Embraer EMB-135LR

Service difficulty reports · 2,545

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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 = 'EMB135LR'
  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 C2XA03IA106Light · inoperativeFLIGHT 2833 - DURING PREFLIGHT INSPECTION THE FLIGHT CREW REPORTED THAT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM AND COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT WAS THEN RETURNov 24, 2003 · N27523 · Emb EMB135LR · Emergency LightingSDR C2XA03SH471Buttstrap · corrodedSHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Nov 23, 2003 · N12528 · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA03SH469Floorbeam · corrodedSHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED T-FRAME 18. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Nov 23, 2003 · N12528 · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA03SH470Buttstrap · corrodedSHV- DURING C-CHECK THE INBOARD BUTTSTRAP BETWEEN FRAMES 14 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Nov 23, 2003 · N12528 · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA03SH468Angle · corrodedSHV-DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Nov 23, 2003 · N12528 · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA03BT111Switch · out of positionCREW REPORTED, FUEL NR 1 LOW LEVEL MESSAGE CAME ON INFLIGHT ON ARRIVAL INTO EWR. NR 1 FUEL QTY INDICATOR SHOWS ZERO FUEL. DECLARED EMERGENCY AND LANDED UNEVENTFULLY IN EWR. MAINTENANCE FOUND REFUELING SWITCH TO BE IN THE OPEN POSITION ON THE REFUELING PANELNov 22, 2003 · N16510 · Emb EMB135LR · Fuel StorageSDR SIMA200332703Pin · lack of lubeCREW REPORTED SEAT TRACK WOULD NOT LOCK. MAINTENANCE REMVOED AND LUBRICATED THE LT AND RT LOCKING PINS AND LUBRICATED THE PIN SHAFTS. THE PINS WERE REINSTALLED IAW WORK CARD 25-200-07. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Nov 20, 2003 · N716AE · Emb EMB135LR · Flight Compartment EquipmentSDR SIMA200332701Seat Track · lack of lubeRDU - FLT 4852 - PILOT REPORTED AN UNCOMMANDED SEAT MOVEMENT. MAINTENANCE CLEANED AND LUBRICATED THE SEAT TRACK AND RAILS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Nov 20, 2003 · N705AE · Emb EMB135LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200334409Sill · corrodedABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING SERVICE DOOR SILL AND INSTALL NEW SILL IAW EMB STATMENT IC2003-145/0818 AND 3829. (M)Nov 18, 2003 · N724AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA03CL189Light · inoperativeCLE FLIGHT 2051 THE CREW REPORTED THE RIGHT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE RIGHT WING AFT EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD.Nov 18, 2003 · N15527 · Emb EMB135LR · Emergency LightingSDR SIMA200334408Profile · corrodedABI - DURING A IMBV INSPECTION, THE RIGHT PROFILE AFT OF FRAME 18 WAS FOUND CORRODED BELOW LIMITS AROUND NUT PLATE. CUT OUT SECTION OF CORRODED PROFILE, PERFORMED NDT INSPECTION AND TREATED BARE METAL. FABRIATED A REPAIR ANGLE. REPAIR DONE IAW EMB REPAIR STNov 17, 2003 · N724AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200334407Floor Support · corrodedABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL AS FOUND CORRODED BELOW SRM LIMITS. CUT OUT CORRODED SECTION OF THE FORWARD DIGITAL. MADE REPLACEMENT STRAP, FABRICATED SHIM, TWO DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 23, CHAPTER 53-Nov 15, 2003 · N724AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200332402Fcu · failedFLAP FAIL ON APPROACH, FLAPS STUCK AT ZERO. REPLACED FECU OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Nov 14, 2003 · N723AE · Emb EMB135LR · Trailing Edge Flap Control SystemSDR SIMA200334410Stringer · chafedDURING AN IMBV INSPECTION STRINGER 19 WAS FOUND CHAFED BELOW SRM LIMITS BETWEEN FRAMES 52R AND 53R. BLENDED THE CHAFE ON STRINGER 19R AND PERFORMED AN NDT INSPECTION. FABRICATED A REPAIR ANGLE, TWO SHIMS. REPAIRS DONE IAW EMB REPAIR STATEMENT IC2003-145/309Nov 12, 2003 · N724AE · Emb EMB135LR · Fuselage Main, Longeron/StringerSDR C2XA03CL186Inverter · failedDURING ROUTINE MAINTENANCE THE LEFT SIDE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.Nov 12, 2003 · N28529 · Emb EMB135LR · Emergency LightingSDR SIMA200331401Ecu · inoperativeDURING APPROACH, CREW REPORTED FLAPS FAILED TO DEPLOY WHEN LEVER SELECTED TO NINE DEGREES. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH ZERO FLAPS. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WASNov 8, 2003 · N717AE · Emb EMB135LR · Elevator Control SystemSDR SIMA200330901Seat Track · dirtyCAPTAIN REPORTED HIS SEAT LATCH DOES NOT REMAIN LATCHED, SEAT UNLATCHES AT TIMES BY ITSELF. COMPLIED WITH COCKPIT SEAT LOCKING PIN AND SEAT TRACK CLEANING AND LUBRICATION. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Nov 3, 2003 · N734EK · Emb EMB135LR · Fuselage, Seat/Cargo Attach FittingsSDR C2XA03CL179Fuel Nozzle · cokedCLE FLIGHT NR 2827 THE CREW REPORTED A VERY STRONG FUEL SMELL AFTER STARTING APU. MAINTENANCE INSPECTED AND REPLACED THE NR 4 AND NR 6 APU FUEL NOZZLES. OPERATIONAL CHECKS WERE GOOD.Oct 23, 2003 · N12530 · Emb EMB135LR · APU Engine Fuel and ControlSDR SIM2004F00000Floorbeam · corrodedDURING INSPECTION THE LT FLOORBEAM WAS FOUND TO BE CORRODED BELOW SRM LIMIT BETWEEN FRAMES 24 AND 25. COMPLETELY REMOVED THE CORROSION BY CREATING A CUT OUT IN THE DAMAGED FLANGE AND WEB OF THE LT FLOORBEAM. FABRICATED A REPAIR ANGLE, FILLER AND SHIMS FOR REOct 8, 2003 · N722AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200328804Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS BETWEEN FRAMES 24 AND 25. COMPLETELY REMOVED THE CORROSION BY CREATING A CUT OUT IN THE DAMAGED FLANGE AND WEB OF THE RIGHT FLOORBEAM. FABRICATED A REPAIR ANGLE, FOct 8, 2003 · N722AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200328806Floorbeam · corrodedDURING AN IMBV INSPECTION, THE CENTER SECTION OF THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED SECTION OF THE FORWARD DIGITAL BY CUTOUT. FABRICATED A REPLACEMENT FORWARD DIGITAL CENTER SECTION, FABRICATED TWO DOUBLERS, SHIMSOct 8, 2003 · N722AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200328805Floorbeam · corrodedDURING AN IMBV INSPECTION, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS BETWEEN FRAMES 24 AND 25. COMPLETELY REMOVED THE CORROSIN BY CREATING A CUT OUT IN THE DAMAGED FLANGE AND WEB OF THE LEFT OMEGA BEAM. FABRICATED A REPAIR ANGLE, FILLER ANOct 8, 2003 · N722AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200327911Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE GALLEY HAT BEAM AT FRAME 22 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PERFORMED AN NDT INSPECTION. CLEANED, TREATED AND APPLIED EPOXY PRIMER TO BLENDED AREA. FABRICATED A DOUBLER REPAIR DONOct 5, 2003 · N722AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200328201Stringer · chafedABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REINFORCEMENT ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3093A. (M)Oct 5, 2003 · N722AE · Emb EMB135LR · Fuselage Main, Longeron/StringerSDR SIMA200327909Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE GALLEY CENTER HAT BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS AT FRAME 23. BLENDED THE CORRODED AREA OF THE HAT BEAM AND PERFORMED NDT INSPECTION. CLEANED, TREATED, AND APPLIED EPOXY PRIMER TO THE BLENDED AREA. FABRICAOct 4, 2003 · N722AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200327910Sill · corrodedABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING SERVICE DOOR SILL AND INSTALLED NEW SERVICE DOOR SILL IAW EMB 145 SRM, SRM 145/1142 REV 22, CHAPTERS 51-20-03, 51-40-02 AND 51-40-06. (M)Oct 3, 2003 · N722AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA03CL172Light · inoperativeCLE FLIGHT NR 3217 THE CREW REPORTED THE EMERGENCY LIGHT OVERHEAD OF EXIT ROW IS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE BULB ON THE OVERHEAD EMERGENCY LIGHT AT EXIT ROW 9. OPERATIONAL CHECKS WERE GOOD.Oct 2, 2003 · N12528 · Emb EMB135LR · Emergency LightingSDR C2XA03IA098Bulb · burned outTHE CREW NOTED THAT THE EMERGENCY LIGHT WAS INOPERATIVE IN THE CABIN DURING PREFLIGHT. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 20, 2003 · N11526 · Emb EMB135LR · Emergency LightingSDR SIMA200326506Stringer · chafedABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R WAS FOUND TO BE CHAFED BEYOND SRM LIMITS AFT OF FRAME 52. COMPLETELY REMOVED CHAFED BY BLENDING AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA. NO DEFECTS NOTED. FABRICATED ON REPAIR ANGLESep 16, 2003 · N720AE · Emb EMB135LR · Fuselage Main, Longeron/StringerSDR SIMA200326505Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE TOP OF THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS AT FRAME 20 REMOVED CORROSION BY CREATING A CUT OUT IN THE OTP OF THE CENTER OMEGA BEAM AT FRAME 20. FABRICATED A U-SHAPED EXTERNAL DOUBLER. REPAIR DOSep 12, 2003 · N720AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200325303Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED BELOW SRM LIMITS. CUT OUT SECTION OF THE OMEGA BEAM. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2917. (M)Sep 4, 2003 · N717AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200325302Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED THE DAMAGED SECTION OF THE LEFT OMEGA BEAM, THE CUTOUT OF THE FLANGED AREA WAS EXTENDED BEYOND THAT OF THE WEB TO EMCOMPASS THE RESep 2, 2003 · N717AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200325306Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE GALLEY FLOOR CENTER BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER BEAM AND INSTALLED NEW BEAM. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, 51-40-02, AND 51-40-04 AND CPM 51-21-04. (M)Sep 2, 2003 · N717AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200325305Stringer · chafedABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R WAS FOUND TO BE CHAFED BEYOND SRM LIMITS AFT OF FRAME 52. COMPLETELY REMOVED CHAFED BY BLENDING AREA. PERFORMED EDDY CURRENT INSPECTION OF THE BLENDED AREA. NO DEFECTS NOTED. FABRICATED ONE REPAIR ANGLE, Sep 2, 2003 · N717AE · Emb EMB135LR · Fuselage Main, Longeron/StringerSDR SIMA200325304Sill · corrodedABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER SILL AND INSTALLED A NEW SILL. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 22, 51-40-02 AND EMB REPAIR STATEMENT IC2003-145/081Sep 1, 2003 · N717AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200324601Seat Track · dirtyBGR - FLT 4622 - DURING TAKEOFF, THE FIRST OFFICERS SEAT SLIPPED LOOSE TO THE FULL AFT POSITION. MAINTENANCE FOUND THE OUTBOARD SEAT TRACK TO BE DIRTY. SEAT TRACKS WERE INSPECTED, SEAT TRACK PIS WERE REMOVED, CLEANED AND REINSTALLED IAW EMB MM. OPS CHECK WAAug 31, 2003 · N738NR · Emb EMB135LR · Fuselage, Seat/Cargo Attach FittingsSDR C2XA03CL157Sign · malfunctionedCLE FLIGHT NR 2130 THE CREW REPORTED THE PAX DOOR EMERGENCY EXIT SIGN OVER THE FLIGHT ATTENDANTS SEAT INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL TEST OF EXIT SIGN.OPERATIONAL TESTS CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.Aug 29, 2003 · N28518 · Emb EMB135LR · Emergency LightingSDR SIMA200324604Skin · crackedABI - DURING AN IMBV INSPECTION, A CRACK WAS DISCOVERED ON THE LEFT FUSELAGE SKIN BETWEEN FRAMES 48 AND 49 AT THE OVERWING PANEL AFT UPPER ATTACH POIT. PERFORMED CUT OUT OF THE DAMAGE AREA. FABRICATED A FILLER, REPAIR DOUBELR. REPAIR DONE IAW EMB 145 SRM, SAug 25, 2003 · N718AE · Emb EMB135LR · Fuselage Main, Plate/SkinSDR SIMA200324603Beam · corrodedABI - DURING AN IMBV INSPECTION, THE GALLEY CENTER BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. PERFORMED CUT OUT OF THE DAMAGED AREA. FABRICATED REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTERS 53-21-10 PARA 5 FAug 24, 2003 · N718AE · Emb EMB135LR · Fuselage Main, StructureSDR C2XA03CL149Inverter · inoperativeCLE FLIGHT NR 2138 THE CREW REPORTED THE NR 2 AND NR 3 EMERGENCY LIGHTS DID NOT WORK. MAINTENANCE REPLACED THE NR 3 INVERTER. OPERATIONAL CHECKS WERE GOOD.Aug 24, 2003 · N14522 · Emb EMB135LR · Emergency LightingSDR SIMA200324611Floorbeam · corrodedABI - FOUND DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/27Aug 21, 2003 · N716AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200323602Sign · inoperativeDURING PREFLIGHT CREW REPORTED THE LEFT WING EXIT SIGN DID NOT WORK. AIRCRAFT WAS INSPECTED AND FERRIED TO LGA FOR CORRECTIVE ACTION. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.Aug 20, 2003 · N707EB · Emb EMB135LR · Emergency LightingSDR SIMA200324607Sill · corrodedABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING SERVICE DOOR CENTER SILL AND INSTALLED NEW SILL IAW EMB SRM, SRM EMB-145/1142 REV 22, CHAPTERST 51-40-02, 51-20-01, 51-20-03, 51-40-06 ANAug 15, 2003 · N716AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200324606Frame · dentedABI - DURING AN IMBV INSPECTION, THE LOWER RIGHT SECTION OF FRAME 72 WAS FOUND TO BE CREASED AND DENTED. REMOVED THE DAMAGED LOWER SECTION OF FRAME 72. INSTALLED NEW FRAME IAW EMB SRM, SRM 145/1142 REV 22, 51-40-02 AND STANDARD SRM PRACTICES. (M)Aug 14, 2003 · N719AE · Emb EMB135LR · Fuselage Main, FrameSDR SIMA200324608Stringer · chafedABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R WAS FOUND TO BE CHAFED BEYOND SRM LIMITS AFT OF FRAME 52. COMPLETELY REMOVED CHAFE BLENDING AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA. NO DEFECTS NOTED. FABRICATED ONE REPAIR ANGLE, TAug 14, 2003 · N719AE · Emb EMB135LR · Fuselage Main, Longeron/StringerSDR SIMA200324605Sill · corrodedABI - DURING AN IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED CENTER SILL AND INSTALLED NEW SILL IAW EMB 135 SRM, SRM 145/1142 REV 22, 51-40-02, 06, 51-20-03 EMB 145 CPM 51-21-04, 51-21-05. (M)Aug 13, 2003 · N719AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA03IA091Light · inoperativeIAH-DURING PREFLIGHT THE CREW NOTED THAT THE ROW 9 OVERHEAD EMERGENCY LIGHTS FAILED TO ILLUMINATE ABOVE SEATS 9A, AND, 9B. IAH- MAINTENANCE REMOVED AND REPLACED THE LIGHT BULBS IN THE EXIT LIGHT, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEMAug 13, 2003 · N14516 · Emb EMB135LR · Emergency LightingSDR SIMA200323004Floorbeam · corrodedDURING AN IMBV INSPECTION, THE CENTER FLOORBEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED BELOW SRM LIMITS. PERFORMED A CUT OUT OF THE DAMAGED ARAE. FABRICATED A REPAIR DOUBLER, FILLER AND TWO SHIMS FOR REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/114Aug 12, 2003 · N719AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200323005Floorbeam · corrodedDURING AN IMBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. PERFORMED A CUT OUT OF THE DAMAGED FLOORBEAM. FABRICATED A REPAIR ANGLE, FILLER, FORWARD SHIMS, AFT SHIMS AND PLATE. REPAIR DONE IAW EMB 145 SRM, SRM EMB 14Aug 12, 2003 · N719AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200322508Beam · corrodedABI - DURING AN IMBV INSPECTION, THE GALLEY AREA CENTER HAT BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING HAT BEAM AND INSTALLED NEW HAT BEAM IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTERS 51-40-02 AND 51-20-03. (M)Aug 10, 2003 · N719AE · Emb EMB135LR · Fuselage Miscellaneous Structure
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