Embraer EMB-135KL

Service difficulty reports · 5,598

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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 = 'EMB135KL'
  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 SIMA200327905Skin · gougedABI - DURING AN MBV INSPECTION, TWO GOUGES WERE FOUND IN FUSELAGE SKIN BETWEEN FRAMES 19 AND 20 AND STRINGERS 1L AND 2L, CENTER FUSELAGE 1. BLENDED THE GOUGED AREAS AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER FOct 1, 2003 · N823AE · Emb EMB135KL · Fuselage Main, Plate/SkinSDR SIMA200327903Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 20. REMOVED CORROSION BY CREATING A CUTOUT IN THE FLANGED AND WEB AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM Sep 30, 2003 · N823AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200327904Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 24 AND 25. REMOVED CORROSION CREATING A CUTOUT IN THE FLANGED AND WEB AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMBSep 30, 2003 · N823AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200327907Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 24 AND 25. REMOVED CORROSION BY CREATING A CUTOUT IN THE FLANGED AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRMSep 30, 2003 · N823AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200327902Stringer · chafedABI - DURING AN MBV INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS BETWEEN FRAMES 52 AND 53. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS FOR REPAIR. REPAIR DONESep 27, 2003 · N823AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200327906Stringer · chafedABI - DURING AN MBV INSPECTION, FOUND STRINGER 19L WAS FOUND CHAFED BELOW SRM LIMITS BETWEEN FRAMES 52 AND 53. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS FOR REPAIR. REPAIR DONESep 27, 2003 · N823AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200326802Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE CENTER FLOORBEAM BETWEEN FRAMES 24 AND 25 AS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGE SECTION OF THE CETNER FLOORBEAM, CLEANED, AND TREATED THE REPAIR AREA. FABRICATED A EXTERNAL ANGLE, FILLER AND TWO SHIMS. Sep 20, 2003 · N821AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200326807Stringer · chafedABI - DURING AN MBV INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 22, CHAPTERS 53-24-02 AND Sep 20, 2003 · N821AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200326805Stringer · chafedABI - DURING A MBV INSPECTION, FOUND STRINGER 19L WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142, REV 22, CHAPTER 53-24-02 AND EMB IC2003-Sep 20, 2003 · N821AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200326804Floorbeam · corrodedABI - DURING A MBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMTIS. CUT OUT DAMAGE SECTION OF BEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMSep 20, 2003 · N821AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200325902Smoke Detector · malfunctionedIND - FLT 4296 - IN FLIGHT DURING CLIMB PASSING 600 FT BAGGAGE SMOKE LIGHT ILLUMINATED. CREW DISCHARGED BOTTLES, DECLARED EMERGENCY LANDED WITHOUT INCIDENT. INSPECTED BAGGAGE SMOKE DETECTION SYSTEM WITH NO DEFECTS NOTED. RAI FIRE BOTTLES AND A/C RETURNED TOSep 15, 2003 · N801AE · Emb EMB135KL · Smoke DetectionSDR SIMA200326503Stringer · chafedABI - DURING A MBV INSPECTION, FOUND STRINGER 19L WAS FOUND TO BE CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-24-02 Sep 9, 2003 · N820AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200325309Lockpin · lack of lubeDURING TAKEOFF, CRWE REPORTED THE CAPTAINS SEAT PINS FAILED TO ENGAGE AND PILOTS SEAT SLIDE TO THE AFT POSITION. MAINTENANCE CLEANED THE CAPTAINS SEAT TRACKS AND LUBRICATED THE SEAT PINS. OPS CHECK WAS GOOD IAW CMM 25-21. (M)Sep 8, 2003 · N830AE · Emb EMB135KL · Flight Compartment EquipmentSDR SIMA200325103Light · inoperativeCREW REPORTED THE LAST THREE FLOOR PROXIMITY EMERGENCY LIGHT STRIPS TO BE INOPERATIVE. (M)Sep 8, 2003 · N853AE · Emb EMB135KL · Emergency LightingSDR SIMA200325102Acm · seizedSYR - FLT 4320 - DURING CRUISE FLIGHT, THE FLIGHT ATTENDANT REPORTED LOUD NOISE UNDER THE FLOORBOARD FOLLOWED BY A BURNING SMELL AND SMOKE. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT AIR CYCLE MACHINE. OPERATIOSep 7, 2003 · N838AE · Emb EMB135KL · Cabin Cooling SystemSDR SIMA200325301Stringer · chafedABI - DURING AN MBV INSPECTION, FOUND STRINGER 19L WAS FOUND CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-21-02 FIG 201. (M)Sep 1, 2003 · N817AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200324401Inverter · inoperativeCREW REPORTED AN OVERHEAD EMERGENCY LIGHT IN THE CABIN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 INVERTER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 27, 2003 · N823AE · Emb EMB135KL · Emergency LightingSDR SIMA200323903Smoke Detector · inoperativeFLT 3595 - CRP - CREW REPORTED DURING CRUISE FILGHT THE CARGO FIRE DETECTION LIGHT CAME ON CREW FOLLOWED AOM PROCEDURES AND FIRED THE CARGO FIRE BOTTLES. LIGHT EXTINGUISHED AFTER 60 SECONDS. AFTER AN INSPECTION SYSTEM WAS PUT ON MEL. S/D - MAINTENANCE REMOVEAug 26, 2003 · N843AE · Emb EMB135KL · Smoke DetectionSDR SIMA200324610Stringer · chafedABI - DURING AN MBV INSPECTION, STRINGER 19L WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED AN NDT INSPECTION. FABRICATED TWO REPAIR DOUBLERS, FOUR SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2777. (M)Aug 21, 2003 · N818AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200324609Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGE SECTION OF OMEGA BEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS AND PLATE. REPAIR DONE IAW Aug 19, 2003 · N818AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200323003Light · inoperativeFLIGHT ATTENDANT REPORTED THE EXIT SIGN ABOVE THE SERVICE DOOR TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTION ON LUMINSCENT STRIP TO BE SHEARED OFF. MAINTENANCE REPLACED TEH LIGHT STRIP. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 17, 2003 · N834AE · Emb EMB135KL · Emergency LightingSDR SIMA200323002Fcu · inoperativeDURING APPROACH, TEH CREW REPORTED THE FLAPS BECAME STUCK IN THE DOWN POSITION. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED IN CMH WITH NO FURTHER PROBLEMS NOTED. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB MM. OPERATIONAAug 15, 2003 · N839AE · Emb EMB135KL · Trailing Edge Flap Control SystemSDR SIMA200322506Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED BELOW SRM LIMITS. BLENDED THE DAMAGE AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR DOUBLER, FILLER, SHIMS AND REPAIR PLATE. REPAIR DONE IAW EMB REPAIR SAug 10, 2003 · N819AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200322505Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. PERFORMED A CUTOUT OF THE CORRODED SECTION OF THE OMEGA BEAM. FABRICATED A REPAIR DOUBLER, FILLER TWO SHIMS AND A REPAIR PLATE. REPAIR DONE IAW EMB 14Aug 9, 2003 · N819AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200322502Stringer · chafedABI - DURING AN MBN INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED ARE AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE, SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-24-02. (M)Aug 9, 2003 · N819AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200322507Stringer · chafedABI - DURING AN MBV INSPECTION, STRINGER 19L WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 22, CHAPTERS 53-24-02. (M)Aug 9, 2003 · N819AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200322302Odor · detectedDURING CLIMB CREW REPORTED A BURNING ELECTRICAL ODOR. NO SMOKE WAS REPORTED. AN EMERGENCY WAS DECLARED AND FLIGHT LANDED WITH NO FURTHER INCIDENTS. THE ODOR DISSIPATED DURING DESCENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AN INSPECTION OF THE ELECTAug 8, 2003 · N807AE · Emb EMB135KL · Air Distribution SystemSDR SIMA200322504Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED BELOW SRM LIMITS. CUT OUT SECTION OF DAMAGED OMEGA BEAM. FABRICATED A REPAIR ANGLE, FILLER, SHIMS, REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTERAug 7, 2003 · N819AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200321803Windshield · crackedRIC - FLT 4128 - DURING CLIMB AT ABOUT 10,000 FEET, CREW NOTED FIRST OFFICER WINDSHIELD ARCING SHORTLY AFTER HEAT WAS SELECTED OFF THE WINDSHIELD STARTED TO SHATTER. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITH NO FURTHER PROBLEMS REPORTED. MAINTENANCEAug 4, 2003 · N821AE · Emb EMB135KL · Flight Compartment WindowsSDR SIMA200321604Battery · dischargedCREW REPORTED THE LAST THREE FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE CHARGED THE BATTERY AND AN OPERATIONAL CHECK WAS COMPLIED WITH. AICRAFT WAS RETURNED TO SERVICE. (M)Jul 31, 2003 · N847AE · Emb EMB135KL · Emergency LightingSDR SIMA200321808Stringer · chafedABI - DURING AN MBV INSPECTION, STRINGER 19R WAS FOUND AT FRAME 53. BLENDED THE CHAFE AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/2577 AND EMB SRM, SRM EMB 145/1142 REV 22, CHAPTJul 31, 2003 · N816AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200321804Stringer · chafedABI - DURING AN MBV INSPECTION, STRINGER 19L WAS FOUND CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB145/1142 REV 22, CHAPTER 53-24-02 FIG 201. (M)Jul 31, 2003 · N816AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200321809Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGE SECTION OF LEFT OMEGA BEAM. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142, REV 22, CHAPTER 5Jul 30, 2003 · N816AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200321807Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED NUT PLATE FROM ATTACHED AREA. COMPLETELY REMOVED CORROSION BY BLENDING. PERFORMED EDDY CURRENT INSPECTION OF BLENDED AREA WITH NO DEFECTS NOTEJul 19, 2003 · N815AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200319708Stringer · chafedABI - DURING AN MBV INSPECTION, FOUND STRINGER 19L WAS CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED TWO REPAIR ANGLES AND SHIMS. REPAIR DONE IAW EMB STATEMENT IC2003-145/2225-A AND SRM, SRM EMB 145/1142 REV 21, CHAPTEJul 10, 2003 · N814AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200319709Stringer · chafedABI - DURING AN MBV INSPECTION, STRINGER 19R WAS FOUND CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE SHIMS. REPAIR DONE IAW EMB SRM EMB 145/1142 REV 21, CHAPTER 53-241-02 FIGURE 201. (M)Jul 10, 2003 · N814AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200319705Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGED SECTIN OF OMEGA BEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AND EXTERNAL ANGLE, ANGLE, FILLER, AND TWO SHIMS. REPAIR DONE IAJul 10, 2003 · N814AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200319706Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT DAMAGED SECTION OF LEFT OMEGA BEAM CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMBJul 10, 2003 · N814AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200319003Sensor · inoperativeDURING DESCENT CREW REPORTED THE FLAPS FAILED TO DEPLOY. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE LEFT FLAP VELOCITY SENSOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETUJul 7, 2003 · N804AE · Emb EMB135KL · Trailing Flap Position Indicating SystemSDR SIMA200318102Battery Pack · inoperativeCREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT BETWEEN SEAT 7A AND 11A WILL NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY PACK IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 28, 2003 · N831AE · Emb EMB135KL · Emergency LightingSDR SIMA200317603Stringer · chafedABI - DURING AN MBV INSPECTION, FOUND STRINGER 19R CHAFED AT FRAME 53. BLENDED THE CAHFED AREA AND PERFORMED NDT INSPECTION NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS AND INSTALLED. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 21, CHAPTER 53-24-Jun 23, 2003 · N811AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200317605Stringer · chafedABI - DURING AN MBV INSPECTION, FOUND STRINGER 19L WAS FOND CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND SHIMS AND INSTALLED. REPAIR DONE IAW EMB SRM, SRM EMB 145-1142 REV 21, CHAPTER 53-24-02 FIGURJun 23, 2003 · N811AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200317606Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT DAMAGE SECTION ON LEFT OMEGA BEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER, PLATE AND SHIMS AND INSTALLED. REJun 23, 2003 · N811AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200317607Rivet · lightning strikeABI - DURING A LIGHTNING STRIKE INSPECTION ONE RIVET AT STRINGER 6R, 2 INCHES FORWARD OF FRAME 34 WAS FOUND DAMAGED. REMOVED DAMAGED RIVET AND PERFORMED A CIRCULAR CUTOUT .6 INCHES IN DIAMETER. FABRICATED A REPAIR PLUG, REPAIR DOUBLER. REPAIR DONE IAW BME IJun 20, 2003 · N811AE · Emb EMB135KL · FastenersSDR SIMA200316904Control Unit · inoperativeDURING DESCENT, CREW NOTED FLAP FAIL INDICATION WITH SPS ADVANCE CREW FOLLOWED AOM AND DECLARED AN EMERGENCY. DURING THE DESCENT INTO ORD THE FLAPS WERE STUCK AT ZERO. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACJun 17, 2003 · N840AE · Emb EMB135KL · Trailing Edge Flap Control SystemSDR SIMA200316402Relay · inoperativeCREW RECEIVED A PITOT THREE INOPERATIVE ON EICAS. MESSAGE FLICKERING THEN EXTINGUISHED. AFTER MESSAGE EXTINGUISHED FA REPORTED SMOKE IN GALLEY AND CREW NOTED ODOR IN COCKPIT. CREW DECLARED EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMJun 12, 2003 · N803AE · Emb EMB135KL · Pitot/Static SystemSDR SIMA200316002Smoke Detector · inoperativeDURING CLIMB, CREW REPORTED A FIRE WARNING FOR THE AFT BAGGAGE COMPARTMENT. AN EMERGENCY WAS DECLARED AND QRH PROCEDURES WERE FOLLOWED. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CARGO SMOKE DETECTOR IAW EMB MM. OPERJun 8, 2003 · N806AE · Emb EMB135KL · Smoke DetectionSDR SIMA200315302Connector · disconnectedCREW REPORTED GALLEY EMERGENCY LIGHTS AND RIGHT BULKHEAD EMERGENCY LIGHT WERE INOPERATIVE. FOUND CONNECTOR BY SERVICE DOOR OVERHEAD CEILING PANEL DISCONNECTED AT P8530. RECONNECTED CONNECTOR, OPS CHECK GOOD. (M)Jun 1, 2003 · N810AE · Emb EMB135KL · Emergency LightingSDR SIMA200315501Damper · brokenDURING PHASE 4 INSPECTION, THE RT AILERON DAMPER CONTROL ROD WAS FOUND TO BE BROKEN CAUSING DAMAGE MOUNTING BRACKET ON THE AILERON. RAI RT AILERON DAMPER IAW AMM 27-12 & RAI RT AILERON IAW AMM 27-12. FCF PERFORMED AND FOUND TO BE SATISFACTORY. AIRCRAFT RETURJun 1, 2003 · N837AE · Emb EMB135KL · Elevator Control SystemSDR SIMA200316006Stringer · chafedDURING AN MBV INSPECTION, FOUND STRINGER 19L CHAFED AT FRAME 53. BLENDED THE CHAFED AREA AND PERFORMED AN NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB 145/1142 REV 21, CHAPTER 53-24-01 FIGURE 20May 29, 2003 · N809AE · Emb EMB135KL · Fuselage Main, Longeron/Stringer
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