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 C2XA02CL043Acm · seizedTHE CREW REPORTED A PACK 2 OVERLOAD EICAS MESSAGE. F/A REPORTED A BURNING SMELL IN CABIN. MAINTENANCE INSPECTED AND REPLACED THE NR 2 AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 9, 2002 · N25504 · Emb EMB135ER · Cabin Cooling SystemSDR C2XA02CL042Meter · inoperativeCLE FLIGHT 3061 THE CREW REPORTED THE NR 1 FUEL FLOW INDICATOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 FUEL FLOW METER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 9, 2002 · N25504 · Emb EMB135ER · Fuel Flow SensorSDR C2XA02CL040Connector · looseCLE FLIGHT# 3084 THE CREW REPORTED THE EMERGENCY LIGHT BELOW COCKPIT DOOR WAS INOPERATIVE.MAINTENANCE INSPECTED AND RESECURED THE CONNECTOR ON THE LIGHT ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.Feb 9, 2002 · N17507 · Emb EMB135ER · Emergency LightingSDR C2XA02CL039Receptacle · burnedCLE FLIGHT 3208 THE CREW REPORTED A BURNING SMELL AT THE COFFEE POT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 COFFEE POT RECEPTACLE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 8, 2002 · N17507 · Emb EMB135ER · Buffet/GalleysSDR C2XA02CL034Sign · inoperativeCLE FLIGHT 3144 THE CREW REPORTED THE EXIT SIGN IN THE FORWARD CABIN DID NOT ILLUMINATE. MAINTENANCE REPLACED THE EXIT SIGN. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 6, 2002 · N17507 · Emb EMB135ER · Emergency LightingSDR C2XA02CL031Firewall · crackedDURING ROUTINE MAINTENANCE THE APU FIREWALL WAS FOUND CRACKED AT UPPER RIGHT CORNER OF FIREWALL.THE FIREWALL WAS REPAIRED I/A/W EMBRAER GST-0401/02.THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 3, 2002 · N14508 · Emb EMB135ER · Fuselage Structure (General)SDR C2XA02CL030Odor · detectedTHE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN WHEN THE APU WAS STARTED ON THE GROUND. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS AND NO DEFECTS WERE NOTED.THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 2, 2002 · N19503 · Emb EMB135ER · Air Distribution SystemSDR C2XA02CL028Battery · dischargedDURING ROUTINE MAINTENANCE THE EMERGENCY LIGHTS AT THE OVERWING EXITS WERE FOUND TO BE INOPERATIVE.MAINTENANCE REPLACED THE #3 EMERGENCY LIGHT BATTERY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.Jan 31, 2002 · N27506 · Emb EMB135ER · Emergency LightingSDR C2XA02CL027Engine · failedCLE FLIGHT 3052 THE CREW REPORTED THE NR 2 ENGINE SHUT DOWN IN FLIGHT UNCOMMANDED. THEY REPORTED A LOUD BANG AND HIGH ITT. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE.OPERATIONAL CHECKS WERE GOOD. THE AIRJan 29, 2002 · N16510 · Emb EMB135ER · Engine (Turbine/Turboprop)SDR C2XA02CL020Sensor · false activationCLE FLIGHT#4010 THE CREW REPORTED A LAV SMOKE WARNIG ON CLIMBOUT.THE MESSAGE CLEARED AFTER 20 SECONDS.MAINTENANCE REPLACED THE LAV SMOKE SENSOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.Jan 24, 2002 · N14505 · Emb EMB135ER · Smoke DetectionSDR C2XA02CL012Switch · out of adjDURING A 2A INSPECTION MAINTENANCE FOUND THE RIGHT HAND OVERWING EMERGENCY EXIT DID NOT PRODUCE A MESSAGE ON THE EICAS WHEN THE DOOR WAS OPEN. MAINTENANCE ADJUSTED THE MICROSWITCH ON THE RIGHT HAND EMERGENCY EXIT DOOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCJan 18, 2002 · N16510 · Emb EMB135ER · Door Warning SystemSDR C2XA02CL011Connector · looseCLE FLIGHT 4014, THE CREW REPORTED THE EXIT SIGN BY THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESET THE NR 1 BATTERY PACK CONNECTOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Jan 17, 2002 · N17507 · Emb EMB135ER · Light System WiringSDR C2XA02CL007Light · inoperativeCLE FLIGHT 3084 THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE BY EXIT DOOR. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY AISLE PATH LIGHT STRIP AT ROW 8. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Jan 12, 2002 · N19503 · Emb EMB135ER · Emergency LightingSDR C2XA02TY002Battery · dischargedTYS During a scheduled inspection, the emergency overhead lights at both exit rows was found not working. Maintenance removed and replaced the #3 Emergency light battery, I.A.W.-EMB-135-MM-33-50-04, operational checks good. Aircraft released to service.Jan 1, 2002 · N27506 · Emb EMB135ER · Emergency LightingSDR C2XA02TY001Light · inoperativeTYS DURING A SCHEDULED INSPECTION, THE NR 4 (AT SEAT 8 ) EMERGENCY LIGHT STRIP WAS FOUND NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE NR 4 LIGHT STRIP IAW EMB-135-MM-33-50-12, OPERATIONAL CHECKS GOOD. AIRCRAFT RELEASED TO SERVICE.Jan 1, 2002 · N27506 · Emb EMB135ER · Emergency LightingSDR C2XA01TY225Battery · dischargedTYS During a scheduled inspection, the emergency overhead lights at both exit rows was found not working. Maintenance removed and replaced the #3 Emergency light battery, I.A.W.-EMB-135-MM-33-50-04, operational checks good. Aircraft released to service.Jan 1, 2002 · N27506 · Emb EMB135ER · Emergency LightingSDR C2XA01TY224Light · inoperativeTYS DURING A SCHEDULED INSPECTION, THE NR 4 (SEAT 8) EMERGENCY LIGHT STRIP WAS FOUND NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE NR 4 LIGHT STRIP, IAW EMB-135-MM-33-50-12. OPERATIONAL CHECKS GOOD. AIRCRAFT RELEASED TO SERVICE.Jan 1, 2002 · N27506 · Emb EMB135ER · Emergency LightingSDR C2XA01CL252Odor · detectedCLE FLIGHT 3160 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT WHEN THE APU WAS STARTED IN FLIGHT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF APU AND APU BLEED SYSTEM AND FOUND NO DEFECTS. THE AIRCRAFT WAS RELEASED FOR SERVICE.Dec 22, 2001 · N27506 · Emb EMB135ER · Air Distribution SystemSDR C2XA01CL248Odor · detectedCLE FLIGHT 3184 THE CREW REPORTED A STRONG FUEL SMELL WHEN THE APU WAS STARTED IN FLIGHT. THE APU WAS SHUT DOWN IMMEDIATELY. MAINTENANCE INSPECTED AND PERFORMED A OPERATIONAL CHECK OF THE APU AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.Dec 16, 2001 · N19503 · Emb EMB135ER · Air Distribution SystemSDR C2XA01TY202Bypass Jacket · corrodedTYS DURING A SCHEDULE INSPECTION, BETWEEN THE FAN CASE AND THE OUTER BYPASS, OXIDATION WAS FOUND ON NR 1 AND NR 2 ENGINE. MAINTENANCE REMOVED THE OXIDATION, PERFORMED TOUCHUP OF PERMANENT RESIN COATING ON ACCESS, GEAR BOX MOUNTS, PLACED A CHEMICAL-FILM COATIDec 15, 2001 · N27512 · Emb EMB135ER · Turbine Engine Bypass SectionSDR C2XA01TY204Skin · dentedTYS DURING A SCHEDULE INSPECTION THE FUSELAGE WAS DAMAGED BEHIND FRAME 31 BETWEEN STRINGER 12 AND 13R. REMOVED DAMAGED AREA. FABRICATED A DOUBLER, ALODINED AND INSTALLED, SEALED, PRIMED AND PAINTED IAW EMB 135 SRM 51-40-02 AND 51-22-01 AND CPM 51-21-05. ALLDec 15, 2001 · N27512 · Emb EMB135ER · Fuselage Main, Plate/SkinSDR C2XA01TY203Bypass Jacket · corrodedTYS DURING A SCHEDULE INSPECTION, BETWEEN THE FAN CASE AND THE OUTER BYPASS, OXIDATION WAS FOUND ON NR 1 ENGINE. MAINTENANCE REMOVED THE OXIDATION, PERFORMED TOUCH UP OF PERMANENT RESIN COATING ON ACCESS, GEAR BOX MOUNTS, PLACED A CHEMICAL-FILM COATING FOR MDec 15, 2001 · N27512 · Emb EMB135ER · Turbine Engine Bypass SectionSDR C2XA01CL244Charger · inoperativeDURING ROUTINE MAINTENANCE THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE AT BOTH OVERWING EXITS IN THE CABIN. MAINTENANCE REPLACED THE NR 3 BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.Dec 14, 2001 · N27506 · Emb EMB135ER · Emergency LightingSDR C2XA01TY201Attach Fitting · damagedTYS DURING A SCHEDULED INSPECTION THE LEFT HAND COCKPIT PARTITION WALL ATTACHMENT POINTS WERE FOUND TO BE DAMAGED. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR AND PERFORMED A DYE PENETRANT INSPECTION IAW EMBRAER GST 3877/01, EMB-135 CPM 51-21-04, 51-21-05 ADec 14, 2001 · N27512 · Emb EMB135ER · Passenger Compartment EquipmentSDR C2XA01TY200Floor Support · corrodedTYS DURING A SCHEDULED INSPECTION THE FLOOR SUPPORT ANGLES LOCATED BELOW THE THRESHOLD STRIP AT THE MAIN ENTRY DOOR WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE ACCOMPLISHED A BLEND-OUT REPAIR IAW EMB-135 SRM 51-20-03, 51-40-02 AND CPM 51-21-04,Dec 14, 2001 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA01TY199Inlet · damagedTYS DURING A SCHEDULED INSPECTION THE RIGHT HAND ENGINE AIR INLET WAS FOUND TO HAVE TWO NICKS ON THE ACOUSTIC PERFORATED INNER SKIN. MAINTENANCE REWORKED THE NICKS (BLEND-OUT) IAW EMB-135 SRM 54-20-01 AND EMBRAER GST 3879/01, THE REPAIR WAS FOUND TO BE SATIDec 14, 2001 · N27512 · Emb EMB135ER · Turbine Engine Air Inlet SectionSDR C2XA01TY198Limiter · gougedTYS DURING A SCHEDULED INSPECTION THE LEFT HAND ELEVATOR INBOARD LIMITER TUBE WAS FOUND TO BE GOUGED. MAINTENANCE ACCOMPLISHED THE BLEND-OUT REPAIR AND PERFORMED A DYE PENETRANT INSPECTION IAW EMBRAER GST-3934/01, THE REPAIR AND INSPECTION WERE SATISFACTORY.Dec 13, 2001 · N27512 · Emb EMB135ER · Elevator Control SystemSDR C2XA01TY197Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE LOCATED BELOW THE FLOORING AND JUST AFT OF THE COCKPIT ENTRANCE WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE FORWARD DIGITAL IAW EMB-135 SRM 51-40-02, THE REPADec 13, 2001 · N27512 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA01TY196Gusset · corrodedTYS DURING A SCHEDULED INSPECTION THE SUBFLOOR GUSSET LOCATED JUST AFT OF THE COCKPIT ENTRANCE WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE GUSSET IAW EMB-135 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILLDec 13, 2001 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA01TY195Floor Support · corrodedTYS DURING A SCHEDULED INSPECTION THE TOP CAP ON THE CENTER OMEGA BEAM BETWEEN FRAMES 19 AND 23 WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB-135 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WIDec 13, 2001 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA01TY194Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION THE LEFT HAND CENTER OMEGA BEAM AT FRAME 20 WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED THE CORRODED AREA AND ACCOMPLISHED A DOUBLER REPAIR IAW EMB-135 SRM 53-21-10, THE REPAIR WAS SATISFACTORY. THE AIDec 13, 2001 · N27512 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA01TY193Angle · corrodedTYS DURING A SCHEDULED INSPECTION THE RAMP ANGLE ON THE CENTER OMEGA BEAM BETWEEN FRAMES 19 AND 20 WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-135 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRDec 13, 2001 · N27512 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA01CL242Bulb · burned outDURING A 1A INSPECTION MAINTENANCE FOUND THE SERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE.MAINTENANCE REPLACED THE LIGHT BULB FOR THE SERVICE DOOR EMERGENCY LIGHT AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.Dec 12, 2001 · N25504 · Emb EMB135ER · Emergency LightingSDR C2XA01TY192Line · corrodedTYS During a scheduled inspection the pottable water line was found corroded at the fuselage to tube fitting. Maintenance removed and replaced the potable water overflow line I.A.W.-EMB-135-AMM-38-10-07. Repairs where satisfactory and the aircraft will be relDec 12, 2001 · N27512 · Emb EMB135ER · Potable Water SystemSDR C2XA01TY191Actuator · failedTYS DURING A SCHEDULED INSPECTION THE HORIZONTAL STABILIZER ACTUATOR FAILED A FUNCTIONAL CHECK. THE ACTUATOR INNER PISTON HAS PLAY AND NONE WAS ALLOWED IAW CONTINENTAL EXPRESS TASK CARD 27-40-02-220-001-A00. MAINTENANCE REMOVED AND REPLACED THE ACTUATOR IAWDec 11, 2001 · N27512 · Emb EMB135ER · Stabilizer ActuatorSDR C2XA01CL235O-Ring · damagedCLE FLIGHT 3237 THE CREW REPORTED NR 2 ENGINE OIL LEVEL AND PRESSURE WAS DROPPING. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE SHAFT O-RING ON THE NR 4 GENERATOR. OPERATIONAL CHECKS Nov 29, 2001 · N17507 · Emb EMB135ER · Turbine Engine Oil SystemSDR C2XA01CL233Actuator · leakingCLE FLIGHT#3128 THE CREW REPORTED INFLIGHT WITH GEAR UP INDICATION.THERE WAS A LOUD NOISE AND VIBRATION COMING FROM THE NOSE AREA.THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE RIGHT HAND NOSE LANDING GEAR DOOR ACNov 27, 2001 · N27512 · Emb EMB135ER · Landing Gear ActuatorSDR C2XA01CL232Smoke Warning · malfunctionedCLE FLIGHT 3207 THE CREW REPORTED AFTER TAKEOFF RECEIVED A LAV SMOKE WARNING. THE AIRCRAFT RETURNED TO MDT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE LAV SMOKE SYSTEM. NO DEFECTS WERE FOUND. THE AIRCRNov 25, 2001 · N14508 · Emb EMB135ER · Smoke DetectionSDR C2XA01CL231Pin · brokenCLE FLIGHT#3062 THE CREW REPORTED THE MAIN CABIN DOOR CATCHES WHEN BEING OPENED AND THE INTERIOR HANDLE APPEARED TO BE BROKEN.MAINTENANCE INSPECTED AND FOUND THE ROLL PIN FOR THE INTERIOR LOCKING HANDLE TO BE BROKEN. THEY REPLACED THE PIN AND FUNCTIONALY CHECKNov 24, 2001 · N27506 · Emb EMB135ER · Passenger/Crew DoorsSDR C2XA01TY186Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE LOCATED JUST AFT OF THE COCKPIT ENTRANCE DOOR WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FORWARD DIGITAL PLATE IAW EMB 135 SRM 51-40-02 AND EC 35320-01059, THE REPAIR WAS FOUND TNov 23, 2001 · N16511 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA01TY185Stringer · chafedTYS DURING A SCHEDULED INSPECTION THE EXTERNAL STRINGER 19L WAS FOUND CHAFED JUST AFT OF HYDRAULIC PUMP. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR OF STRINGER 19L IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION 5310-01207, THE REPAIR WAS SANov 23, 2001 · N16511 · Emb EMB135ER · Fuselage Main, Longeron/StringerSDR C2XA01TY184Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION THE CENTER FLOORBEAM TOP CAP WAS FOUND CORRODED BETWEEN FRAMES 19 AND 22. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB135 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INNov 23, 2001 · N16511 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA01TY183Fire Loop · chafedTYS DURING A SCHEDULE INSPECTION THE LEFT HAND ENGINE FIRE DETECTION LOOP WAS FOUND TO BE CHAFED BEYOND MANUFACTURES LIMITS. MAINTENANCE REMOVED AND REPLACED THE FIRE DETECTION LOOP IAW EMB135 MM 26-11-01, OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT Nov 23, 2001 · N16511 · Emb EMB135ER · Fire DetectionSDR C2XA01CL230Blanket · looseCLE-CVG FLIGHT#3093 THE CREW REPORTED ON 20 MILE FINALE APPROACH INTO CVG THE COCKPIT FILLED WITH ELECTRIC SMOKE AND WENT AWAY AFTER TOUCHDOWN.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE INSULATION BLANKET PULLED AWAY FROM Nov 21, 2001 · N27506 · Emb EMB135ER · Air Distribution SystemSDR C2XA01TY182Connector · brokenTYS DURING A SCHEDULED 1-C INSPECTION, PANEL 251 HF EMERGENCY LIGHT STRIP, WAS INOPERATIVE, DUE TO A BROKEN CONNECTOR. MAINTENANCE INSTALLED A NEW CONNECTOR ON PANEL 251 HF IAW EMB 135/145 AMM AND PERFORM A OPS CHECK, EVERYTHING WAS ACCOMPLISH AND WILL BE RELNov 19, 2001 · N16511 · Emb EMB135ER · Emergency LightingSDR C2XA01TY181Floor Support · corrodedTYS DURING A SCHEDULED 1-C INSPECTION THE LEFT FLOOR SUPPORT PLATE FWD OF SERVICE DOOR WAS FOUND CORRODED AROUND SCREW HOLES. MAINTENANCE REMOVED AND REPLACED THE NUT PLATE, CLEAN THE CORROSION, REFINISH THE AREA IAW EMB 135/145 SRM 51-40-02, CPM 51-21-17-00Nov 18, 2001 · N16511 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA01TY180Sill · corrodedTYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND UNDER THE SERVICE DOOR SILL AND SCREW HOLES. MAINTENANCE REMOVED AND REPLACED ONE NUT PLATE, CLEAN THE CORROSION, REFINISH THE AREA IAW EMB 135/145 SRM 51-40-02 AND CPM 51-17-04--51-21-07, ALL WORK WASNov 18, 2001 · N16511 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA01TY179Floorbeam · corrodedTYS DURING A SCHEDULED 1C INSPECTION THE FLOORBEAM SPLICE CAP OVER FRAME 20 ON RIGHT SIDE WAS FOUND CORRODED AROUND THE RIVETS. MAINTENANCE REMOVED AND REPLACED THE RIVETS, CLEAN THE CORROSION, REWORKED THE AREA IAW EMB 135/145 SRM 51-40-02 AND CPM 51-17-00-Nov 18, 2001 · N16511 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA01CL228Actuator · failedMSN FLIGHT#3110 THE CREW REPORTED THE HORIZONTAL STABILIZER PITCH TRIM FAILED AFTER TAKEOFF.THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE HORIZONTAL STABILIZER PITCH TRIM ACTUATOR AND THE HORIZONTAL STABILIZER CONTNov 12, 2001 · N16502 · Emb EMB135ER · Stabilizer ActuatorSDR C2XA01TY178Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE FORWARD DIGITAL BETWEEN FRAMES 15 AND 16 AT CENTER AND LEFT SIDE. MAINTENANCE REMOVED THE DAMAGED SECTION, FABRICATED NEW ANGLE, SHIM, FILLER AND PLATE. INSTALLED REPAIRED PARTS IAW-EMB-135/145-Nov 11, 2001 · N15509 · Emb EMB135ER · Fuselage Main, Floor Beam
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