Embraer EMB-135ER

Service difficulty reports · 465

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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 = 'EMB135ER'
  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 C2XA03TY203Tie Rod · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND WING TO FUSELAGE TIE ROD ASSEMBLE. MAINTENANCE REMOVED AND REPLACED THE TIE ROD IAW EMB IC 2003-145/4092. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Dec 7, 2003 · N17507 · Emb EMB135ER · Wing, Fuselage Attach FittingsSDR C2XA03TY202Support Fitting · damagedDURING A SCHEDULED 2C INSPECTION THE LT AND RT VERT STAB SPHERICAL BEARINGS HAD AXIAL PLAY. MAINT REMOVED THE SPHERICAL BEARINGS, REAMED AND INSTALL THE 1ST OVERSIZE BUSHINGS, REINSTALL BEARINGS AND PERFORMED A DIEHEDRIAL CHECK IAW EC5510-01045; EC5510-01069 Dec 3, 2003 · N27506 · Emb EMB135ER · Vertical StabilizerSDR C2XA03TY198Sill · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR FORWARD SILL. MAINTENANCE REMOVED AND REPLACED THE DOOR SILL IAW EMB SRM 51-40-02 AND CPM 51-21-05/06, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTDec 2, 2003 · N27506 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03TY201Floor Support · corrodedTYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FRAMES 18 TO 23. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTIONDec 2, 2003 · N17507 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03TY200Fitting · wornDURING A SCHEDULED INSPECTION THE LEFT HAND AILERON PCA INBOARD ATTACH FITTING FLANGE HOLE WAS WORN OUT OF ROUND. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND AILERON PCA ATTACH FITTING IAW EC 5750-01177 AND CPM 51-21-05/06, THE REPAIR WAS SATISFACTORY. THDec 2, 2003 · N17507 · Emb EMB135ER · Wing, Attach FittingsSDR C2XA03TY199Floor Support · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT JUST AFT OF MAIN DOOR. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSDec 2, 2003 · N27506 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03TY192Engine · failedAIRCRAFT AIR-RETURNED TO CLE, EMERGENCY DECLARED, THE LEFT ENGINE FAILED IN FLIGHT, ITT SPIKED AT 1100 DEG C, WITH A LOUD BANG. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE, OPS AND LEAK CHECKED GOOD IAW EMB135-MM-71-00-00 AND TASK CARD 6271001. AIRCRAFTNov 7, 2003 · N27512 · Emb EMB135ER · Engine (Turbine/Turboprop)SDR C2XA03SH396Inverter · inoperativeDURING C-CHECK THE NR 1 EMERGENCY AISLE LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 INVERTER IAW EMB 135 AMM 33-50-11. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 18, 2003 · N25504 · Emb EMB135ER · Emergency LightingSDR C2XA03SH387Buttstrap · corrodedSHV- DURING C-CHECK THE LEFT BUTTSTRAP BETWEEN FRAMES 18 AND 23 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.Oct 14, 2003 · N25504 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03SH386Floorbeam · corrodedSHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 19 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10 FIGURE 201 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 14, 2003 · N25504 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA03SH385Buttstrap · corrodedSHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP BETWEEN FRAMES 15 AND 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A NEW SECTION IAW EMB 135 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 14, 2003 · N25504 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03SH376Strap · corrodedSHV- DURING C-CHECK THE CENTER STRAP AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 8, 2003 · N25504 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03SH375Crossbeam · corrodedDURING C-CHECK THE CROSSBEAM AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 8, 2003 · N25504 · Emb EMB135ER · Fuselage Main, StructureSDR C2XA03SH374Sill · corrodedSHV- DURING C-CHECK THE RIGHT HAND SILL AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 8, 2003 · N25504 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03SH372Stiffener · chafedSHV- DURING C-CHECK THE NUMBER 2 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 7, 2003 · N25504 · Emb EMB135ER · Engine Cowling SystemSDR C2XA03SH371Buttstrap · corrodedSHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 23 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.Oct 7, 2003 · N25504 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03SH370Buttstrap · corrodedDURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 17 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.Oct 7, 2003 · N25504 · Emb EMB135ER · Fuselage Main, StructureSDR 2003FA0001004Button · crackedINDICATOR BUTTON FAILURE OCCURED ON THREE UNITS AND CRACKS CLEARLY EVIDENT ON TWO OTHERS IN SAME AREA OF BREAKAGE. ONCE BROKEN, A SECTION OF THE BUTTON CAN TRAVEL BEYOND THE SEALED AREA OF THE HOUSING AND HAS THE CAPABILITY OF ALLOWING A FUEL LEAK OF UP TO 1.5Sep 26, 2003 · Emb EMB135ER · APU Engine Fuel and ControlSDR C2XA03TY166Floorbeam · corrodedDURING A SCHEDULED 2C INSPECTION THE LT FLOORBEAM WAS FOUND CORRODED. MAINT. REMOVED AND FAB. A NEW FLOORBEAM. CLEANED SURFACE CORROSION,PRIMED,PAINTED AND INSTALL THA NEW FAB. PART IAW EMB 135/145 SRM 51-10-03 AND CPM 51-21-03,05,06. ALL WORK WAS ACCOMPLISHEDSep 22, 2003 · N19503 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA03TY163Strap · corrodedTYS DURING A SCHEDULED 2C INSPECTION THE FWD DIGITAL IN GALLEY WAS FOUND CORRODED. MAINT. R/R THE FWD DIGITAL,ALLODINED,PRIMED AND PAINTED IAW EMB 135/145 SRM 53-21-10 AND EMB 135/145 CPM51-21-04,05,06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETISep 13, 2003 · N19503 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03TY162Gusset · corrodedDURING A SCHEDULED 2C INSPECTION THE AFT GUSSET WAS FOUND CORRODED IN SEVERAL SPOTS. MAINT. R/R THE AFT GUSSET IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.Sep 13, 2003 · N19503 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03TY161Floorbeam · corrodedDURING A SCHEDULED INSPECTION THE RT HAND FORWARD DIGITAL UNDER THE GALLEY WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04,05AND 06. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPSep 11, 2003 · N16502 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA03TY160Angle · corrodedTYS DUEING A SCHEDULED INSPECTION THE LEFT HAND FORWARD RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Sep 11, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03TY159Floorbeam · corrodedDURING A SCHEDULED INSPECTION THE FORWARD FLOORBEAM TOP CAP WAS FOUND TO BE CORRODED UNDER SEAT TRACK LF1. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB SRM 51-40-02 AND M.M. 53-01-06, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COSep 11, 2003 · N16502 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA03TY158Sill · damagedDURING A SCHEDULED INSPECTION, DAMAGE WAS FOUND TO THE SERVICE DOOR FORWARD SILL AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR SILL IAW EMB SRM 53-00-04, 51-40-02, 51-30-01 AND CPM 51-21-04, 05. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL Sep 11, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03TY157Axle · damagedDURING A SCHEDULED INSPECTION THE RIGHT MLG RETRACTION AXLE CHROME PLATED AREA DAMAGED. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG RETRACTION AXLE I/A/W-EMB-135-AMM-32-10-03. OPS AND LEAK CHECKED GOOD.Sep 10, 2003 · N16502 · Emb EMB135ER · Main Landing Gear Strut/Axle/TruckSDR C2XA03TY156Sill · damagedDURING A SCHEDULED INSPECTION, DAMAGE WAS FOUND TO THE MAIN DOOR SILL SKIN, MAINTENANCE REMOVED AND REPLACED THE SILL I/A/W-EMB-135-AMM-53-21-00.Sep 10, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03TY155Skin · dentedDURING A SCHEDULED INSPECTION 2 DENTS WHERE FOUND AFT OF THE PAX DOOR BETWEEN FRAMES 19 AND 20, ABOVE STR 12L. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED A FILLER AND DOUBLER, ALIDINED, INSTALLED THE PATCH, PRIMED AND PAINTED. I/A/W-EMB-135/145-SRM-53-21Sep 10, 2003 · N16502 · Emb EMB135ER · Fuselage Main, Plate/SkinSDR C2XA03TY153Bearing Cap · crackedDURING A SCHEDULED INSPECTION THE RIGHT HAND AFT MAIN LANDING GEAR BEARING CAP FAILED NDI FOR CRACKS AT THE MOUNTING HOLES. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND AFT MAIN LANDING GEAR BEARING CAP IAW EMB M.M. 32-10-01, THE REPAIR WAS SATISFACTORY. Sep 10, 2003 · N16502 · Emb EMB135ER · Main Landing GearSDR C2XA03TY152Cap · crackedDURING A SCHEDULED INSPECTION THE LT MLG BEARING CAP FAILED NDI FOR CRACKS AT THE MOUNTING HOLES. MAINTENANCE REMOVED AND REPLACED THE BEARING CAP IAW EMB M.M. 32-10-01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTIONSep 10, 2003 · N16502 · Emb EMB135ER · Main Landing GearSDR C2XA03TY151Floorbeam · corrodedDURING A SCHEDULED INSPECTION THE FLOORBEAM AT FRAME 22 RT, WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 22 IAW EMB SRM 51-40-02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPOSep 10, 2003 · N16502 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA03TY150Gusset · corrodedDURING A SCHEDULED INSPECTION THE GALLEY FLOOR AFT GUSSET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT GUSSET IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Sep 10, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03TY149Plate · corrodedDURING A SCHEDULED INSPECTION THE GALLEY RIGHT HAND AFT CROSS BEAM PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CROSS BEAM PLATE IAW EMB SRM 51-10-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPESep 10, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03TY148Cam · corrodedDURING A SCHEDULED INSPECTION THE NOSE LANDING GEAR STRUT MAIN HOUSING AND LOWER CAM WERE FOUND TO HAVE AREAS OF CORROSION AND PITTING. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR LEG ASSEMBLY IAW EMB MM 32-20-01, ALL OPERATIONAL AND LEAK CHECKS WESep 10, 2003 · N16502 · Emb EMB135ER · Nose/Tail Landing GearSDR C2XA03TY147Bracket · corrodedDURING A SCHEDULE INSPECTION THE MAIN PASSENGER DOOR THRESHOLD BRACKETS WERE FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE THRESHOLD BRACKETS IAW EMB SRM 51-40/02, 51-30-02 AND CPM 51-21-04,05 AND 06. THE REPAIR WAS FOUND TO SATSep 10, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03TY145Sill · corrodedTYS DURING A SCHEDULED INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR SILL IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Sep 4, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03TY144Buttstrap · corrodedTYS DURING A SCHEDULED 2C INSPECTION THE FWD DIGITAL BUTTSTRAP WAS CORRODED. MAINT REMOVED THE FWD DIGITAL, FAB A DOUBLER AND INSTALL A NEW FWD DOUBLER, ALLODINED, PRIMED AND PAINTED. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.Aug 30, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03TY142Floorbeam · corrodedTYS DURING A SCHEDULED 2C INSPECTION THE FLOORBEAM AT FR 22 RT SIDE WAS FOUND CORRODED IN SEVERAL AREAS. MAINT R&R THE FLOOR BEAM AT FR 22 IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.Aug 28, 2003 · N16502 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA03TY141Plate · corrodedTYS DURING A SCHEDULED 2C INSPECTION THE RT AFT CROSS BEAM PLATE WAS CORRODED. MAINT R&R THE AFT CROSS BEAM PLATE IAW EMB 135/145 SRM 51-10-02 ALLODINED, PRIMED AND PAINTED REWORK AREA IAW EMB 135/145 CPM 51-21-04'05'06. ALL WORK WAS ACCOMPLISHED AND WILL BAug 28, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03TY140Gusset · corrodedTYS DURING A SCHEDULED 2C INSPECTION THE AFT GUSSET WAS FOUND WITH SEVERAL AREAS THAT WAS CORRODED. MAINT R&R THE AFT GUSSET IAW 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK.Aug 28, 2003 · N16502 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA03CL146Proximity Switch · defectiveCVG FLIGHT NR 2645 THE CREW REPORTED AFTER GEAR RETRACTION THE NOSE GEAR DOOR REMAINED OPENED. THE GEAR WAS RECYCLED AND ON THE 2ND RETRACTION THE MAIN GEAR REMAINED DOWN WITH LANDING GEAR LEVER DISAGREE. THE AIRCRAFT RETURNED TO CVG AND LANDED WITHOUT FURTHAug 18, 2003 · N19503 · Emb EMB135ER · Landing Gear Position and WarningSDR C2XA03CL140Dau · faultyCLE FLIGHT NR 2802 THE CREW REPORTED THE NR 1 ENGINE SHOWED NO FUEL FLOW WHILE ENGINE NR 1 WAS RUNNING. MAINTENANCE INSPECTED AND REPLACED THE NR 1 DAU. OPERATIONAL CHECKS WERE GOOD.Aug 7, 2003 · N19503 · Emb EMB135ER · Central ComputersSDR C2XA03CL130Light · inoperativeCLE FLIGHT 2239, THE CREW REPORTED THE EMERGENCY LIGHT IN THE GALLEY WAS INOPERATIVE. MAINTENANCE REPLACED THE GALLEY EMERGENCY LIGHT, OPERATIONAL CHECKS WERE GOOD.Jul 29, 2003 · N25504 · Emb EMB135ER · Emergency LightingSDR C2XA03CL110Wire · brokenCLE FLIGHT 2008 THE CREW REPORTED AISLE PATH LIGHTING STRIP INOPERATIVE BY LAVATORY. MAINTENANCE REPAIRED BROKEN WIRE ON LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.Jun 12, 2003 · N14505 · Emb EMB135ER · Light System WiringSDR C2XA03CL106Control Handle · failedTHE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Jun 6, 2003 · N14505 · Emb EMB135ER · Landing Gear SelectorSDR C2XA03CL105Electrical Box · failedCLE FLIGHT 2226 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD.Jun 6, 2003 · N14505 · Emb EMB135ER · Landing Gear Retraction/Extension SystemSDR C2XA03CL104Light · inoperativeCLE FLIGHT 2083, THE CREW REPORTED AISLE PATH EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.Jun 5, 2003 · N15509 · Emb EMB135ER · Emergency LightingSDR C2XA03BT061Battery · inoperativeCREW (DURING WALKAROUND) NOTICED THE EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERIES AND OPS CHECKED SYSTEM GOOD.May 24, 2003 · N27512 · Emb EMB135ER · Emergency LightingSDR SWIA200312115Stringer · crackedLEFT NACELLE OUTBOARD STRINGER CRACKED AT RIVET HOLES. FOUND DURING C-CHECK INSPECTION. APPLIED DOUBLER TO CRACKED AREA IAW SRM120 51-10-02.May 22, 2003 · N189SW · Emb EMB135ER · Nacelle/Pylon, Longeron/StringerSDR C2XA03CL081Control Cable · looseCLE FLT 2828 THE CREW REPORTED ELEVATOR LOST EFFECTIVENESS ON FINAL AT 130-125 KIAS. ELEVATOR FEELS SLOPPY ON GROUND. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MX ADJUSTED CABLE TENSIONS AND REMOVED AND REPLACED CAPTAINS ELEVATOR CABLE TENSIONER/REGULATOR OPMar 31, 2003 · N25504 · Emb EMB135ER · Elevator Control System
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