Embraer EMB-135KL

Service difficulty reports · 5,598

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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 = '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 SIMA200507001Bolt · brokenDURING PHASE 2A INSPECTION, FOUND RIGHT AILERON DAMPER ROD END BOLT BROKEN. REMOVED AND REPLACED BOLT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Mar 10, 2005 · N803AE · Emb EMB135KL · FastenersSDR SIMA200506609Battery Pack · dischargedALB - FLT 4155 - CREW REPORTED THE FIRST THREE STRIPS OF FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FOUR BATTERY PACKS IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Mar 7, 2005 · N816AE · Emb EMB135KL · Emergency LightingSDR SIMA200507503Floor Support · corrodedABI - DURING INSPECTION AIRCRAFT, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVED THE CORROSION. FABRICATED A EXTERNAL DOUBLER, FILLER, SHIMS AND PLATE. REPAIR DONE IAW EMB 145 SRM, SRM EMB145/1142 REV 28, CHAPTER 53-21-10Mar 3, 2005 · N801AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA200500047Light · inoperativeEMERGENCY EGRESS FLOOR PROXIMITY LIGHT STRIP NR 7 IN INOPERATIVE. REMOVED AND REPLACED EMERGENCY EGRESS FLOOR LIGHT IAW EMB 140 MM 33-50-00-5.Mar 3, 2005 · N372SK · Emb EMB135KL · Emergency LightingSDR SIMA200506606Floor Support · corrodedABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FRAMES 23 AND 25 WERE FOUND CORRODED. BLENDED THE CORRODED AREAS TO REMOVED THE CORROSION AND PERFORMED NDT INSPECTION AND FABRICATED AN EXTERNAL DOUBLER FOR REPAIR. REPAIR DONE IAW EMB REPAIR DONE IAMar 2, 2005 · N801AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200506605Floor Support · corrodedDURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUTOUT TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28 CHAPTERS 53-21-10 FIG 201. (Mar 2, 2005 · N801AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200506604Floor Support · corrodedABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIRS DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28, CHAPTER 53-22-10 FIG 2Mar 1, 2005 · N801AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200506602Sill · corrodedSAW - DURING CPCP INSPECTION, MAINTENANCE FOUND THE AFT SERVICE DOOR SILL CORRODED BETWEEN FRAMES 22-23. INSTALLED NEW SILL IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 26, 2005 · N804AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200506603Gusset · corrodedSAW - DURING CPCP INSPECTION MAINTENANCE, FOUND THE GUSSET OVER LEFT OUTBOARD FLOORBEAM BETWEEN FRAMES 16-17 HAS CORROSION. INSTALLED NEW GUSSET IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 26, 2005 · N804AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200506106Stringer · gougedABI - DUIRNG A IMBV INSPECTION OF AIRCRAFT, STRINGER 19R WAS FOUND TO BE GOUGED BETWEEN FRAMES 49 AND 50. BLENDED OUT THE GOUGE, PERFORMED EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SFeb 25, 2005 · N801AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200506107Stringer · gougedABI - DURING INSPECTION OF AIRCRAFT, STRINGER 19L AS FOUND TO BE GOUGED BETWEEN FRAMES 49 AND 50. BLENDED OUT THE GOUGE. PERFORMED EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRMFeb 25, 2005 · N801AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA200506108Beam · corrodedABI - DURING AN IMBV INSPECTION, THE GALLEY AREA CENTER BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER BEAM. INSTALLED NEW BEAM IAW EMB SRM, SRM 145/1142 REV 28 CHAPTER 51-40-02. (M)Feb 25, 2005 · N801AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA200500035Light · disconnectedMAIN CABIN DOOR EMERGENCY EGRESS LIGHT IS INOP. FOUND GROUND WIRE MISSING FOR LIGHT ASSEMBLY. CLEANED BONDING SURFACE FOR GROUND AND REINSTALLED TERMINAL. OPS CHECK GOOD IAW EMB 140 MM 33-50-0.Feb 17, 2005 · N378SK · Emb EMB135KL · Emergency LightingSDR CHQA200500033Lamp · burned outLEFT OVERWING EMERGENCY EGRESS LIGHT IS INOP. RELAMPED IAW EMB 140 MM 33-50-07.Feb 16, 2005 · N377SK · Emb EMB135KL · Emergency LightingSDR CHQA200500034Light · inoperativeRIGHT OVERWING EMERGENCY EGRESS LIGHT IS INOP. RELAMPED RIGHT OVERWING EMERGENCY EGRESS LIGHT IAW EMB 140 MM 33-50-07.Feb 16, 2005 · N378SK · Emb EMB135KL · Emergency LightingSDR SIMA200506101Doubler · corrodedSAW - DURING CPCP INSPECTION, FOUND FORWARD DOUBLER CORRODED TOP AND BOTTOM SURFACES. REMOVED AND REPLACED FORWARD DOUBLER AS PER SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)Feb 11, 2005 · N805AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200506102Sill · corrodedSAW - DURING CPCP INSPECTION, FOUND AFT RIGHT SILL CORRODED IN NUMEROUS AREAS. REMOVED AND REPLACED RIGHT AFT SILL AS PER SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 11, 2005 · N805AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200506103Sill · corrodedSAW - DURING CPCP INSPECTION, FOUND RIGHT FORWARD SERVICE DOOR SILL CORRODED IN NUMEROUS AREAS. REMOVED AND REPLACED SILL ASSEMBLY AS PER SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 11, 2005 · N805AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200506104Sill · corrodedSAW - FOUND DURING CPCP INSPECTION, FOUND CORROSION ON SERVICE DOOR SILL IN FORWARD CABIN GALLEY. REMOVED AND REPLACED SERVICE DOOR SILL IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 8, 2005 · N805AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200506105Floor Support · corrodedSAW - DURING CPCP INSPECTION, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20, FORWARD CABIN. COMPLIED WITH LEFT OMEGA SHAPED BEAM REPAIR IAW SRM 53-21-10. AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 8, 2005 · N805AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200503802Floor Support · corrodedABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE BEAM TO REMOVED CORROSION. FABRICATED A REPAIR DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28, CHAPTER 53-21-1Feb 3, 2005 · N843AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200502803Light · malfunctionedEMERGENCY FLOOR LIGHTING AT ROWS 7 THRU 11 DIM AFTER 30 SECONDS. PERFORMED OPERATIONAL CHECK OF EMERGENCY FLOOR LIGHTS WITH NO DISCREPANCIES NOTED. RETURNED TO SERVICE. (SW21200503032) (K)Jan 27, 2005 · N834AE · Emb EMB135KL · Emergency LightingSDR CHQA200500020Light · inoperativeEMERGENCY FLOOR EGRESS LIGHTING AT SEAT 1 AND 2A IS INOPERATIVE. REPLACED FLOOR PROXIMITY STRIP LIGHT. OPS CHECK GOOD IAW EMB 140 AMM 33-50-00.Jan 27, 2005 · N378SK · Emb EMB135KL · Emergency LightingSDR SIMA200502802Connector · disconnectedEMERGENCY EXIT SIGN ABOVE SEAT, 3B INOPERATIVE. RECONNECTED THE CONNECTOR PLUG AT ROW 3B EMERGENCY EXIT SIGN. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200503030) (K)Jan 26, 2005 · N819AE · Emb EMB135KL · Emergency LightingSDR SIMA200502401Windshield · crackedON CLIMB OUT AT 11,000 FL CAPTAINS WINDSCREEN SHATTERED RETURNED TO AIRPORT, LANDED SAFELY. NO LOSS OF CABIN PRESSURIZATION. REPLACED CAPTAIN WINDSHIELD. AC RETURNED TO SERVICE. (SW21200503048) (K)Jan 21, 2005 · N842AE · Emb EMB135KL · Flight Compartment WindowsSDR CHQA200500005Squat Switch · contaminatedFLIGHT 5880 ATL TO STL - AFTER GEAR RETRACTION AN LG AIR/GRD FAIL MESSAGE APPEARED ON EICAS. GEAR RETRACTED NORMALLY AND INDICATED UP. THE AIRCRAFT WAS DIVERTED TO IND AND AN EMERGENCY WAS DECLARED. THE BRAKE SYSTEM DEGRADED AFTER LANDING BUT THE AIRCRAFT LJan 12, 2005 · N373SK · Emb EMB135KL · Landing Gear Position and WarningSDR SIMA200501205Floor Support · corrodedDURING AN INSPECTION, THE LT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA TO REMOVE CORROSION. FABRICATED A FILLER, DOUBLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200502476) (K)Jan 6, 2005 · N846AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200501204Floor Support · corrodedDURING AN INSPECTION OF AIRCRAFT THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200502476) (K)Jan 6, 2005 · N846AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200501201Floor Support · corrodedDURING AN MBV INSPECTION THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW SRM. (SW21200502476) (K)Jan 6, 2005 · N846AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200500910Engine · failedNR 2 ENGINE FAILED DURING TAKEOFF ACCOMPANIED BY A NOISE THAT SOUNDED LIKE A COMPRESSOR STALL. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE IAW MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502355) (K)Jan 4, 2005 · N823AE · Emb EMB135KL · Engine (Turbine/Turboprop)SDR SIMA200500907Charger · inoperativeCREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 7 THROUGH 11 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200503041) (K)Jan 1, 2005 · N817AE · Emb EMB135KL · Emergency LightingSDR SIMA200500402Charger · inoperativeEMERGENCY FLOOR LIGHTS AT ROWS 7 THROUGH 11 INOPERATIVE. REPLACED NR 3 EMERGENCY BATTERY CHARGER. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200503043) (K)Jan 1, 2005 · N817AE · Emb EMB135KL · Emergency LightingSDR CHQA000600Light · inoperativeLEFT OVERWING EMERGENCY LIGHT IS INOP. RELAMPED LEFT OVERWING EMERGENCY LIGHT. OPS CHECK GOOD PER EMB 140 MM 33-50-10.Dec 24, 2004 · N372 · Emb EMB135KL · Emergency LightingSDR SIMA200534801Battery Pack · dischargedCREW NOTED WHEN ACTIVATING EMERGENCY LIGHTS FOR TEST, LIGHTS WOULD ILLUMINATE THEN FADE OUT FAST. CA REPLACED ALL 4 EMERGENCY LIGHT BATTERIES. OPERATONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)Dec 11, 2004 · N828AE · Emb EMB135KL · Emergency LightingSDR SIMA200435202Skin · dentedDURING AN MBV INSPECTION AND REPAIR OF A DENT DEFERRED UNDER TDMI NR 84053525 BETWEEN FRAMES 21 AND 22 AND BETWEEN STRINGERS 12L AND 13L. PERFORMED A CUTOUT OF THE DAMAGED SKIN AND TREATED THE BARE METAL EDGES. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIRDec 10, 2004 · N840AE · Emb EMB135KL · Fuselage Main, Plate/SkinSDR SIMA200435201Floor Support · corrodedDURING AN MBV INSPECTION OF AIRCRAFT. THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. CUTOUT A SECTION OF THE DAMAGED OMEGA BEAM AND TREATED THE BARE METAL EDGES. FABRICATED A REPAIR ANGLE .050 IN, REPAIR PLATE .125 IN, SHIMS AND A FILLER. REPAIR DONE IADec 9, 2004 · N842AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200434501Bulb · inoperativeFA REPORTED A BURNING SMELL AT 16000 FT. DECLARED EMERGENCY AND RETURNED TO FIELD. THE FLIGHT ATTENDANT NOTICED AFTER LANDING THAT THE FORWARD OVERHEAD ENTRY LIGHT ABOVE HIS SEAT WAS BURNED OUT. CONTACTED MAINTENANCE, VERIFIED THAT THE BULBS WERE BURNED ANDDec 7, 2004 · N826AE · Emb EMB135KL · Emergency LightingSDR SIMA200434202Relay · inoperativeICE CONDITION ANTI-ICE WARNING. ENGINE 2, FIRE DETECTION FAIL EICAS MESSAGE. REPLACED AIR GROUND RELAY AT LT RELAY SUPPORT B14. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.(K)Dec 5, 2004 · N803AE · Emb EMB135KL · Fire DetectionSDR CHQA000590Light · inoperativeLEFT OVERWING EMERGENCY EXIT LIGHT IS INOP. RELAMPED LEFT OVERWING EMERGENCY EXIT LIGHT IAW EMB 140 MM 25-50-00. OPS CHECK GOOD.Dec 3, 2004 · N375 · Emb EMB135KL · Emergency LightingSDR SIMA200433603Battery Pack · dischargedDURING PRE-FLIGHT, THE EMERGENCY LIGHTS DID NOT WORK DURING TEST FROM FLIGHT ATTENDANT PANEL. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK AND POWER SUPPLY IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502113) (K)Nov 29, 2004 · N800AE · Emb EMB135KL · Emergency LightingSDR SIMA200433401Control Unit · failedCREW REPORTED MAIN AND BACKUP PITCH TRIM FAILURE. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200501201)Nov 27, 2004 · N853AE · Emb EMB135KL · Stabilizer Control SystemSDR SIMA200434205Floor Support · corrodedDURING A MBV INSPECTION THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. PERFORMED A CUTOUT OF DAMAGED AREA. FABRICATED EXTERNAL ANGLE, FILLER, SHIMS. REPAIR DONE IAW SRM. (K)Nov 26, 2004 · N839AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200434203Floor Support · corrodedDURING MBV INSPECTION THE CENTER OMEGA BEAM BETWEEN FRAMES 23 AND 25 WAS FOUND TO BE CORRODED. PERFORMED A CUTOUT OF DAMAGED AREA. FABRICATED EXTERNAL ANGLE, SHIMS AND FILLER. REPAIR DONE IAW SRM. (K)Nov 26, 2004 · N839AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200433604Control Unit · failedCREW REPORTED MAIN AND BACKUP PITCH TRIM FAILURE. MAINTENANCE COMPLIED WITH ENT AND FAULT ISOLATION MANUAL AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K)Nov 26, 2004 · N853AE · Emb EMB135KL · Elevator Control SystemSDR SIMA200432801Control Unit · failedDURING CRUISE FLIGHT THE CREW REPORTED PITCH TRIM .5 INOPERATIVE. MASTER WARNING WHEN A/P DISCONNECTED MOMENTARILLY. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVNov 20, 2004 · N816AE · Emb EMB135KL · Stabilizer Control SystemSDR CHQA000588Engine · unserviceableON ADVANCING THRUST LEVERS, CREW FELT A VIBRATION COMING FROM NR 2 ENGINE, AT THE SAME TIME A TRIPLE CHIME OF "E2 LOW N1". TAKEOFF ABORTED JUST BEFORE 80 KNOTS & TAXIED A SHORT DISTANCE TO J INTERSECTION. AFTER TAKEOFF ABORTED TRIPLE CHIME MESSAGE WENT AWAY Nov 20, 2004 · N376 · Emb EMB135KL · Engine (Turbine/Turboprop)SDR CHQA000585Battery · malfunctionedWITH BATTERY AND EMERGENCY SWITCHES SET TO THE OFF POSITION, THE OVER WING EXIT LIGHTS ARE ILLUMINATING. REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY. OPS CHECK GOOD IAW EMB 140 MM 33-50-04.Nov 20, 2004 · N382 · Emb EMB135KL · Emergency LightingSDR SIMA200432202Charger · failedEMERGENCY FLOOR LIGHTING ROWS 1-6 FAIL TO LIGHT DURING TEST. REPLACED BATTERY AND BATTERY CHARGER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Nov 15, 2004 · N800AE · Emb EMB135KL · Emergency LightingSDR SIMA200432201Battery · dischargedEMERGENCY FLOOR LIGHT ON LT SIDE (FIRST 6 ROWS) DID NOT ILLUMINATE DURING TEST. REPLACED BATTERY POWER SUPPLY 2 IAW AMM. OPERATIONAL CHECK GOOD. (SW21200502112) (K)Nov 14, 2004 · N800AE · Emb EMB135KL · Emergency LightingSDR SIMA200432101Engine · malfunctionedUNCOMMANDED SHUTDOWN ON ENGINE NR 1 ON CLIMBOUT. REPLACED NR 1 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Nov 13, 2004 · N850AE · Emb EMB135KL · Engine (Turbine/Turboprop)
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