40-02. - [SDR C2XA09TY151](https://openairdocs.org/sdr/C2XA09TY151.md): Shear Tie · cracked · Jul 13, 2009 · N41104 · Emb EMB145XR · Fuselage Internal Mounting Structure > SHEAR CLIP HAS A CRACK AT FR 81 AND STR 10L. REMOVED AND REPLACED CRACKED SHEAR CLIP IAW SRM 51-40-02. - [SDR C2XA09TY138](https://openairdocs.org/sdr/C2XA09TY138.md): Skin · dented · Jul 4, 2009 · N41104 · Emb EMB145XR · Fuselage Main, Plate/Skin > FUSELAGE 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 C2XA09TY137](https://openairdocs.org/sdr/C2XA09TY137.md): Sill · corroded · Jul 1, 2009 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > LT FLOOR SILL CORRODED AT FRAME 47. REMOVED AND REPLACED FLOOR SILL. - [SDR C2XA09TY136](https://openairdocs.org/sdr/C2XA09TY136.md): Sill · corroded · Jul 1, 2009 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > LT FLOOR SILL IS CORRODED AT FRM 49. REMOVED AND REPLACED FLOOR SILL. - [SDR C2XA09TY135](https://openairdocs.org/sdr/C2XA09TY135.md): Sill · corroded · Jul 1, 2009 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > AFT GUSSET IN GALLEY AREA CORRODED. THE AFT GUSSET WAS REMOVED AND REPLACED. - [SDR C2XA09TY133](https://openairdocs.org/sdr/C2XA09TY133.md): Sill · corroded · Jun 29, 2009 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > TYS - 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 O - [SDR C2XA09TY134](https://openairdocs.org/sdr/C2XA09TY134.md): Sill · corroded · Jun 29, 2009 · N41104 · Emb EMB145XR · Fuselage Miscellaneous Structure > TYS - 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 C2XA09IA145A](https://openairdocs.org/sdr/C2XA09IA145A.md): Controller · inoperative · Jun 4, 2009 · N41104 · Emb EMB145XR · Windshield/Door Rain/Ice Removal > THE 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 C - [SDR C2XA09TY104](https://openairdocs.org/sdr/C2XA09TY104.md): Warning System · malfunctioned · Jun 4, 2009 · N41104 · Emb EMB145XR · Windshield/Door Rain/Ice Removal > TYS - 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 C2XA08IA251](https://openairdocs.org/sdr/C2XA08IA251.md): Engine · smoke · Dec 11, 2008 · N41104 · Emb EMB145XR · Engine (Turbine/Turboprop) > IAH - 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 WAS - [SDR C2XA08RI177](https://openairdocs.org/sdr/C2XA08RI177.md): Control Panel · defective · Dec 3, 2008 · N41104 · Emb EMB145XR · Smoke Detection > FLIGHT 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 Next page: https://openairdocs.org/aircraft/N41104/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N41104/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.