Embraer EMB-145ER

Service difficulty reports · 1,266

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 = 'EMB145ER'
  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 ASOA20121107123VSill · corrodedDURING C-CHECK, THE SERVICE DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2012 · N14938 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20121107122VHinge Fitting · wornDURING C-CHECK, THE RUDDER LOWER CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MX OVERSIZED THE HOLES AND REPLACED THE HAT BUSHINGS IAW EC5540-01178. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2012 · N14938 · Emb EMB145ER · Rudder StructureSDR ASOA20121107121VSkin · corrodedDURING C-CHECK, THE CARGO DOOR LOWER INTERNAL SKIN WAS FOUND TO BE CORRODED AROUND THE BOTTOM NUT PLATES. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5230-01208. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2012 · N14938 · Emb EMB145ER · Cargo/Baggage DoorsSDR ASOA20121107120VDoubler · crackedDURING C-CHECK THE VERTICAL STAB DOUBLER BETWEEN FRAMES 80-81 AND STRINGERS 1L-1R WAS FOUND TO BE CRACKED. MX R & R THE DOUBLER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2012 · N14938 · Emb EMB145ER · Vertical StabilizerSDR ASOA20121107119VShear Tie · corrodedDURING C-CHECK THE SHEAR TIE AT FRAME 19 BETWEEN STRINGERS 21L AND 21R WAS FOUND TO BE CORRODED. MX R & R THE SHEAR CLIP IAW EC5320-01713. ACFT APPROVED FOR RETURN TO SERVICE.Nov 7, 2012 · N14938 · Emb EMB145ER · Fuselage Internal Mounting StructureSDR ASOA20121107118VShear Tie · crackedDURING C-CHECK THE CENTERLINE SHEAR TIE AT FRAME 42, 6:00 POSITION IN THE WING BOX WAS FOUND TO BE CRACKED. MX R & R THE SHEAR TIE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2012 · N14938 · Emb EMB145ER · Fuselage Internal Mounting StructureSDR ASOA20121107117Skin · corrodedDURING C-CHECK, THE INTERNAL SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 17-19 AND STRINGERS 21L-21R. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-02633. ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 7, 2012 · N14938 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR ASOA20121005142Skin · damagedDENT AFT OF PAX DOOR BETWEEN FRAME 18 & 20 AND STRINGERS 13 & 15L. CUT OUT CREASED AREA, FABRICATED DOUBLER & FILLER AND INSTALLED.Oct 3, 2012 · N12934 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR ASOA20120725124Firewall · crackedDURING C CHECK, FOUND APU FIREWALL CRACKED AT THE RT SIDE 03:00 POSITION. MX REPAIRED THE APU FIREWALL IAW EC 5330-02578, FIG 8. CUT OUT THE DAMAGE AREA AND REPLACED IT WITH A DOUBLER AND FILLER ALL IAW EC 5330-02578.Jul 25, 2012 · N16976 · Emb EMB145ER · APU Cowling/ContainmentSDR ASOA20120716095Skin · crackedDURING A INSPECTION, LT WING SKIN AT THE CENTER HINGE POINT FOR THE GROUND SPOILER WAS FOUND TO BE CRACKED. MX STOP DRILED THE CRACK. MX INSTALLED A DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5710-01193, ACFT WAS APPROVED FOR RETURN TO SEJul 16, 2012 · N12934 · Emb EMB145ER · Wing, Plate/SkinSDR ASOA20120716094Mount · crackedDURING C INSPECTION, THE NR 2 ENGINE FORWARD LOWER ENGINE MOUNT YOKE LINKAGE WAS FOUND TO BE CRACKED IN THE INNER RADIUS. CRACK STOP DRILLED.Jul 16, 2012 · N12934 · Emb EMB145ER · Engine Mount SectionSDR ASOA20111210012Torque Box · damagedDURING C-CHECK RIB 19 TORQUE BOX III FLAP ROLLER BUSHING HSG DAMAGED OUT OF LIMITS. MX PERFORMED REPLACEMENT OF RIB 19-TORQUE BOX III IAW EC5710-01181, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 10, 2011 · N14940 · Emb EMB145ER · Trailing Edge FlapsSDR ASOA2011112600005Skin · damagedDURING C-CHECK, WORKING RIVETS AT FRAME 77, STRINGER 4R-10R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 77, STRINGER 4R-10R IAW EC5330-02501 ORIG. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 26, 2011 · N14939 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR ASOA2011112600004Skin · crackedDURING C-CHECK, FUSELAGE CRACKED AROUND RIVET AT FRAME 78, STRINGER 6R-7R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 78, STRINGER 6R-7R IAW EC5330-02501 ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Nov 26, 2011 · N14939 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR ASOA2011112600003Skin · crackedDURING C-CHECK, FUSELAGE CRACKED AROUND RIVET AT FRAME 78, STRINGER 7R-8R. MX PERFORMED REPAIR OF FUSELAGE AT FRAME 78, STRINGER 7R-8R IAW EC5330-02501 ORIG. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 26, 2011 · N14939 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR ASOA201111261009Threshold · corrodedDURING C-CHECK SERVICE DOOR THRESHOLD CORRODED AROUND NUTPLATES. MX R & R SERVICE DOOR CENTER SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 26, 2011 · N14939 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA201111261008Skin · crackedDURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 79 STRINGER 5R-6R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 79 STRINGER 5R-6R IAW EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 26, 2011 · N14939 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR ASOA201111261006Skin · crackedDURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 75 STRINGER 3R-4R. MX PERFORMED REPAIR OF FUSELAGE EXTERNAL SKIN AT FRAME 75 STRINGER 3R-4R IAW EC5330-02353. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Nov 26, 2011 · N14939 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR C2XA11TY157Skin Panel · crackedTYS - A/C WAS IN MOB WHEN A BELTLOADER HIT THE 191 BELLY PANEL AND CRACKED THE PANEL AFT OF THE PORTABLE WATER DOOR. A/C WAS FERRIED TO TYS WHERE THE COMPOSITE SHOP MADE THE REPAIR IAW ETD 2011-145-106533. ALL WORK ACCOMPLISHED AND WAS RELEASED TO SERVICE. Oct 14, 2011 · N15941 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR C2XA11TY149Skin · damagedAIRCRAFT SUSTAINED GROUND DAMAGE TO THE RT REAR FUSELAGE BETWEEN FRAMES 63 AND 68. CUT OUT DAMAGE, PERFORMED EDDY CURRENT INSPECTION, FABRICATED FILLERS AND DOUBLERS. REPLACED FRAME 66 INTERNAL SKIN SPLICE BETWEEN STRINGERS 8R & 9R AND 14R & 15R. GENERATED Sep 23, 2011 · N14945 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR C2XA11TY141Skin · corrodedTYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND VARIOUS AREAS OF CORROSION IN THE LOWER FUSELAGE BETWEEN FRAMES 13 AND 14, STRINGERS 20L TO 20R. MAINTENANCE REMOVED AND REPLACED THE SKIN, ALLODINED, PRIMED AND PAINTED. ALSO REMAPPED THE RVSM AREA. RVSMSep 13, 2011 · N14925 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR C2XA11ASH134Skin · corrodedSHV - DURING C-CHECK INNER FUSELAGE SKIN BETWEEN FRAMES 14-15, STRINGERS 18R-20R IS CORRODED. MAINTENANCE PERFORMED REPAIR ON INNER FUSELAGE SKIN BETWEEN FRAMES 14-15, STRINGERS 17R-21L IAW EC5330-02474. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 12, 2011 · N13929 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR C2XA11SH133Skin Splice · corrodedSHV - DURING C-CHECK LONGITUDINAL SKIN SPLICE BETWEEN FRAME 14-15, STRINGER 18L-19L CORRODED (LOCAL LEVEL 2). MAINTENANCE PERFORMED REPAIR ON LONGITUDINAL SKIN SPLICE BETWEEN FRAME 14-15, STRINGER 18L- 19L IAW EMB-145 CPM 51-21-00. THE AIRCRAFT WAS APPROVED Sep 12, 2011 · N13929 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR C2XA11SH132Skin Splice · corrodedSHV - DURING C-CHECK CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 14-15, STRINGERS 20L-15R CORRODED (LOCAL LEVEL 2). MAINTENANCE PERFORMED REPAIR ON CIRCUMFERENTIAL SPLICE BETWEEN FRAMES 13-15, STRINGERS 20L-15R IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROSep 12, 2011 · N13929 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR C2XA11TY138Sill · corrodedTYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE LT FLOOR SILL PITTED AT FR18 THRU FR 20. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB 135/145 SRM-51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Sep 10, 2011 · N14925 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA11SH035Fire Detector · defectiveSHV - FLIGHT NUMBER 4921 FROM LFT TO SHV WITH TAKEOFF THRUST ON TAKEOFF ROLL ENGINE NR 1 FIRE DET FAIL MESSAGE PRESENTED ON EICAS. NO OTHER INDICATIONS AND MESSAGE WENT AWAY WITH THROTTLE REDUCTION. MAINTENANCE VISUALLY INSPECTED FIRE LOOP AND VISUALLY INSPEFeb 5, 2011 · N12946 · Emb EMB145ER · Fire DetectionSDR C2XA10SH400Inverter · inoperativeEMERGENCY LIGHT EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT INOP. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY LIGHT INVERTER IAW EMB-145 AMM 33-50-11. OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Nov 17, 2010 · N15926 · Emb EMB145ER · Emergency LightingSDR C2XA10SH363Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM LWR FLANGE HAS CORROSION (LEVEL 2 LOCAL) FR 35-36. MAINTENANCE PERFORMED REPAIR AT LT OMEGA BEAM LOWER FLANGE FRAME 35-36 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N13978 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH362Skin · crackedSHV - DURING C-CHECK SKIN CRACKS AROUND RIVET HEAD FR 78 RT SIDE. MAINTENANCE PERFORMED REPAIR TO AFT FUSELAGE SKIN FR 78 RT SIDE IAW EC5330-02260. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR C2XA10SH361Skin · crackedSHV - DURING C-CHECK SKIN CRACKS AROUND RIVET AT RT SIDE FR 77. MAINTENANCE PERFORMED REPAIR TO AFT FUSELAGE SKIN RT SIDE FR 77 IAW EC5330-02260. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR C2XA10SH360Floor Support · corrodedSHV - DURING C-CHECK (FR 29) LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR FOR LT OMEGA BEAM L-FLANGE AT FRAME 29 IAW EMB-145 SRM 53-00-10 AND 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SEOct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH359Floor Support · corrodedSHV - DURING C-CHECK (FR 29) CTR OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON CENTER BEAM CROSSBEAM SUPPORT AT FR 29 AND RESTORED TO ORIGINAL FINISH IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APOct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH358Floor Support · corrodedSHV - DURING C-CHECK (FR 33) CTR OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE AT CARBON FIBER CROSSBEAM. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH357Floor Support · corrodedSHV - DURING C-CHECK (FR 33) LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM FR 33 IAW EMB-145 SRM 53-00-10 FIG 202 STEP 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH356Yoke · crackedSHV - DURING C-CHECK NR 1 ENGINE FWD LWR ENGINE YOKE CRACKED. MAINTENANCE REMOVED AND REPLACED NR1 ENGINE FWD LWR ENGINE YOKE IAW EC5450-01028 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Engine Mount SectionSDR C2XA10SH355Door Frame · corrodedSHV - DURING C-CHECK CARGO DOOR CUTOUT LWR STRUCTURE CORRODED (LEVEL 2 LOCAL) IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER STRUCTURE IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Main, StructureSDR C2XA10SH354Bracket · wornSHV - DURING C-CHECK RT AILERON CONTROL ROD ATTACHMENT BRACKET (I/B) ATTACHMENT POINT (I/B) BUSHING (HAT) MISSING. MAINTENANCE REMOVED AND REPLACED RT AILERON CONTROL ROD ATTACHMENT BRACKET (I/B) ATTACHMENT POINT (I/B) BUSHING (HAT) IAW EMB-145 SRM 51-40-02. Oct 25, 2010 · N15948 · Emb EMB145ER · AileronsSDR C2XA10SH353Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FR 49-50 AT CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE BETWEEN FR 49-50 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH352Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 58 CARBON CROSS MEMBER. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRAME 58 CARBON CROSS MEMBER IAW SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICOct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH351Floor Support · corrodedSHV-DURING C-CHECK CENTER OMEGA BEAM L-FLANGE AT FR 44 HAS CORROSION (LEVEL 2 LOCAL) TO CARBON CROSS MEMBER. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE AT FRM 44 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH350Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FRAME 44 TO CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FR 44 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH349Beam · corrodedSHV-DURING C-CHECK LT OMEGA BEAM LOWER SUPPORT FLANGE AT FR 54-59 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM LOWER SUPPORT FLANGE AT FRAME 54-59 IAW EMB-145 EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Structure (General)SDR C2XA10SH348Floor Support · corrodedSHV-DURING C-CHECK CENTER OMEGA BEAM L-FLANGE AT FR 49-50 AT CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM "L" FLANGE AT 49-50 AT CARBON CROSS MEMBER IAW EMB-145 SRM 51-40-02, 53-00-10 AND RESTORED TO ORIOct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH347Floor Support · corrodedSHV - DURING C-CHECK (FR 38) CTR OMEGA BEAM L-FLANGE AT CARBON FIBER CROSSBEAM HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CTR OMEGA BEAM L-FLANGE AT FRAME 38 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH346Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM AT FRAME 20 FLANGE HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 19-20 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH345Floor Support · corrodedSHV - DURING C-CHECK (FR 38) LT OMEGA BEAM L-FLANGE AT CARBON FIBER CROSSBEAM HAS CORROSION (LOCAL LEVEL 2). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRM 38 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 25, 2010 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA10SH313Beam · corrodedSHV - DURING C-CHECK RT OMEGA BEAM HAS CORROSION (LEVEL 2 LOCAL) FRAMES 19 TO 23. MAINTENANCE REMOVED AND REPLACED RT OMEGA BEAM AT FRAME 18-24 IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 15, 2010 · N14945 · Emb EMB145ER · Fuselage Main, StructureSDR C2XA10TY133Bracket · wornTYS - A/C WAS IN C-CHECK AND INSPECTION FOUND A HAT BUSHING FIT LOOSELY ON A PCA BRACKET ON LT AILERON. MAINTENANCE REMOVED AND REPLACED THE PCA BRACKET IAW E5750--01177. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED AT THE END OF THE CHECK.Sep 14, 2010 · N12946 · Emb EMB145ER · AileronsSDR C2XA10TY127Skin · gougedFUSELAGE SKIN GOUGED IN TWO PLACES INSIDE PYLON ACCESS 414DB. CUT OUT GOUGES FABRICATED AND INSTALLED A FILLER AND A CIRCULAR DOUBLER IAW EC5330-02219. AIRCRAFT RELEASED FROM C-CHECK AND RETURNED TO SERVICE.Sep 11, 2010 · N12946 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR C2XA10TY126Light · inoperativeLEFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP IAW EMB 145 AMM 33-50-10, OPS CHECK GOOD.Sep 11, 2010 · N12946 · Emb EMB145ER · Emergency Lighting
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