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 SIMA20121018003Inverter · inoperativeDURING B INSPECTION FOUND SEAT 12A FORWARD EMERGENCY SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE INVERTER PER EMB AMM 33-50-11-000-801-A AND 33-50-11-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TOct 18, 2012 · N606AE · Emb EMB145LR · Emergency LightingSDR SIMA20121018002A/C Pack · dirtyFLIGHT 3916, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN IMMEDIATELY AFTER PUSHBACK FROM GATE. AIRCRAFT REMOVED FROM SERVICE. FOUND NR 2 PACK BLOWING DUST & DIRT. NO EVIDENCE OF SMOKE OR OIL ODOR. REMOVED AND REPLACED THE NR 1 PACK VALVE IAW AMM 21-51-01. OOct 18, 2012 · N905JH · Emb EMB145LR · Cabin Cooling SystemSDR CHQA20121017394Cup · corrodedDURING INSPECTIONS, THE LAVATORY SHUT OFF VALVE SUPPORT WAS FOUND TO BE CORRODED. THE LAVATORY CUP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND 53-30-02.Oct 17, 2012 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20121017093RBolt · unsecureCREW REPORTED MAIN CABIN DOOR LEVER PRODUCES LOUD METAL POP SOUND WHEN OPENING AND FEELS UNUSUALLY HARD TO OPEN. MX INSPECTED AND FOUND HARDWARE LOOSE, RESECURED THE INTERNAL HANDLE BOX BOLTS WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICEOct 17, 2012 · N16987 · Emb EMB145LR · Passenger/Crew DoorsSDR SIMA20121017004Holder · defectiveON FLIGHT 3909 THE CREW REPORTED WHEN BATTERY POWER WAS ESTABLISHED ON AIRCRAFT THE FIRST OFFICERS YOKE CHART HOLDER STARTED SMOKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS YOKE CHART HOLDER IAW EMB 145 AMM 25-12-11. Oct 17, 2012 · N676AE · Emb EMB145LR · Flight Compartment EquipmentSDR SIMA20121017002Battery · dischargedDURING MAINTENANCE INSPECTION FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY AND CHARGER IAW AMM 33-50-04. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAOct 17, 2012 · N692AE · Emb EMB145LR · Emergency LightingSDR ASOA20121017116Floor Support · corrodedDURING C CHECK, R & R OMEGA BEAM AT FRAME 18 HAS CORROSION (LOCAL LEVEL 2). MX PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 18 IAW EC5310-01631. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Oct 17, 2012 · N14977 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20121017115Beam · corrodedDURING C CHECK, CARGO LOWER BEAM FRAME 65-68 IS CORRODED. MX R & R CARGO LOWER BEAM BETWEEN FRAME 65-68 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Oct 17, 2012 · N14977 · Emb EMB145LR · Fuselage Structure (General)SDR ASOA20121018153Skin · crackedLT WING UPPER SKIN T/E WAS FOUND CRACKED AT THE LT GROUND SPOILER HINGE POINT. CUTOUT THE CRACKED AREA, FABRICATED AND INSTALLED DOUBLER AND TRIPLER. ACFT STILL IN C CHECKOct 17, 2012 · N14953 · Emb EMB145LR · Wing, Plate/SkinSDR ASOA20121017152Window Frame · corrodedLEFT & RIGHT WINDSHIELD FRAME HAS CORROSION IN SEVERAL HOLES. REMOVED CORROSION FROM BOLT HOLES AND SOME OF THE HOLES REQUIRED BUSHINGS TO BE INSTALLED IAW ETD2012-145-014418-A AND EC5310-01633. ACFT IS STILL IN C-CHECK.Oct 17, 2012 · N14953 · Emb EMB145LR · Fuselage Main, StructureSDR SIMA20121016011Structure · corrodedAFT SCREW HOLE ON BOTTOM EDGE OF PAX DOOR IS CORRODED. REPAIRED AFT SCREW HOLE CORRODED AREA ON BOTTOM EDGE OF PAX DOOR IAW AEA EO-EM-52MR-331.Oct 16, 2012 · N649PP · Emb EMB145LR · Passenger/Crew DoorsSDR SIMA20121016010Gusset · corrodedDURING B INSPECTION FOUND THE RIGHT FLOORBEAM DIAMOND GUSSET CORRODED BETWEEN FRAMES 59-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOORBEAM DIAMOND GUSSET BETWEEN FRAMES 59-61 IAW EMB SRM 51-40-02, EMB SRM 51-20-03, EMB SRM 51Oct 16, 2012 · N649PP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20121016009Gusset · corrodedDURING B INSPECTION FOUND THE RIGHT FLOORBEAM DIAMOND GUSSET CORRODED AT FRAME 22. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOORBEAM DIAMOND GUSSET IAW EMB SRM 51-40-02, EMB SRM 51-20-03, EMB SRM 51-40-06 AND EMB SRM 51-40-09. Oct 16, 2012 · N649PP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20121016008Sill · corrodedDURING B INSPECTION FOUND THE LEFT FLOOR SILL IS CORRODED BETWEEN FRAMES 61-65. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FLOOR SILL BETWEEN FRAMES 61-65 IAW EMB SRM 51-40-02, EMB SRM 51-20-03, EMB SRM 51-40-06 AND EMB SRM 51-40-09Oct 16, 2012 · N649PP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20121016007Gusset · corrodedDURING B INSPECTION FOUND THE LEFT OMEGA BEAM GUSSET CORRODED BETWEEN FRAMES 19-24. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED WITH SERVICEABLE GUSSET IAW EMB SRM 51-40-02, EMB SRM 51-20-03, EMB SRM 51-40-06 AND EMB SRM 51-40-09. THE AIRCRAOct 16, 2012 · N649PP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20121016006Support · crackedDURING B INSPECTION FOUND THE RIGHT FLOORBEAM SUPPORT CRACKED ON THE RIGHT SIDE BETWEEN FRAMES 47-48. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOORBEAM SUPPORT ON THE RIGHT SIDE BETWEEN FRAMES 47-48 IAW EMB SRM 53-23-02. THE OPOct 16, 2012 · N649PP · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA20121016005Support · crackedDURING B INSPECTION FOUND THE RIGHT FLOORBEAM SUPPORT CRACKED ON THE LEFT SIDE BETWEEN FRAMES 47-48. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOORBEAM SUPPORT ON LEFT SIDE BETWEEN FRAMES 47-48 IAW EMB SRM 53-23-02. THE OPERATIOOct 16, 2012 · N649PP · Emb EMB145LR · Fuselage Main, Floor BeamSDR SIMA20121016004Light · crackedDURING B INSPECTION FOUND THE LEFT NR 1, 5 AND 6 PROXIMITY LIGHT FLOOR SIDEWALL ASSEMBLIES CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1, 5 AND 6 PROXIMITY LIGHT FLOOR SIDEWALL ASSEMBLIES IAW EMB AMM 33-50-2.1.(3) AND 3.I.(1).Oct 16, 2012 · N649PP · Emb EMB145LR · Emergency LightingSDR SIMA20121016003Cover · brokenDURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT STRIP PANEL COVER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT STRIP PANEL COVER IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCOct 16, 2012 · N933JN · Emb EMB145LR · Emergency LightingSDR SIMA20121016002Sill · corrodedDURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW CARGO DOOR CENTER SILL IAW EMB SRM 51-40-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 16, 2012 · N933JN · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20121016001Sill · corrodedDURING MAINTENANCE INSPECTION FOUND THE SERVICE DOOR AFT SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICE DOOR AFT SILL IAW EMB SRM 51-40-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 16, 2012 · N933JN · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20121015022Shear Tie · corrodedFRAME 65 SHEAR TIE CORRODED. REPAIRED SHEAR TIE IAW AEA EO EM-53MR-1129.Oct 15, 2012 · N931AE · Emb EMB145LR · Fuselage Internal Mounting StructureSDR SIMA20121015019Sill · corrodedDURING MAINTENANCE INSPECTION FOUND THE SERVICE DOOR FORWARD SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICE DOOR FORWARD SILL IAW EMB SRM 51-40-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 15, 2012 · N931AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20121015018Sill · corrodedDURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW CARGO DOOR CENTER SILL IAW EMB SRM 51-40-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 15, 2012 · N931AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA20121015017Battery · dischargedDURING MAINTENANCE INSPECTION FOUND THE PROXIMITY FLOOR STRIP FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETUNRED TO SERVICE.Oct 15, 2012 · N931AE · Emb EMB145LR · Emergency LightingSDR ASOA20121015092Sleeve · leakingCREW REPORTED ICE COND- ANTI ICE SYS INOPERATIVE WITH WING ANTI/ICE FAIL. AN ODOR THAT SMELLED LIKE BURNED CRAYONS ENTERED THE CABIN. ANTI-ICE WAS OBSERVED TO WORK INTERMITTENTLY. MX R & R DUAL TEMP CONTROL VALVE SLEEVES THAT WERE FOUND LEAKING. OPS CHECKSOct 15, 2012 · N13964 · Emb EMB145LR · Airfoil Anti/De-ice SystemSDR CHQA20121015384Battery · dischargedDURING INSPECTION, BOTH EXTERNAL OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Oct 15, 2012 · N566RP · Emb EMB145LR · Emergency LightingSDR SIMA20121015009Cradle · brokenDURING B INSPECTION FOUND THE CAPTAIN'S FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT CRADLE IAW EMB 145 AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIROct 15, 2012 · N696AE · Emb EMB145LR · Emergency EquipmentSDR SIMA20121015007Light · inoperativeDURING B INSPECTION FOUND THE EMERGENCY LIGHT ON THE MAIN DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNOct 15, 2012 · N939AE · Emb EMB145LR · Emergency LightingSDR SIMA20121015005Bar · out of adjustON FLIGHT 3392 THE FLIGHT ATTENDANTS REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN, IT APPEARED TO CATCH ON THE UPPER LEFT CORNER. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED 1 ADDITIONAL WASHER BETWEEN DOOR ARM FITTING NR 1 AND NR 2 PER ETN #EM-52-013ROct 15, 2012 · N646AE · Emb EMB145LR · Passenger/Crew DoorsSDR SIMA20121015004Guide · unserviceableON FLIGHT 2814 THE CREW REPORTED THE MAIN CABIN DOOR WAS VERY HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD LOWER MAIN DOOR GUIDE REF AMM 53-71-06. THE OPERATIONAL CHECK WAS GOOD REF AMM 52-18-00. NO FURTHER DEFECTS Oct 15, 2012 · N688AE · Emb EMB145LR · Passenger/Crew DoorsSDR SIMA20121015002Flashlight · inoperativeON FLIGHT 2878 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT AS PER EMB MM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO Oct 15, 2012 · N663AR · Emb EMB145LR · Emergency EquipmentSDR SIMA20121015001Flashlight · inoperativeON FLIGHT 2877 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WOULD NOT HOLD A CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 15, 2012 · N633AE · Emb EMB145LR · Emergency EquipmentSDR CHQA20121014383Light · inoperativeDURING INSPECTION, THE LEFT FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Oct 14, 2012 · N568RP · Emb EMB145LR · Emergency LightingSDR CHQA20121014382Thermostat · faultyCREW REPORTED, RECEIVED A BLEED 2 OVERTEMP MESSAGE WHILE ENTERING ICING CONDITIONS IN FLIGHT. THE CREW DIVERTED TO KCMH AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT FAN AIR CONTROL THERMOSTAT AND THE RIGHT FAN AIR VALVE. OPERATIONAL CHECKS OFOct 14, 2012 · N568RP · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA201201014381Valve · faultyCREW REPORTED, RECEIVED A BLEED 2 OVERTEMP MESSAGE WHILE ENTERING ICING CONDITIONS IN FLIGHT. THE CREW DIVERTED TO KCMH AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT FAN AIR CONTROL THERMOSTAT AND THE RIGHT FAN AIR VALVE. OPERATIONAL CHECKS OFOct 14, 2012 · N568RP · Emb EMB145LR · Pneumatic Distribution SystemSDR SIMA20121014004Inverter · inoperativeDURING B INPSECTION FOUND THE OVERHEAD AFT 12A CEILING EMERGENCY IDENTIFIER SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPS CHECK OF EMERGENCY EXIT SIGN. FOUND SIGN GOOD TESTED INVERTER FOUND TO BE BAD. REMOVED AND REPLACED THE EMERGEOct 14, 2012 · N670AE · Emb EMB145LR · Emergency LightingSDR SIMA20121014003Inverter · inoperativeON FLIGHT 9801 THE CREW REPORTED THE AFT EMERGENCY FLOOR LIGHTS WERE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT DC/AC INVERTER NR 6 IAW EMB 145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS Oct 14, 2012 · N653AE · Emb EMB145LR · Emergency LightingSDR SIMA20121014002Battery · unknownDURING MAINTENANCE INSPECTION FOUND THE EMERGENCY BATTERY NR 4 REQUIRES REPLACEMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERY NR 4 AND CHARGER IAW AEA MTX WC 33-700-19 AND 33-700-17. THE OPERATIONAL CHECK WAS GOOD. Oct 14, 2012 · N653AE · Emb EMB145LR · Emergency LightingSDR SIMA20121014001Roller · dirtyON FLIGHT 3387 THE FLIGHT ATTENDANT REPORTED THE MAIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED MAIN DOOR ROLLERS PIN IAW AMM 53-21-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 14, 2012 · N646AE · Emb EMB145LR · Passenger/Crew DoorsSDR ASOA20121014114Beam · corrodedDURING C-CHECK THE CARGO DOOR FRAME LOWER CUT-OUT BEAM WAS FOUND TO BE CORRODED. MX R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Oct 14, 2012 · N13913 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA20121014113Fitting · crackedDURING C-CHECK THE VERTICAL STABILIZER FITTING AT FRAME 75 WAS ORIGINALLY REMOVED FOR EVIDENCE OF FRETTING AND THEN FOUND TO BE CRACKED AROUND AN UPPER BOLT HOLE. MX R & R THE FITTING IAW EC5310-01317. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Oct 14, 2012 · N13913 · Emb EMB145LR · Fuselage, Stabilizer Attach FittingsSDR SIMA20121013004Light · inoperativeDURING B INSPECTION FOUND THE GALLEY CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY CEILING EMERGENCY LIGHT IAW EMB AMM TASK: 33-26-05-000-801-A, AND 33-26-05-400-801-A. THE OPERATIONAL CHECK WAS GOct 13, 2012 · N664MS · Emb EMB145LR · Emergency LightingSDR SIMA20121013003Battery · dischargedDURING B INSPECTION FOUND THE FLIGHT ATTENDANT’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT’S FLASHLIGHT BATTERY IAW EMB AMM TASK: 33-50-16-000-801-A, AND 33-50-16-400-801-A. THE OPERATIONAL CHECKOct 13, 2012 · N664MS · Emb EMB145LR · Emergency EquipmentSDR SIMA20121013002Light · inoperativeDURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT IAW EMB AMM TASK: 33-50-07-000-801-A, AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOOct 13, 2012 · N664MS · Emb EMB145LR · Emergency LightingSDR SIMA20121013001Flashlight · brokenDURING MAINTENANCE INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT SWITCH BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNEDOct 13, 2012 · N620AE · Emb EMB145LR · Emergency EquipmentSDR ASOA20121015148Inverter · inoperativeAFT CENTER AISLE OVER-WING EMERGENCY EXIT SIGN INOPERATIVE. R & R NR 4 EMERGENCY LIGHT INVERTER. OPS CK GOOD ACFT RELEASED AND RETURNED TO SERVICE.Oct 13, 2012 · N16954 · Emb EMB145LR · Emergency LightingSDR ASOA20121014112Skin · crackedDURING C-CHECK THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FRAME 79 STRINGER 5R/6R. MX REAMED OUT THE SKIN CRACK AND PERFORMED A BUSHING REPAIR IAW EC5330-02622. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Oct 13, 2012 · N36915 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA20121014111Skin · crackedDURING C-CHECK THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FRAME 79 BETWEEN STRINGERS 6L/7L. MX REAMED OUT THE SKIN CRACK AND PERFORMED A BUSHING REPAIR IAW EC5330-02622. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Oct 13, 2012 · N36915 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA20121014110Fitting · wornDURING C-CHECK THE RUDDER II CENTER UPPER MOUNT FITTING FOR THE RUDDER I HINGE WAS FOUND TO BE MISALIGNED. MX REPAIRED THE WORN BOLT HOLES IN THE FITTING AND REINSTALLED IT IAW EC5540-01177. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Oct 13, 2012 · N36915 · Emb EMB145LR · Rudder/Tab, Attach Fittings
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