Embraer EMB-135ER

Service difficulty reports · 465

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 = '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 C2XA04SH243Floorbeam · corrodedSHV- DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 24, 2004 · N27512 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA04SH242Firewall · crackedSHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE TOP OF THE RIGHT VERTICAL STIFFENER. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 23, 2004 · N27512 · Emb EMB135ER · APU Cowling/ContainmentSDR C2XA04SH241Floorbeam · corrodedSHV- DURING C-CHECK THE CENTER FLOORBEAM AT FRAME 18 TO 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 23, 2004 · N27512 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA04SH240Bracket · corrodedSHV- DURING C-CHECK THE PASSENGER DOOR THRESHOLD AFT BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 23, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH239Bracket · corrodedSHV- DURING C-CHECK THE PASSENGER DOOR FORWARD THRESHOLD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 23, 2004 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH238Structure · gougedSHV- DURING C-CHECK THE STRINGER REINFORCEMENT ON STRINGER 19 RIGHT WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5310-01260. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 23, 2004 · N27512 · Emb EMB135ER · Fuselage Main, Longeron/StringerSDR C2XA04CL033Drag Strut · seizedCLE FLIGHT 2127 THE CREW REPORTED ON APPROACH THE NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. THE CREW FOLLOWED THE QRH AND ACCOMPLISHED LANDING GEAR EXTENSION. ALL GEAR INDICATED DOWN AND LOCKED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCEApr 8, 2004 · N27512 · Emb EMB135ER · Nose/Tail Landing GearSDR C2XA04SH181Rib · gougedSHV- DURING C-CHECK THE NR 1 ENGINE UPPER COWLING, AFT OUTBOARD RIB WAS FOUND TO BE GOUGED. 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.Mar 24, 2004 · N15509 · Emb EMB135ER · Nacelle/Pylon, Frame/Spar/RibSDR C2XA04SH180Strap · corrodedSHV- DURING C-CHECK THE AFT FLOORBEAM AT FRAME 17 TO 19 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVMar 24, 2004 · N15509 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA04SH179Strap · corrodedSHV- DURING C-CHECK THE FORWARD FLOORBEAM AT FRAME 16 TO FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DIGITAL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 24, 2004 · N15509 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA04CL024Lamp · inoperativeDURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP FOR THE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD.Mar 19, 2004 · N19503 · Emb EMB135ER · Emergency LightingSDR C2XA04TY051Sill · corrodedTYS, DURING A SCHEDULED INSPECTION THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR CUTOUT LOWER SILL IAW EMB-135 SRM 51-40-02.Mar 13, 2004 · N16510 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04TY049Channel · corrodedTYS DURING A SCHEDULED 2C INSPECTION A GOUGE WAS FOUND AT FR 15, STR 16L. MAINT REPAIRED CENTER FUSELAGE 1 AT LT FLOOR CROSSBEAM. ALODINED, PRIMED AND PAINTED IAW IC 2004-145/0816 AND CPM 51-21-04;05;06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON Mar 12, 2004 · N16510 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04TY048Sill · corrodedTYS DURING A SCHEDULED 2C INSPECTION THE SERVICE DOOR FWD SILL WAS FOUND CORRODED. MAINT BLENDED AND MEASURED AREA, FAB AND INSTALL DOUBLER IAW EMB 135/145 SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.Mar 12, 2004 · N16510 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04TY047Floorbeam · corrodedTYS DURING A SCHEDULED 2C INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT THE GALLEY AREA. MAINT REMOVED AND REPLACED THE RAMP ANGLE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.Mar 12, 2004 · N16510 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA04TY041Bracket · corrodedTYS DURING A SCHEDULED 2C INSPECTION THE PAX DOOR SILL BRACKETS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE FORWARD AND AFT PAX DOOR SILL BRACKETS IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WOMar 4, 2004 · N16510 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04TY040Sill · corrodedTYS DURING A SCHEDULED 2C INSPECTION THE LT WALL FLOOR SILL WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE LT FLOOR SILL AFT OF PAX DOOR IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.Mar 4, 2004 · N16510 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH113Control Panel · inoperativeSHV- DURING C-CHECK THE EMERGENCY LIGHT PUSH BUTTON ON THE FLIGHT ATTENDANTS CONTROL PANEL WOULD NOT OPERATE THE EMERGENCY LIGHTING TEST. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANTS CONTROL PANEL IAW EMB 135 AMM II 25-27-09. THE AIRCRAFT WAS APPROFeb 27, 2004 · N14508 · Emb EMB135ER · Emergency LightingSDR C2XA04SH108Support · corrodedDURING C CHECK THE MAIN DOOR THRESHOLD SILL SUPPORT WAS FOUND TO BE CORRODED AT FRAME 15 TO 18 AND STRINGER 15 LT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL SUPPORT IAW AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 26, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH107Stringer · corrodedSHV- DURING C-CHECK THE CENTER OMEGA BEAM STRINGER FROM FRAMES 22 TO 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRINGER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 26, 2004 · N14508 · Emb EMB135ER · Fuselage Main, Longeron/StringerSDR C2XA04SH106Buttstrap · corrodedSHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE BLENDED OUT THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 26, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH105Hinge Bracket · corrodedSHV- DURING C-CHECK THE UPPER CENTER HINGE BRACKET ON THE VERTICAL STABILIZER TO THE RUDDER WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 AMM 20-10-01 AND EMB 135 IPC 55-31-00. THE AIRCRAFT WAS APPROVED FOR RETURFeb 26, 2004 · N14508 · Emb EMB135ER · Vertical StabilizerSDR C2XA04SH104Crossbeam · corrodedSHV- DURING C-CHECK THE CROSSBEAM AT FRAME 22 BETWEEN THE CENTER OMEGA BEAM AND THE SERVICE DOOR AFT SILL 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 SERVFeb 26, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH103Skin · chafedSHV- DURING C-CHECK THE RIGHT HAND LOWER COWLING SKIN WAS FOUND TO BE CHAFED IN TWO AREAS BETWEEN STATIONS XN=2180.0 AND XN=2905.0. MAINTENANCE REMOVED THE DAMAGED AREAS AND PERFORMED DOUBLER REPAIRS IAW EMB 135 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR REFeb 26, 2004 · N14508 · Emb EMB135ER · Engine Cowling SystemSDR C2XA04SH102Stiffener · chafedSHV- DURING C-CHECK THE RIGHT HAND LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 26, 2004 · N14508 · Emb EMB135ER · Engine Cowling SystemSDR C2XA04CL012Connector · looseCLE FLIGHT 2152 THE CREW REPORTED THE FORWARD AISLE PATH EMERGENCY LIGHT WAS INTERMITTENT WHEN TESTED. MAINTENANCE INSPECTED AND RESECURED THE CONNECTION ON THE FORWARD EMERGENCY LIGHT STRIP. OPERATIONAL CHECK WAS GOOD.Feb 23, 2004 · N15509 · Emb EMB135ER · Emergency LightingSDR C2XA04SH088Structure · chafedSHV- DURING C-CHECK THE NR 1 ENGINE UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 20, 2004 · N14508 · Emb EMB135ER · Engine Cowling SystemSDR C2XA04SH087Structure · chafedSHV- DURING C-CHECK THE AFT EDGE MEMBER ON THE NR 2 ENGINE UPPER COWLING WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 20, 2004 · N14508 · Emb EMB135ER · Engine Cowling SystemSDR C2XA04SH086Floorbeam · corrodedSHV- DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 1SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA04SH085Floorbeam · corrodedSHV- DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA04SH084Sill · corrodedSHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LOWER SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH083Splice · gougedSHV- DURING C-CHECK STRINGER 19 LEFT INTERNAL SPLICE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPLICE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH082Angle · corrodedSHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH081Bracket · corrodedSHV- DURING C-CHECK THE PASSENGER DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH080Sill · corrodedSHV- DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FORWARD SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH079Buttstrap · corrodedSHV- DURING C-CHECK THE CENTER BUTTSTRAP 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.Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH078Buttstrap · corrodedSHV- DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED AROUND THE SCREW HOLES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04SH077Stringer · gougedSHV- DURING C-CHECK STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-24-02 AND EC 5320-01106. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Main, Longeron/StringerSDR C2XA04SH070Buttstrap · corrodedSHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED IN THE LAVATORY BETWEEN FRAMES 55 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 16, 2004 · N14508 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA04SH060Sill · corrodedSHV-DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAMES 18 AND 24 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.Feb 12, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04CL011Light · inoperativeCLE FLIGHT 2683 THE CREW REPORTED THE FIRST EMERGENCY AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE FIRST FLOOR LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.Feb 9, 2004 · N16501 · Emb EMB135ER · Emergency LightingSDR C2XA04CL007Connector · looseCLE FLIGHT 2028 THE CREW REPORTED THE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND RECONNECTED LOOSE CONNECTOR. OPERATIONAL CHECKS WERE GOOD.Feb 2, 2004 · N14505 · Emb EMB135ER · Emergency LightingSDR C2XA04TY019Sill · corrodedDURING A SCHEDULED INSPECTION THE CARGO DOOR LOWER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL BEAM. IAW-EMB-SRM-51-40-02.Jan 18, 2004 · N14505 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA04TY006Attach Fitting · gougedDURING A SCHEDULED INSPECTION, GOUGES WERE FOUND ON THE INNER BEARING MATING SURFACES AT THE HORIZONTAL STABILIZER ATTACH POINT. MAINTENANCE ACCOMPLISHED A REAM TO FIRST OVERSIZE REPAIR IAW EC5530-01062, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEJan 10, 2004 · N16501 · Emb EMB135ER · Vertical Stabilizer, Attach FittingsSDR C2XA03CL212Battery · dischargedCLE FLIGHT 2026 THE CREW REPORTED THE EMERGENCY LIGHT AT THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.Dec 26, 2003 · N16510 · Emb EMB135ER · Emergency LightingSDR C2XA03CL217Battery · dischargedTHE CREW REPORTED THE EMERGENCY EXIT LIGHTING WOULD NOT REMAIN ILLUMINATED DURING TESTING. MAINTENANCE RECHARGED THE EMERGENCY EXIT LIGHTING BATTERIES. OPERATIONAL CHECKS WERE GOOD.Dec 25, 2003 · N16510 · Emb EMB135ER · Emergency LightingSDR C2XA03CL202Access Door · stickingCLE FLIGHT 2438 THE CREW REPORTED, COULD NOT OPEN THE LANDING GEAR EMERGENCY EXTENSION ACCESS DOOR LOCATED IN THE COCKPIT. MAINTENANCE INSPECTED AND LUBED AND UNSTUCK THE ACCESS DOOR. OPERATIONAL CHECKS WERE GOOD.Dec 19, 2003 · N27512 · Emb EMB135ER · Accessory Compartment DoorsSDR C2XA03CL203Battery Pack · dischargedDURING ROUTINE MAINTENANCE THE SECOND AND THIRD EMERGENCY AISLE PATH LIGHT STRIPS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD.Dec 18, 2003 · N16510 · Emb EMB135ER · Emergency LightingSDR C2XA03TY206Spar · crackedDURING A SCHEDULED INSPECTION DAMAGE WAS FOUND ON THE RUDDER 1 AFT SPAR. MAINTENANCE ACCOMPLISHED A SPLICE REPAIR IAW EC 5540-01022 AND EMB CPM 51-21-04/05, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Dec 8, 2003 · N27506 · Emb EMB135ER · Rudder, Spar/RibSDR C2XA03TY204Tie Rod · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND WING TO FUSELAGE TIE ROD ASSEMBLY. 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 Fittings
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