Embraer EMB-145LR

Service difficulty reports · 36,799

Newest first. 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'
  WHERE aircraft_model_key = 'EMB145LR'
  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 CHQA20121205456Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND AROUND THE NUT PLATES AND FASTENER ON THE RIGHT OMEGA BEAM TOP GUSSET PLATE AT FRAME 59 TO THE COMPOSITE FLOOR. THE GUSSET PLATE WAS REPLACED IN ACCORDANCE WITH ETD 2012-145-017227-A.Dec 5, 2012 · N562RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20121205005Light · inoperativeDURING B INSPECTION FOUND THE MAIN CABIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN DOOR EMERGENCY LIGHT IAW EMB 145 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE AIRCRAFT WAS RETURNED TODec 5, 2012 · N697AB · Emb EMB145LR · Emergency LightingSDR CHQA20121204450Battery · dischargedDURING INSPECTION, THE NUMBER 2 EMERGENCY BATTERY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 4, 2012 · N273SK · Emb EMB145LR · Emergency LightingSDR SIMA20121204005Pressure Switch · defectiveON FLIGHT 3336 THE CREW REPORTED THAT WHILE CLIMBING THROUGH FL300 AUTOPILOT FAILED (WARNING) FOLLOWED BY RUDDER SYS 1-2 INOP (CAUTION) FOLLOWED AOM PROCEDURE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RUDDER SYS 2 PRESSURE SWITCH IAW EDec 4, 2012 · N662EH · Emb EMB145LR · Rudder Control SystemSDR SIMA20121204004Inverter · inoperativeDURING B INSPECTION FOUND THE SERVICE DOOR UPPER, LOWER FORWARD, AND FIRST FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND REMOVED AND REPLACED INVERTER ASSEMBLY IAW EMB 145 M/M 33-50-11. THE OPERATIONAL Dec 4, 2012 · N609DP · Emb EMB145LR · Emergency LightingSDR ASOA20121204162Structure · corrodedDIGITAL AT Y=0 CORRODED BEYOND LIMITS. R & R DIGITAL.Dec 4, 2012 · N14902 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20121203468Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 13 BETWEEN STRINGERS 20L AND 21L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Dec 3, 2012 · N279SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20121203007Light · inoperativeDURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY EXIT DOOR LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY EXIT DOOR LIGHT IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFTDec 3, 2012 · N645AE · Emb EMB145LR · Emergency LightingSDR SIMA20121203005Wire · brokenDURING MAINTENANCE INSPECTION FOUND THE FLOOR PROXIMITY LIGHT HAS BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY LIGHT IAW 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Dec 3, 2012 · N661JA · Emb EMB145LR · Light System WiringSDR SIMA20121203004Holder · brokenDURING MAINTENANCE INSPECTION FOUND THE FLIGHT ATTENDANT’S FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED SERVICEABLE FLASHLIGHT HOLDER. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.Dec 3, 2012 · N644AE · Emb EMB145LR · Emergency EquipmentSDR SIMA20121203003Unknown · malfunctionedON FLIGHT 3309 THE CREW REPORTED THAT 5 MINUTES AFTER TAKEOFF A/P FAILED FOLLOWED BY RUDDER SYS 1-2 INOP MESSAGE. THE CREW FOLLOWED AOM PROCEDURES. NO RESET WAS ACCOMPLISHED. THE CREW DECLARED AN EMERGENCY AND RETUNED TO MOB. THE AIRCRAFT LANDED WITHOUT INCDec 3, 2012 · N662EH · Emb EMB145LR · Autopilot SystemSDR ASOA20121203143Stringer Splice · corrodedDURING C-CHECK STRINGER 21R SPLICE BETWEEN FRAME 13-14 CORRODED (LOCAL LEVEL 2). MX R & R STRINGER SPLICE BETWEEN FRAME 13-14 AT STRINGER 21R IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 3, 2012 · N13955 · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR ASOA20121203142Skin · corrodedDURING C-CHECK INTERNAL SKIN CORRODED BETWEEN FRAMES 12-13 STRINGERS 20L-20R. MX PERFORMED REPAIR TO INTERNAL SKIN BETWEEN FRAMES 12-13 STRINGER 20L-20R IAW EC5310-01639. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 3, 2012 · N13955 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA20121203141Skin · corrodedDURING C-CHECK INTERNAL SKIN CORRODED FRAMES 13-14 STRINGERS 20L-20R. MX PERFORMED REPAIR OF INTERNAL SKIN AT FRAMES 13-14 STRINGERS 20L-20R IAW EC5330-02651. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 3, 2012 · N13955 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA20121203140Frame · chafedDURING C-CHECK FRAME 60 CHAFED STRINGER 4L-5L. MX PERFORMED REPAIR OF FRAME 60 STRINGER 4L-5L IAW EC5320-01728. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 3, 2012 · N13955 · Emb EMB145LR · Fuselage Main, FrameSDR ASOA20121203139VFrame · crackedDURING C-CHECK CRACK AT FRAME 10 JUST BELOW RT DV WINDOW (STRINGER 9). MX R & R FRAME 10 UNDER RT DV WINDOW AT STRINGER 9R IAW SRM 51-40-02. ALODINED, PRIMED, AND PAINTED IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 3, 2012 · N13955 · Emb EMB145LR · Fuselage Main, FrameSDR ASOA20121203138VFrame · crackedDURING C-CHECK CRACK AT FRAME 10 JUST BELOW LT DV WINDOW (STRINGER 9). MX R & R FRAME 10 LT UNDER DV WINDOW IAW SRM 51-40-02. ALODINED, PRIMED AND PAINTED IAW CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 3, 2012 · N13955 · Emb EMB145LR · Fuselage Main, FrameSDR ASOA20121203137Smoke Detector · no testDURING PREFLIGHT, LAVATORY SMOKE DETECTOR WILL NOT TEST. MX R & R LAVATORY SMOKE DETECTOR IAW AMM 26-14-01, OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 3, 2012 · N13956 · Emb EMB145LR · Smoke DetectionSDR CHQA20121202449Skin · damagedCREW REPORTED A LIGHTNING STRIKE ON CLIMBOUT. THE CREW DIVERTED TO CMH AND LANDED WITHOUT INCIDENT. DURING THE LIGHTNING STRIKE INSPECTION, MAINTENANCE FOUND BURN MARKS BETWEEN STRINGERS 2L AND 3L, BETWEEN FRAMES 56 AND 57. MAINTENANCE REPAIRED THE AREA IN Dec 2, 2012 · N566RP · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA20121204163Floor Support · corrodedRT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.Dec 2, 2012 · N14902 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20121204161Support · corrodedLEFT WALL SUPPORT/DOUBLER WEB AT FLOOR SUPPORT AND FRM 61 CORRODED BEYOND LIMITS. R & R SUPPORT/DOUBLER.Dec 2, 2012 · N14902 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20121202006Pipe · disconnectedON FLIGHT 3526 THE CREW REPORTED A STRONG BLEED AIR SMELL IN COCKPIT AND CABIN ON CLIMB AND DESCENT. THE FLIGHT ATTENDANT REPORTED IT MADE HER COUGH AND WAS WORSE TOWARDS THE FRONT OF THE CABIN. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH FIM 21-20Dec 2, 2012 · N634AE · Emb EMB145LR · Cabin Cooling SystemSDR SIMA20121202005Charger · inoperativeDURING MAINTENANCE INSPECTION FOUND THE EMERGENCY BATTERY CHARGER ASSEMBLY NR 3 NEEDED TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY CHARGER ASSEMBLY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD.Dec 2, 2012 · N649PP · Emb EMB145LR · Emergency LightingSDR SIMA20121202004Charger · inoperativeDURING MAINTENANCE INSPECTION FOUND THE EMERGENCY BATTERY CHARGER ASSEMBLY NR 1 NEEDED TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY CHARGER ASSEMBLY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD.Dec 2, 2012 · N649PP · Emb EMB145LR · Emergency LightingSDR SIMA20121202003Charger · inoperativeDURING MAINTENANCE INSPECTION FOUND THE EMERGENCY BATTERY CHARGER ASSEMBLY NR 4 NEEDED TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY CHARGER ASSEMBLY IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD.Dec 2, 2012 · N649PP · Emb EMB145LR · Emergency LightingSDR SIMA20121202002Light · inoperativeDURING B INSPECTION FOUND THE LEFT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS REDec 2, 2012 · N692AE · Emb EMB145LR · Emergency LightingSDR SIMA20121202001Battery · dischargedDURING B INSPECTION FOUND THE RIGHT OVER WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT CHARGER AND BATTERY IAW EMB W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURDec 2, 2012 · N692AE · Emb EMB145LR · Emergency LightingSDR SIMA20121201003Pressure Switch · defectiveON FLIGHT 2862 THE CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED AN EICAS RUDDER SYSTEM 2 INOP MESSAGE. THE CREW COMPLETED THE AOM VOL 1 CHECK LIST, NOTIFIED SOC AND ATC, DECLARED AN EMERGECNY AND RETURNED TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE Dec 1, 2012 · N651AE · Emb EMB145LR · Hydraulic System, MainSDR SIMA20121201002Battery · dischargedDURING B INSPECTION FOUND THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB IAW EMB 33-50-10-000-801-A AND 33-50-10-400-801-A. PART NUMBER 1317. NO FIX. REMOVED AND RDec 1, 2012 · N617AE · Emb EMB145LR · Emergency LightingSDR SIMA20121201001Roller · unknownON FLIGHT 4208 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS EXTREMELY HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. SERVICED PASSENGER DOOR FRAME ROLLERS AS PER EMB AMM 53-21-02. THE PASSENGER DOOR OPENS WITH EASE. THE OPERATIONAL CHECK WASDec 1, 2012 · N678AE · Emb EMB145LR · Passenger/Crew DoorsSDR SIMA20121130014Frame · corrodedCARGO DOOR LATERAL L-SHAPE CORRODED FRAME. COMPLIED WITH EO EM-53MR-1129.Nov 30, 2012 · N604AE · Emb EMB145LR · Cargo/Baggage DoorsSDR SIMA20121130013Sill · corrodedDURING B INSPECTION FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.Nov 30, 2012 · N604AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20121130012Sign · looseDURING MAINTENANCE INSPECTION FOUND THE OVERWING EMERGENCY EXIT LOCATING SIGN ASSEMBLY AFT SIDE OF CEILING PANEL LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVERWING EMERGENCY EXIT LOCATING SIGN AFT ASSEMBLY OF CEILING PANEL 253CLCNov 30, 2012 · N604AE · Emb EMB145LR · Emergency LightingSDR SIMA20121130011Wire · cutDURING MAINTENANCE INSPECTION FOUND THE EXTERIOR EMERGENCY LIGHT ON THE RIGHT OVERWING WOULD NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CUT WIRE W102-8502-22 IAW EMB 145 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RNov 30, 2012 · N604AE · Emb EMB145LR · Emergency LightingSDR SIMA20121130010Terminal · brokenDURING MAINTENANCE INSPECTION FOUND THE VERY AFT EMERGENCY LIGHT STRIP HAS A BROKEN TERMINAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE VERY AFT EMERGENCY LIGHT STRIP CONNECTOR IAW EMB 145 SWPM 20-00-03 AND 20-21-00 IAW EMB 145 SWPM 20-00-03 AND 20Nov 30, 2012 · N604AE · Emb EMB145LR · Emergency LightingSDR SIMA20121130009Light · damagedDURING MAINTENANCE INSPECTION FOUND THE NR 2 EMERGENCY LIGHT STRIP DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SENov 30, 2012 · N658AE · Emb EMB145LR · Emergency LightingSDR SIMA20121130008Wire · brokenDURING B INSPECTION FOUND THE NR 1 FORWARD EMERGENCY LIGHT STRIP HAS BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 FORWARD EMERGENCY LIGHT STRIPS IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WANov 30, 2012 · N658AE · Emb EMB145LR · Light System WiringSDR CHQA20121130462Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 53 THROUGH FRAME 58. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.Nov 30, 2012 · N279SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20121130007Flap · malfunctionedON FLIGHT 3339 THE CREW REPORTED THE FLAPS FAILED AT 22 DEGREES WOULD NOT RETRACT. RECEIVED AN "FLAP FAIL" MESSAGE ON EICAS. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED CMC DOWNLOAD; FLAP JAMMING MSG ON CMC. COMPNov 30, 2012 · N928AE · Emb EMB145LR · Trailing Edge Flap Control SystemSDR SIMA20121130005Battery · dischargedDURING B INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW EMB AMM TASK: 33-50-07-000-801-A, AND 33-50-07-400-801-A. PART NUMBER 1317. NO FIX RNov 30, 2012 · N699AE · Emb EMB145LR · Emergency LightingSDR SIMA20121130004Light · inoperativeDURING B INSPECTION FOUND THE FORWARD CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CEILING EMERGENCY LIGHT IAW EMB 145 AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GONov 30, 2012 · N617AE · Emb EMB145LR · Emergency LightingSDR CHQA20121129467Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 59. THE LEFT OMEGA BEAM GUSSET AT FRAME 59 WAS REPLACED IN ACCORDANCE WITH 51-40-02.Nov 29, 2012 · N279SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20121129466Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT INBOARD SEAT TRACK AT FRAME 30 THROUGH FRAME 36. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.Nov 29, 2012 · N279SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20121129465Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 47 THROUGH FRAME 52. THE SEAT TRACK WAS REPLACED IN ACORDANCE WITH AMM 53-01-06.Nov 29, 2012 · N279SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20121129464Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT INBOARD SEAT TRACK AT FRAME 36 THROUGH FRAME 45. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.Nov 29, 2012 · N279SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20121129463Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 42. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.Nov 29, 2012 · N279SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20121129461Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OUTBOARD SEAT TRACK AT FRAME 23 THROUGH FRAME 30. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.Nov 29, 2012 · N279SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20121129460Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OUTBOARD SEAT TRACK AT FRAME 47 THROUGH FRAME 52. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.Nov 29, 2012 · N279SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20121128011Grip · out of adjustON FLIGHT 3322 THE CREW REPORTED THE MAIN CABIN DOOR HANDLE GRIP CAME OFF MAKING IT DIFFICULT TO OPERATE. DEFERRED MAIN DOOR RUBBER HANDGRIP IAW CDL 52-1, AUTH. NO.111334CDL-D. NO DEFECTS NOTED WITH DOOR OPERATION WITH GRIP FULLY REMOVED. INSTALLED MAIN DOONov 28, 2012 · N692AE · Emb EMB145LR · Passenger/Crew DoorsSDR ASOA201228111Lamp · inoperativeDURING A-CHECK INSPECTION, IT WAS FOUND THAT THE LT OVERWING AND ROW 12 EMERGENCY LIGHTS WERE INOPERATIVE. MX R & R THE LIGHT BULBS IN BOTH THE LT OVERWING AND ROW 12 EMERGENCY LIGHTS WITH OPS CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 28, 2012 · N11548 · Emb EMB145LR · Emergency Lighting
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