N11121

Service difficulty reports · 101

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 = 'N11121' 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.

SDR ASOA20150208027Bushing · migratedDURING C-CHECK HORIZONTAL STABILIZER LT HINGE FITTING OTBD PLAIN BUSHING MIGRATED. MAINTENANCE PERFORMED REPAIR OF HORIZONTAL STAB LH HINGE FITTING OTBD PLAIN BUSHING HOUSING IAW SRM 55-10-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2015 · N11121 · Emb EMB145XR · Horizontal Stabilizer StructureSDR ASOA20150208026Skin · corrodedDURING C-CHECK INTERNAL SKIN CORRODED, LOCAL LEVEL 2, BETWEEN FRAMES 13-14 STRINGER 21R-20R. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN BETWEEN FRAMES 3-14 STRINGERS 21R-20R IAW EC5320-02000. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2015 · N11121 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR ASOA20150208025Skin · crackedDURING C-CHECK, CRACKS AROUND 2 MARKED RIVETS FRAME 79 STRINGER 5L-7L. MAINTENANCE PERFORMED REPAIR TO SKIN FRAME 79 STRINGER 5L-7L IAW EC5330-02970. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2015 · N11121 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR ASOA20150208024Floor Support · corrodedDURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION, LOCAL LEVEL 2 AROUND 2 NUTPLATE HOLES, FRAME 59-61. MAINTENANCE PERFORMED REPAIR OF CENTER OMEGA BEAM AT 2 NUTPLATE HOLES FRAME 59 AND 61 IAW EC5310-01473, REV D. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2015 · N11121 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR ASOA20150208023Skin · crackedDURING C-CHECK, CRACKS AROUND 2 MARKED RIVETS ON FUSELAGE SKIN AT FRAME 78, STRINGER 5L-7L. MAINTENANCE PERFORMED REPAIR TO FUSELAGE SKIN AT FRAME 78, STRINGER 5L-7L SKIN IAW EC5330-02970. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2015 · N11121 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR ASOA20150208022Skin · gougedDURING C-CHECK EXTERNAL SKIN DENTED/GOUGED AT DENT CLUSTER BETWEEN FRAMES 19-20 STRINGER 11L. MAINTENANCE PERFORMED REPAIR TO SKIN FRAME 19-20, STRINGER 11L-12L IAW EC5330-02971. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2015 · N11121 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR ASOA20150208021Connector · damagedDURING C-CHECK, LT EMERGENCY LIGHT ON 191 PANEL HAS BROKEN CONNECTOR PLUG WIRES. MAINTENANCE REPAIRED CONNECTOR PLUG WIRES ON LT EMERGENCY LIGHT ON 191 PANEL IAW AMM 33-50-00, OPS TEST PASSED. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2015 · N11121 · Emb EMB145XR · Light System WiringSDR ASOA20150208020Connector · damagedDURING C-CHECK, RT EMERGENCY LIGHT ON 191 PANEL HAS BROKEN CONNECTOR PLUG WIRES. MAINTENANCE REPAIRED CONNECTOR PLUG WIRES ON RT EMERGENCY LIGHT ON 191 PANEL IAW AMM 33-50-00. OPS TEST PASSED. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2015 · N11121 · Emb EMB145XR · Light System WiringSDR ASOA20150205019Skin · crackedCRACKS AROUND RIVETS FR 78, STR 5L-7L. REPAIRED SKIN IAW EC5330-02970. ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 5, 2015 · N11121 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR ASOA20150205018Skin · corrodedFWD FUSELAGE SKIN CORRODED BETWEEN FRAMES 12-13 STRINGERS 20R - 20L. R & R SKIN IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 5, 2015 · N11121 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR ASOA20150203017Stringer · corrodedSTRINGER 21L HAS CORROSION BETWEEN FRAMES 10 - 14. R & R THE STRINGER IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 3, 2015 · N11121 · Emb EMB145XR · Fuselage Main, Longeron/StringerSDR ASOA20150203016Stringer · corrodedSTRINGER 21R HAS CORROSION BETWEEN FRAMES 12 - 13. R & R THE STRINGER IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 3, 2015 · N11121 · Emb EMB145XR · Fuselage Main, Longeron/StringerSDR ASOA20141012110Clamp · unsecureCREW REPORTED A BLEED NR 2 LEAK INDICATION WITH STRONG ODOR. MX COULD NOT DUPLICATE STRONG ODOR BUT DID REPOSITIONED AND SECURED THE NR 2 BLEED VALVE CLAMP. OPS AND LEAK CHECKS RESULTS GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.Oct 12, 2014 · N11121 · Emb EMB145XR · Pneumatic Distribution SystemSDR ASOA20140820069Smoke Detector · dirtyTHE CREW REPORTED LAVATORY SMOKE WARNING IN FLIGHT. MAINTENANCE INSPECTED AND CLEANED SMOKE DETECTOR SENSOR. OPS CHECKED GOOD.Aug 20, 2014 · N11121 · Emb EMB145XR · Smoke DetectionSDR ASOA20131121131Acm · odorCREW REPORTED A DISTINCTIVE ELECTRICAL BURNING ODOR IN FLIGHT. CABIN EXPERIENCED SLIGHT HAZE. PASSENGER IN 11A STATED SMOKE SEEN COMING FROM ABOVE SEATS 8 AND 9CD. MAINTENANCE R & R NR 1 ACM WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 21, 2013 · N11121 · Emb EMB145XR · Cabin Cooling SystemSDR ASOA20130513047Duct · looseCREW REPORTED DUAL UNANNOUNCIATED PACKS/PRESSURIZATION FAILURE DURING CLIMB OUT. RESULTED IN EMERGENCY DESCENT AND AIR RETURN. MX FOUND A BLOWN DUCT ON PACK 1 AND RESECURED DUCT TO HEAT EXCHANGER WITH PACK 1 OPS CHECK SUCCESSFUL. PACK 2 OPS CHECKED SUCCESSFULMay 13, 2013 · N11121 · Emb EMB145XR · Air Distribution SystemSDR ASOA20130121242Skin · chafedACFT WAS FOUND WITH THE NR 1 ENGINE PYLON SKIN PANEL, CHAFED. MX REPAIRED THE PANEL IAW EC5330-02681. WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF ALL WORK.Jan 21, 2013 · N11121 · Emb EMB145XR · Nacelle/Pylon, Plate/SkinSDR ASOA20130115234Floor Support · corrodedRIGHT FLOOR SUPPORT IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR SUPPORT.Jan 15, 2013 · N11121 · Emb EMB145XR · Fuselage Structure (General)SDR ASOA20130115233Floor Support · corrodedLT OMEGA BEAN TOP CAP IS CORRODED BEYOND LIMITS. R & R TOP CAP.Jan 15, 2013 · N11121 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR ASOA20130115232Attach Bracket · wornLEFT AILERON PCA ATTACH BRACKET HAS A MIGRATED BUSHING. R & R PCA ATTACH BRACKET.Jan 15, 2013 · N11121 · Emb EMB145XR · AileronsSDR ASOA20130115231Frame · corrodedGALLEY AFT STEP-UP CORRODED BEYOND LIMITS. R & R LOWER PORTION OF GALLEY AFT STEP-UP.Jan 15, 2013 · N11121 · Emb EMB145XR · Fuselage Main, FrameSDR ASOA20120128013Acm · smokeTHE CREW REPORTED SMOKE IN THE COCKPIT AFTER PACKS WERE SELECTED FOLLOWED BY PACK NR 1 OVERHEAT MESSAGE. THE ACFT RETURNED TO THE GATE. MX INSPECTED AND RELEASED ACFT IAW MEL PROCEDURES 21-51-00-3. MX REPLACED THE NR 1 PACK ACM. OPS CHECKS WERE GOOD.Jan 28, 2012 · N11121 · Emb EMB145XR · Cabin Cooling SystemSDR C2XA11RI180Fuel Sys · malfunctionedEWR FLT 4270 CREW REPORTED STRONG FUEL SMELL DURING T/O ROLL WHICH DISSIPATED AFTER THE T/O CHECK. EWR MX INSPECTED THE ENGINES AND APU FOR FUEL LEAKS AND FOUND FUEL RESIDUE ON APU COWLING FROM A FAILED APU START. MX RAN APU AND PACKS FOR 20 MINUTES WITH NO Nov 17, 2011 · N11121 · Emb EMB145XR · APU Engine Fuel and ControlSDR C2XA11IA122Display · shortedIAH - DURING MX INSPECTION THE NR 1 MFD WENT BLANK AFTER AN ELECTRICAL BURNING SMELL AND FLICKERING SCREEN. MAINTENANCE REMOVED AND REPLACED THE NR 1 MFD, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 16, 2011 · N11121 · Emb EMB145XR · Central DisplaySDR C2XA11IA121Unknown · odorIAH - FLIGHT 2062, THE CREW REPORTED A STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT ON POWERUP, AND STATED THAT IT SEEMED STRONGER ON THE CAPTAINS SIDE. MAINTENANCE INSPECTED THE AIRCRAFT PERFORMED FIM TASKS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROJun 15, 2011 · N11121 · Emb EMB145XR · Air Distribution SystemSDR C2XA11RI109Anti-Ice Valve · defectiveFLIGHT 2186 - EWR - FLIGHT CREW REPORTED, UNABLE TO MAINTAIN CLIMB PROFILE LEVELED OFF FL290 TO GAIN SPEED. CLIMB TO FL310 AT 1000 FT MIN FL310 TO 350 AT 600FT PER MIN ONLY ABLE TO MAINTAIN MACH .70 IN CRUISE IN THE CLOUDS, 74-.76 IN CLEAR AIR AT 370. EWR MXJun 10, 2011 · N11121 · Emb EMB145XR · Air Intake Anti/De-Ice SystemSDR C2XA11RI062Contactor · burnedFLIGHT 3081 - EWR - FLIGHT CREW REPORTED STRONG SMELL BURNING RUBBER IN FRONT OF ACFT AFTER LANDING. EWR MX REMOVED AND REPLACED CONTACTOR K0236 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (SUPPLEMENTAL CHANGED DIFF May 7, 2011 · N11121 · Emb EMB145XR · Lighting SystemSDR C2XA11IA053Flapper Valve · damagedCME - IAH DURING CLIMB THE RIGHT WING WAS FOUND TO BE VENTING FUEL. THE AIRCRAFT RETURNED TO CME AND LANDED WITHOUT INCIDENT. UPON INSPECTION MAINTENANCE FOUND THE RIGHT WING FLAPPER (CHECK) VALVE TO BE DAMAGED ALLOWING THE FUEL TO ESCAPE THROUGH THE VENT. Mar 11, 2011 · N11121 · Emb EMB145XR · Fuel StorageSDR C2XA10028Thermostat · inoperativeFLIGHT 2217 - CVG - FLIGHT CREW REPORTED BLEED 1/2 OVERTEMP ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED SENSE LINE AND NR 2 FAN AIR THERMOSTAT. SENSE LINE SDR C2XA10RI027 AND FAN AIR THERMOSTAT SDR C2XA10RI0Feb 5, 2010 · N11121 · Emb EMB145XR · Pneumatic Distribution SystemSDR C2XA10RI027AHose · leakingFLIGHT 2217 - CVG - FLIGHT CREW REPORTED BLEED 1/2 OVERTEMP ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED SENSE LINE AND NR 2 FAN AIR THERMOSTAT.Feb 5, 2010 · N11121 · Emb EMB145XR · Pneumatic SystemSDR C2XA10IA053Hose · leakingCVG - FLIGHT 2217, THE CREW REPORTED A BLEED 1 AND 2 OVERTEMP IN ICING CONDITIONS. THE AIRCRAFT RETURNED TO CVG WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO FAN AIR CONTROL THERMOSTAT, AND THE AFT SERVO HOSE ON THE NR 1 SFeb 5, 2010 · N11121 · Emb EMB145XR · Engine Bleed Air SystemSDR C2XA10IA052Thermostat · inoperativeCVG - FLIGHT 2217, THE CREW REPORTED A BLEED 1 AND 2 OVERTEMP IN ICING CONDITIONS. THE AIRCRAFT RETURNED TO CVG WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO FAN AIR CONTROL THERMOSTAT, AND THE AFT SERVO HOSE ON THE NR 1 SFeb 5, 2010 · N11121 · Emb EMB145XR · Pneumatic Distribution SystemSDR C2XA09IA329Relay · inoperativeIAH - FLIGHT 2412, THE CREW REPORTED THAT THE NR 2 ADC FAILED AT 270FT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RELAYS K0039 AND K0040, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVEDec 28, 2009 · N11121 · Emb EMB145XR · Navigation SystemSDR C2XA09CL159Light · inoperativeDURING ROUTINE MAINTENANCE THE RIGHT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.Dec 12, 2009 · N11121 · Emb EMB145XR · Emergency LightingSDR C2XA08RI076Inverter · inoperativeRIC - DURING ROUTINE MAINTENANCE, MX FOUND RIGHT SIDE EMERGENCY EXIT LOWER SIGN NOT ILLUMINATING. MX REMOVED AND REPLACED NR 3 INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.May 20, 2008 · N11121 · Emb EMB145XR · Emergency LightingSDR C2XA08CL059Controller · faultyEWR FLIGHT NR 2753, THE CREW REPORTED AT FL370 THE PRESSURIZATION STARTED CLIMBING TO 14,000 FT. EMERGENCY DESCENT STARTED AND THE PRESSURIZATION STARTED DESCENDING. THE FLIGHT DIVERTED TO CLE. MAINTENANCE INSPECTED AND REPLACED THE DIGITAL PRESSURIZATION CMay 15, 2008 · N11121 · Emb EMB145XR · Cabin Pressure ControllerSDR C2XA08IA125Actuator · inoperativeIAH - FLIGHT 2172, DURING CLIMB THE CREW REPORTED A RAM AIR VALVE FAILURE MESSAGE WITH THE INABILITY TO HOLD CABIN ALTITUDE BELOW 10K' ABOVE 21K' AIRCRAFT ALTITUDE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCMay 13, 2008 · N11121 · Emb EMB145XR · Hydraulic System, MainSDR C2XA08IA004Engine · leakingGJT - FLIGHT 3029, THE CREW REPORTED SMOKE IN THE CABIN FROM THE NUMBER TWO PACK. THE AIRCRAFT DIVERTED TO GJT WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NUMBER TWO PACK ON MEL 21-51-00 CTL NUMBER 136236. ON 01/02/08Jan 2, 2008 · N11121 · Emb EMB145XR · Engine (Turbine/Turboprop)SDR C2XA08IA003Engine · leakingDFW - FLIGHT 3130, THE CREW REPORTED A LOSS OF OIL PRESSURE AND QTY ON THE NUMBER TWO ENGINE DURING CRUISE. THE NUMBER TWO ENGINE WAS SHUT DOWN AS A PRECAUTION, AND THE AIRCRAFT DIVERTED TO DFW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACJan 2, 2008 · N11121 · Emb EMB145XR · Engine (Turbine/Turboprop)SDR C2XA07TY082Skin · damagedTHE REAR FUSELAGE LOWER SKINS AND ADJACENT STRUCTURE OF FRAME 66 WERE DAMAGED. MAINTENANCE INDUCED. REPLACED TWO SKIN PANELS AND SEVERAL SHEAR CLIPS AT FRAME 66 AND REPAIRED SEVERAL DENTS ON THE SKIN JUST FORWARD OF FRAME 66. REPAIRED IAW EA5330-01109. AIRDec 14, 2007 · N11121 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR C2XA07TY073Rivet · crackedTYS - DURING A CURRENT 3C INSPECTION THE RIGHT AFT FUSELAGE AT FR 76 WAS FOUND WITH SOME CRACKED RIVETS ON THE CONTOUR FLANGE OF THE VERTICAL STAB. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT FUSELAGE CONTOUR FLANGE DRAG ANGLE AT FR 76. ALL WORK WAS ACCOMDec 1, 2007 · N11121 · Emb EMB145XR · Vertical Stabilizer, Plate/SkinSDR C2XA07TY045Smoke Detector · malfunctionedTYS ECIAS SHOWED BAGGAGE SMOKE INDICATION DURING FIRE DETECTION TEST AND BAGGAGE LIGHT NOT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED NR 1 BAGGAGE DETECTOR IAW EMB 145 AMM 26-15-01. ALL OPS CHECKS WERE GOOD AND RELEASED TO SERVICE.Aug 28, 2007 · N11121 · Emb EMB145XR · Fire DetectionSDR C2XA06IA164Unknown · odorIAH - FLIGHT 2973, THE CREW REPORTED A VERY STRONG ODOR ON THE GROUND AFTER ENGINE START THAT WENT AWAY AND CAME BACK DURING ICE TEST IN FLIGHT, AND WHICH WENT AWAY AGAIN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OOct 21, 2006 · N11121 · Emb EMB145XR · Air Distribution SystemSDR C2XA06TY026Housing · gougedLT VERT STAB SPHERICAL BEARING HOUSING GOUGED. REAMED RT AND LT HOUSING AND INSTALLED BEARINGS IAW COEX EC5510-01138.May 1, 2006 · N11121 · Emb EMB145XR · Vertical StabilizerSDR C2XA05IA088Inverter · inoperativeMCI - DURING SCHEDULED MAINTENANCE, THE RIGHT OVERWING EMERGENCY EXIT MARKER WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 INVERTER, OPERATIONALLY TESTED THE EMERGENCY LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY.Jul 13, 2005 · N11121 · Emb EMB145XR · Emergency LightingSDR C2XA05CL009Pin · installedCLE - CREW REPORTED THAT THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THAT THE NOSE GEAR SAFETY PIN HAD NOT BEEN REMOVED. MAINTENANCE REMOVED THE NOSE GEAR SAFETY PIN AND RETURNEFeb 13, 2005 · N11121 · Emb EMB145XR · Landing Gear Retraction/Extension SystemSDR C2XA05IA013Connector · dirtyIAH - FLIGHT 3252, THE CREW REPORTED THAT THE FORWARD EMERGENCY LIGHT IN THE GALLEY WAS INOPERATIVE. MAINTENANCE CLEANED THE INVERTER CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART IS NOT SERIJan 21, 2005 · N11121 · Emb EMB145XR · Emergency LightingSDR C2XA04IA063Battery Pack · dischargedIAH - FLIGHT 2556, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT NUMEROUS EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY PACK IAW EMB-145 AMM 33-50-04, OPERATIONALLY CHECKED GOOD, AND THEJun 9, 2004 · N11121 · Emb EMB145XR · Emergency LightingSDR C2XA04IA040Light · inoperativeTHE EMERGENCY LIGHT AT THE PASSENGER DOOR ENTRANCE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ASSEMBLY, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY.Mar 29, 2004 · N11121 · Emb EMB145XR · Emergency LightingSDR C2XA04IA005Light · inoperativeCREW REPORTED THAT THE EMERGENCY LIGHTS DID NOT WORK. AWAITING FURTHER INFORMATION TO COMPLETE THIS REPORT. THE EMERGENCY LIGHT SYSTEM WAS OPERATIONALLY TESTED AND THE DISCREPANCY COULD NOT BE CONFIRMED.Jan 8, 2004 · N11121 · Emb EMB145XR · Emergency Lighting
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