# Service difficulty reports: N11127 A list on [N11127](https://openairdocs.org/aircraft/N11127.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 · 60 reports - [SDR RAIA2020021520001](https://openairdocs.org/sdr/RAIA2020021520001.md): Engine · odor · Feb 12, 2020 · N11127 · Emb EMB145XR · Engine (Turbine/Turboprop) > SMOKE IN CABIN AT ROW 3 AND AFT CABIN. COMPLIED WITH FIM AND FOUND NO EVIDENCE OR SMELL ANY BURNT. RAN ENGINES AND APU WITH PACKS ON. NO SMELL OR SMOKE NOTED IN CABIN. AIRCRAFT OK FOR SERVICE. SECOND ATTEMPT, SAME FLIGHT NUMBER. F/A REPORTS SOMOE IN CAB - [SDR RAIA201909140001](https://openairdocs.org/sdr/RAIA201909140001.md): Mount Bracket · corroded · Sep 14, 2019 · N11127 · Emb EMB145XR · Fuselage Main, Attach Fittings > MOUNTING PLATE FOR THE RA #2 AFT ANTENNA ON AFT FUSELAGE SEPARATING FROM FUSELAGE. CLEANED SKIN AND FOUND NO CORROSION ON FUSELAGE ONLY RA MOUNTING BRACKET. NO MATERIAL REMOVED. CRACKS FOUND AROUND RIVET HOLES. SUPPLIMENTAL INFORMATION: FOUND CORROSION OF FUS - [SDR RAIA201909110001](https://openairdocs.org/sdr/RAIA201909110001.md): Skin · cracked · Sep 11, 2019 · N11127 · Emb EMB145XR · Fuselage Main, Plate/Skin > MOUNTING PLATE FOR RADIO ALTIMETER #2 FWD ANTENNA ON AFT FUSELAGE IS SEPARATING FROM THE AIRCRAFT. CORROSION FOUND BETWEEN MOUNTING PLATE AND SKIN OF FUSELAGE. NO CORROSION FOUND ON THE FUSELAGE ONLY MOUNTING PLATE. AFTER CLEANING CRACKS WERE FOUND ON THE FUSE - [SDR RAIA2018121440002](https://openairdocs.org/sdr/RAIA2018121440002.md): Support Bracket · gouged · Dec 4, 2018 · N11127 · Emb EMB145XR · Fuselage Main, Attach Fittings > L/H BLEED SYSTEM SUPPORT BRACKET IS GOUGED... REOMOVED AND REPLACED SUPPORT BRACKET... - [SDR RAIA2018121440001](https://openairdocs.org/sdr/RAIA2018121440001.md): Access Door · cracked · Dec 4, 2018 · N11127 · Emb EMB145XR · Doors > EXT POWER ACCESS DOOR IS CRACKED... REOMEVED AND REPLACED EXTERNAL POWER DOOR - [SDR RAIA201812142001](https://openairdocs.org/sdr/RAIA201812142001.md): Floor Support · damaged · Dec 2, 2018 · N11127 · Emb EMB145XR · Fuselage Miscellaneous Structure > LAV L/H FLOOR SUPPORT ASSY AT FR 60 IS DAMAGED... REMOVED AND REPLACED DAMAGED SUPPORT... - [SDR RAIA2018121430007](https://openairdocs.org/sdr/RAIA2018121430007.md): Door Frame · cracked · Nov 30, 2018 · N11127 · Emb EMB145XR · Fuselage Main, Structure > BAGGAGE DOOR FRAME AFT EXT FLANGE IS CRACKED AT BOTTOM END... REPAIRED BAGGAGE DOOR IAW ETD2018-145-129196 - [SDR RAIA2018121430006](https://openairdocs.org/sdr/RAIA2018121430006.md): Gusset · corroded · Nov 30, 2018 · N11127 · Emb EMB145XR · Fuselage Miscellaneous Structure > R/H FLOOR SUPPORT GUSSET BETWEEN FR 59-61 IS CORRODED.... REMOVED AND REPLACED GUSSET... - [SDR RAIA2018121430005](https://openairdocs.org/sdr/RAIA2018121430005.md): Gusset · corroded · Nov 30, 2018 · N11127 · Emb EMB145XR · Fuselage Miscellaneous Structure > L/H FLOOR SUPPORT GUSSET BETWEEN FR 59-61 IS CORRODED.... REMOVED AND REPLACED GUSSET... - [SDR RAIA2018121430004](https://openairdocs.org/sdr/RAIA2018121430004.md): Beam · corroded · Nov 30, 2018 · N11127 · Emb EMB145XR · Fuselage Main, Structure > LOWER CARGO ENTRY BEAM BETWEEN FR 65-68 IS CORRODED AROUND FASTNER HOLES... REMOVED AND REPLACED CARGO ENTRY BEAM... - [SDR RAIA2018121430003](https://openairdocs.org/sdr/RAIA2018121430003.md): Profile · bent · Nov 30, 2018 · N11127 · Emb EMB145XR · Fuselage Miscellaneous Structure > AFT "T" PROFILE AT FR 66 ON CARGO ENTRY RAMP IS BENT... REMOVED AND REPLACED "T" PROFILE... - [SDR RAIA2018121430002](https://openairdocs.org/sdr/RAIA2018121430002.md): Profile · bent · Nov 30, 2018 · N11127 · Emb EMB145XR · Fuselage Miscellaneous Structure > FWD "T" PROFILE AT FR 66 ON CARGO ENTRY RAMP IS BENT... REMOVED AND REPLACED "T" PROFILE... - [SDR RAIA2018121430001](https://openairdocs.org/sdr/RAIA2018121430001.md): Support · cracked · Nov 30, 2018 · N11127 · Emb EMB145XR · Cargo/Baggage Doors > BAGGAGE DOOR HOLD OPEN ROD SUPPORT IS CRACKED ON FR 68... REMOVED AND REPLACED BAGGAGE DOOR HOLD OPEN ROD SUPPORT... - [SDR RAIA2018121490002](https://openairdocs.org/sdr/RAIA2018121490002.md): Structure · corroded · Nov 29, 2018 · N11127 · Emb EMB145XR · Fuselage Miscellaneous Structure > AFT "U" SHAPE BETWEEN FR 18 AND FR19 AT PAX DOOR IS CORRODED... REMOVED AND REPLACED "U" SHAPE - [SDR RAIA201811290001](https://openairdocs.org/sdr/RAIA201811290001.md): Structure · corroded · Nov 29, 2018 · N11127 · Emb EMB145XR · Fuselage Miscellaneous Structure > FWD "U" SHAPE BETWEEN FR 18 AND FR19 AT PAX DOOR IS CORRODED... REMOVED AND REPLACED "U" SHAPE - [SDR RAIA201807260001](https://openairdocs.org/sdr/RAIA201807260001.md): Window · out of adjust · Jul 26, 2018 · N11127 · Emb EMB145XR · Flight Compartment Windows > F/O DV WINDOW W/N CLOSE. ADJUSTED FO'S DV WINDOW AND PERFORMED OPS CHECK. OPS CHECK GOOD AND NO DEFECTS NOTED AT THIS TIME. - [SDR RAIA201709150001](https://openairdocs.org/sdr/RAIA201709150001.md): Shutoff Valve · leaking · Sep 15, 2017 · N11127 · Emb EMB145XR · Pneumatic Distribution System > NR 2 BLEED LEAK EICAS MESSAGE. SECURED LEAK AT PRSOV VALVE, OPS CHECKED GOOD. - [SDR RAIA201709060002](https://openairdocs.org/sdr/RAIA201709060002.md): Container · torn · Sep 6, 2017 · N11127 · Emb EMB145XR · Emergency Locator Beacon > CAPTAIN`S LIFE VEST POUCH TORN. R & R THE LIFE VEST. - [SDR RAIA201709060001](https://openairdocs.org/sdr/RAIA201709060001.md): Flashlight · inoperative · Sep 6, 2017 · N11127 · Emb EMB145XR · Emergency Equipment > FIRST OFFICER`S FLASHLIGHT WAS INOPERATIVE. R & R THE FLASHLIGHT. OPS CHECKED GOOD. - [SDR RAIA201610310001](https://openairdocs.org/sdr/RAIA201610310001.md): Carbon Seal · leaking · Oct 31, 2016 · N11127 · Emb EMB145XR · Turbine Engine Oil System > OIL PRESSURE WENT INTO RED ON FINAL APPROACH. OIL ON NR 1 COWLING. R & R NR 1 ENGINE GENERATOR IAW AMM 24-31-01 AND CORRESPONDING CARBON SEAL WAS R & R IAW MM 72-63-10. NO LEAKS NOTED AT THIS TIME. OPS CHECKED GOOD. - [SDR ASOA20160310010](https://openairdocs.org/sdr/ASOA20160310010.md): Skin · dented · Mar 8, 2016 · N11127 · Emb EMB145XR · Fuselage Main, Plate/Skin > DENT IN ACFT SKIN FORWARD OF SERVICE DOOR AT FRAME 18, STR 11R AND AFT OF SERVICE DOOR BETWEEN FRAMES 23, 24 AND STR 12R, 13R. CUTOUT THE CREASES, FABRICATED AND INSTALLED FILLER AND EXTERNAL DOUBLER IAW EC5320-02092. - [SDR ASOA20160207005R](https://openairdocs.org/sdr/ASOA20160207005R.md): Acm · smoke · Feb 7, 2016 · N11127 · Emb EMB145XR · Cabin Cooling System > SMOKE WAS REPORTED IN COCKPIT. ACFT RETURNED TO GATE AND NR 1 PACK WAS PLACED ON MEL. MAINTENANCE R & R NR 1 ACM WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20150308059](https://openairdocs.org/sdr/ASOA20150308059.md): Door Sill · corroded · Mar 8, 2015 · N11127 · Emb EMB145XR · Fuselage Miscellaneous Structure > DURING C-CHECK THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140826108](https://openairdocs.org/sdr/ASOA20140826108.md): Unknown · odor · Aug 26, 2014 · N11127 · Emb EMB145XR · Air Distribution System > THE CREW REPORTED A STRONG OIL AND DIRTY PACK ODORS IN THE COCKPIT DURING DESCENT AND LANDING. LANDED WITHOUT INCIDENT, MAINTENANCE R & R THE NR 1 ENGINE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130312092](https://openairdocs.org/sdr/ASOA20130312092.md): Floor Support · corroded · Mar 12, 2013 · N11127 · Emb EMB145XR · Fuselage Miscellaneous Structure > DURING C-CHECK CENTER OMEGA BEAM CORRODED (LOCAL LEVEL 2) AT NUTPLATES AT FRAME 59-61. MX PERFORMED REPAIR OF CENTER OMEGA BEAM AT FRAME 59 IAW SRM 51-40-02 AND EC5310-01473. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130311091V](https://openairdocs.org/sdr/ASOA20130311091V.md): Floor Support · corroded · Mar 12, 2013 · N11127 · Emb EMB145XR · Fuselage Miscellaneous Structure > DURING C-CHECK RT OMEGA BEAM CORRODED (LOCAL LEVEL 2) AT NUTPLATES AT FRAME 59-61. MX PERFORMED REPAIR AND INSTALLED DOUBLER REPAIR AT RT OMEGA BEAM AT FRAME 60 IAW SRM 51-40-02 AND EC 5310-01473, REV ORIG. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130226090](https://openairdocs.org/sdr/ASOA20130226090.md): Floor Support · corroded · Mar 7, 2013 · N11127 · Emb EMB145XR · Fuselage Miscellaneous Structure > DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59-61. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01473. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130130008R](https://openairdocs.org/sdr/ASOA20130130008R.md): Charger · inoperative · Jan 30, 2013 · N11127 · Emb EMB145XR · Emergency Lighting > DURING MX INSPECTION, THE EMERGENCY EXIT LIGHT AT SEAT 2B WAS FOUND INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT BATTERY CHARGER AND BATTERY PACK WITH OPS CHECKS PERFORMED SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20121129144](https://openairdocs.org/sdr/ASOA20121129144.md): Engine · smoke · Nov 29, 2012 · N11127 · Emb EMB145XR · Engine (Turbine/Turboprop) > THE CREW REPORTED A LAVATORY SMOKE WARNING ON EICAS WITH SMOKE IN THE CABIN SEEMING TO COME FROM THE LIGHTS. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, R & R THE NR 2 ENGINE, AND THE ACFT WAS APPROVED FOR RETURN - [SDR ASOA2011121822013](https://openairdocs.org/sdr/ASOA2011121822013.md): Audio Panel · failed · Dec 18, 2011 · N11127 · Emb EMB145XR · Audio Integrating System > POST-FLIGHT CREW REPORTED CAPTAINS AUDIO PANEL INOPERATIVE AND THEN POPPED CIRCUIT BREAKER WITH ELECTRICAL ODOR IN COCKPIT. MX PERFORMED GVI AT CAPTAINS AUDIO PANEL WIRING AND R & R CAPTAINS DIGITAL AUDIO PANEL WITH OPS CHECK SUCCESSFUL AND NO FURTHER ELECTRI - [SDR ASOA2011112001001](https://openairdocs.org/sdr/ASOA2011112001001.md): Fan · failed · Nov 20, 2011 · N11127 · Emb EMB145XR · Air Distribution Fan > DURING DESCENT THE CREW REPORTED SMOKE IN THE COCKPIT AND DECLARED AN EMERGENCY LANDING, WITHOUT INCIDENT. UPON INSPECTION, MX DETERMINED THE SOURCE OF SMOKE TO BE THE COCKPIT RECIRCULATION FAN. THE FAN WAS REPLACED, OPS CHECKS PERFORMED AND THE DISCREPANCY - [SDR C2XA11IA258](https://openairdocs.org/sdr/C2XA11IA258.md): Engine · malfunctioned · Nov 12, 2011 · N11127 · Emb EMB145XR · Engine (Turbine/Turboprop) > DURING CRUISE THE CREW REPORTED A LAV SMOKE INDICATION WARNING HOWEVER NO VISUAL SMOKE WAS NOTED. THE AIRCRAFT DIVERTED TO ICT AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED ENGINE RUNS AND DETERMINED THE SOURCE OF THE SMOKE TO BE THE NR 2 ENGINE. T - [SDR C2XA11SH096](https://openairdocs.org/sdr/C2XA11SH096.md): Skin · cracked · Jun 26, 2011 · N11127 · Emb EMB145XR · Fuselage Main, Plate/Skin > SHV - DURING C-CK - LT SKIN HAS CRACKS AROUND 4 RIVETS. REPAIRED SKIN IAW EC5330-02432. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11TY068](https://openairdocs.org/sdr/C2XA11TY068.md): Unknown · smoke · May 27, 2011 · N11127 · Emb EMB145XR · Air Distribution System > SMOKE IN CABIN DURING CLIMBOUT. AIR RETURN. C/W FIM TASK CARDS. NO DEFECTS FOUND AND AIRCRAFT RETURNED TO SERVICE. - [SDR C2XA11TY065](https://openairdocs.org/sdr/C2XA11TY065.md): Unknown · smoke · May 27, 2011 · N11127 · Emb EMB145XR · Air Distribution System > TYS - A/C EN ROUTE FROM CLT TO IAH WHEN SMOKE WAS SEEN IN THE CABIN, CREW RETURN TO CLT WITHOUT INCIDENT OR INJURY. MAINTENANCE RAN A/C ON THE GROUND PER FIM 21-20-00-810-803-A. NO SMOKE OR FUMES DETECTED. OPS CHECK WAS GOOD AND WAS RELEASED BACK TO SERVICE - [SDR C2XA11RI094](https://openairdocs.org/sdr/C2XA11RI094.md): Flapper Valve · leaking · May 25, 2011 · N11127 · Emb EMB145XR · Fuel Storage > FLIGHT 2143 - GSP - FLIGHT CREW REPORTED THAT APPEARED TO BE A LEAK OF FUEL ON LEFT WING, CONFIRMED BY TOWER IN FLT. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED LEFT WING FLAPPER VALVE AT NACA VENT AND PERFORMED OPERATIONA - [SDR C2XA10IA102](https://openairdocs.org/sdr/C2XA10IA102.md): Unknown · malfunctioned · Mar 25, 2010 · N11127 · Emb EMB145XR · Landing Gear Retraction/Extension System > IAH - FLIGHT 2878, THE CREW REPORTED COMING OUT OF PIT THAT THE GEAR WOULD NOT RETRACT WHEN COMMANDED, AND RECEIVED EICAS WARNING LG/LEVER DISAGREE. THE GEAR EVENTUALLY RAISED AND THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE IN - [SDR C2XA10IA015](https://openairdocs.org/sdr/C2XA10IA015.md): Fuel Line · leaking · Jan 13, 2010 · N11127 · Emb EMB145XR · APU Engine Fuel and Control > IAH - FLIGHT 2337, THE CREW REPORTED, SMELLED FUEL AFTER T/O WITH THE APU RUNNING BLEEDS AND AGAIN AFTER STARTING THE APU UPON PARKING AT IAH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE APU FUEL CONTROL LINE, OPERATIONA - [SDR C2XA09RI222](https://openairdocs.org/sdr/C2XA09RI222.md): Proximity Switch · malfunctioned · Dec 21, 2009 · N11127 · Emb EMB145XR · Drag Control System > FLIGHT 2484 - EWR - FLIGHT CREW REPORTED SPOILER FAILURE INDICATION ON EICAS DURING LANDING. CREW ABORTED APPROACH. CREW LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED LEFT INBOARD SPOILER PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY - [SDR C2XA09SH447](https://openairdocs.org/sdr/C2XA09SH447.md): Floor Support · corroded · Nov 22, 2009 · N11127 · Emb EMB145XR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 29. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09 SH424](https://openairdocs.org/sdr/C2XA09%20SH424.md): Skin · cracked · Nov 15, 2009 · N11127 · Emb EMB145XR · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK RT FRAME 78 HAS VISUAL EVIDENCE OF CRACKS AROUND RIVETS. MAINTENANCE PERFORMED REPAIR ON RT FRAME 78 STRINGER 6R IAW EC5330-02011. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH423](https://openairdocs.org/sdr/C2XA09SH423.md): Rivet · worn · Nov 15, 2009 · N11127 · Emb EMB145XR · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK SMOKING RIVETS AT LT FRAME 78. MAINTENANCE PERFORMED REPAIR ON FRAME 78 STRINGER 6L IAW EC5330-02011. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09SH416](https://openairdocs.org/sdr/C2XA09SH416.md): Bracket · corroded · Nov 11, 2009 · N11127 · Emb EMB145XR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CARGO DOOR FWD TRIANGLE BRACKET IS CORRODED (LEVEL 2 LOCAL). MAINTENANCE BLENDED AND EVALUATED THE CORROSION ON THE CARGO DOOR FWD TRIANGLE BRACKET IAW EC5320-01479 REV ORIG. CORRODED AREAS FOUND TO BE WITHIN LIMITS WITH.006 MATERIAL LO - [SDR C2XA09SH411](https://openairdocs.org/sdr/C2XA09SH411.md): Support · corroded · Nov 9, 2009 · N11127 · Emb EMB145XR · Waste Disposal System > SHV - DURING C-CHECK, TOILET WASTE DRAIN VALVE CORRODED. REMOVED AND REPLACED TOILET WASTE DRAIN VALVE SUPPORT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09RI183](https://openairdocs.org/sdr/C2XA09RI183.md): Warning System · malfunctioned · Oct 24, 2009 · N11127 · Emb EMB145XR · Landing Gear Position and Warning > FLIGHT 2353 - YQM - FLIGHT CREW REPORTED LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. CREW DOWN POWERED ACFT AND MESSAGE DISAPPEAR. ACFT RETURNED TO SERVICE. - [SDR C2XA09RI091](https://openairdocs.org/sdr/C2XA09RI091.md): Duct · defective · May 3, 2009 · N11127 · Emb EMB145XR · Cabin Cooling System > FLIGHT 2753 - EWR - FLIGHT CREW REPORTED BLEED OVERTEMP - PACK NR 2 OVERHEAT ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFUL. EWR MX REMOVED AND REPLACED PRE-COOLER DUCT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETUR - [SDR C2XA08CL040](https://openairdocs.org/sdr/C2XA08CL040.md): Inverter · inoperative · Mar 30, 2008 · N11127 · Emb EMB145XR · Emergency Lighting > CLE FLIGHT2252 - THE CREW REPORTED CABIN CEILING EMERGENCY LIGHT WAS INOPERATIVE AT THE OVERWING EMERGENCY EXIT. MAINTENANCE INSPECTED AND REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA08SH041](https://openairdocs.org/sdr/C2XA08SH041.md): Fitting · worn · Feb 29, 2008 · N11127 · Emb EMB145XR · Ailerons > SHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA ACTUATOR ATTACHMENT FITTING ON THE AILERON SPAR HAD MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW CONTINENTAL EXPRESS EC 5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO S - [SDR C2XA07IA039](https://openairdocs.org/sdr/C2XA07IA039.md): Fuel Sys · leaking · Feb 18, 2007 · N11127 · Emb EMB145XR · APU Engine Fuel and Control > IAH - FLIGHT 2097, DURING PREFLIGHT INSPECTION THE CREW REPORTED A FUEL SMELL IN THE COCKPIT WITH THE APU ON. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL 49-00-00 -C- 116102. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RE - [SDR C2XA07IA038](https://openairdocs.org/sdr/C2XA07IA038.md): Fuel Nozzle · unknown · Feb 15, 2007 · N11127 · Emb EMB145XR · APU Engine Fuel and Control > IAH - FLIGHT 2041, THE CREW REPORTED A FUEL SMELL IN THE CABIN ON START. MAINTENANCE PLACED THE APU ON MEL 49-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON FLIGHT 2891 WHERE MAINTENANCE REMOVED AND REPLACED THE A Next page: https://openairdocs.org/aircraft/N11127/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 = 'N11127' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N11127/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.