N613AE

Service difficulty reports · 217

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N613AE' AND registry_match = 'registration'
  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 SIMA2011313003Connector · disconnectedDURING MAINTENANCE INSPECTION FOUND THE RIGHT OVERWING EXIT AFT EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND CONNECTOR ON RIGHT AFT EXTERNAL OVERWING EMERGENCY LIGHT NOT CONNECTED. CONNECTED CONNECTOR IAW EMB-145 AMM 33-Nov 8, 2011 · N613AE · Emb EMB145LR · Light System WiringSDR SIMA201131301Connector · looseDURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EXIT AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED CONNECTOR ON LIGHT ASSEMBLY. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNov 8, 2011 · N613AE · Emb EMB145LR · Light System WiringSDR SIMA2011304004Skin · crackedDURING MAINTENANCE BASE VISIT INSPECTION FOUND APROXIMATELY 2 INCH CRACK ON AFT UPPER CORNER OF THE RIGHT DV WINDOW CUTOUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-1888 PT A. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 30, 2011 · N613AE · Emb EMB145 · Fuselage Main, Plate/SkinSDR SIMA2011304003Skin · crackedDURING MAINTENANCE BASE VISIT INSPECTION FOUND APROXIMATELY 1.5 INCH CRACK ON AFT UPPER CORNER OF THE LEFT HAND DV WINDOW CUTOUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-1888 PT B. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 30, 2011 · N613AE · Emb EMB145 · Fuselage Main, Plate/SkinSDR SIMA201130802Rib · crackedDURING MAINTENANCE VISIT FOUND THE RIGHT WING 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERIVCE. COMPLIED WITH AEA EO EM-57MR-587. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 27, 2011 · N613AE · Emb EMB145LR · Wing, Rib/BulkheadSDR SIMA201130801Rib · crackedDURING MAINTENANCE VISIT FOUND THE LEFT WING 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERIVCE. COMPLIED WITH AEA EO EM-57MR-588. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 27, 2011 · N613AE · Emb EMB145LR · Wing, Rib/BulkheadSDR SIMA2011304002Rib · crackedDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE RIGHT WING 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH AEA EO EM-57MR-587. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 27, 2011 · N613AE · Emb EMB145 · Wing, Rib/BulkheadSDR SIMA2011304001Rib · crackedDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT WING 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH AEA EO EM-57MR-588. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 27, 2011 · N613AE · Emb EMB145 · Wing, Rib/BulkheadSDR SIMA201129101Skin · corrodedDURING MAINTENANCE BASE VISIT FOUND THE COCKPIT UNDERFLOOR CENTER BAYS FROM FRAME 13--15 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED COCKPIT UNDER FLOOR FRAME 13 TO FRAME 15 CORROSION IAW EO EM-53MR-1882. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 17, 2011 · N613AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR E4GR61302Rib · crackedDURING A MBV INSPECTION DISCOVERED THE LT WING RIB NR 5 TO BE CRACKED. THE CRACKS ARE VISIBLE LOOKING I/B THROUGH 532AB LOOK THROUGH THE LIGHTENING HOLES IN RIB 6. THE CRACKS EXTEND OUT FROM THE LIGHTENING HOLES IN RIB 5.Oct 17, 2011 · N613AE · Emb EMB145LR · Wing, Rib/BulkheadSDR E4GR61301Rib · crackedDURING A MBV INSPECTION DISCOVERED THE RT WING RIB NR 5 TO BE CRACKED. THE CRACKS EXTEND OUT FROM THE LIGHTENING HOLES. THE CRACKS CAN BE VISIBLE SEEN BY LOOKING THROUGH ACCESS PANELS 632AB. LOOK THROUGH THE ACCESS PANEL HOLE AND LOOK I/B THROUGH THE LIGHTEOct 17, 2011 · N613AE · Emb EMB145LR · Wing, Rib/BulkheadSDR SIMA201126210Hydraulic Line · damagedBURNING SMELL FROM BEHIND CAPT SEAT. REPAIRED HYD LINE UNDER CAPT FLOORBOARD IN COCKPIT.Sep 16, 2011 · N613AE · Emb EMB145LR · Hydraulic System, MainSDR SIMA201110201Wire · cutDURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT BELOW THE COCKPIT DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. DURING TROUBLESHOOTING, FOUND WIRE CUT. INSTALLED SPLICE IAW EMB AMM P/T 20-21-00, STEP B4. THE OPERATIONAL CHECK WAS GOOD IAWApr 11, 2011 · N613AE · Emb EMB145 · Light System WiringSDR SIMA201026307Gearbox · defectiveON FLIGHT 3940 THE CREW REPORTED DURING DESCENT INTO LEX RECEIVED AN EICAS MESSAGE FLAPS FAIL, ALSO THE FLAPS WOULD NOT MOVE. THE CAPTAIN DECLARED AN EMERGENCY. THE RUNWAY WAS NOT LONG ENOUGH TO LAND IN LEX, SO THE CREW ELECTED TO DIVERT INTO SDF. THE AIRCRSep 18, 2010 · N613AE · Emb EMB145 · Trailing Edge Flap Control SystemSDR SIMA201013202Bracket · brokenFOR FLIGHT 3995 THE CREW DISCOVERED THE TOP PRONG THAT HOLDS THE CAPTAINS SIDE FLASHLIGHT IS BROKEN OFF AND DOES NOT HOLD FLASHLIGHT SECURELY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS FLASHLIGHT ASSEMBLY IAW EMB145 AMM 33-50-1May 11, 2010 · N613AE · Emb EMB145 · Emergency LightingSDR SIMA200934101Sill · corrodedDURING MAINTENANCE INSPECTION FOUND THE SERVICE DOOR CENTER SILL TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.Dec 4, 2009 · N613AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200907001Smoke Detector · inoperativeON FLIGHT 3322, CREW REPORTED BAG SMOKE INDICATION AT 400 AGL AOM PROCEDURES FOLLOWED. AFTER LANDING CFR INSPECTED NO FIRE INDICATED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED AFT CARGO FORWARD SMOKE DETECTOR IAW WITH EMB 145 AMM 26-15-01. OPS CHMar 9, 2009 · N613AE · Emb EMB145 · Smoke DetectionSDR SIMA200906102Smoke Detector · false activationON FLIGHT 3890 CREW REPORTED AT 400 FEET ON FINAL. BAGG SMOKE MESSAGE ON EICAS AND OVERHEAD EXT BUTTON ILLUMINATED. PERFORMED EPC AOM VOL PROCEDURES NO SMOKE/FIRE NOTED BY FLIGHT ATTENDANT OR CFR. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BAGGAGEFeb 26, 2009 · N613AE · Emb EMB145 · Smoke DetectionSDR SIMA200833804Controller · malfunctionedON FLIGHT 9805 CREW REPORTED ON CLIMB-OUT STRONG ODOR OF SMOKE IN COCKPIT. CREW RETURNED TO FIELD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT WINDSHIELD CONTROLLER IAW AMM 30-42-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED Dec 2, 2008 · N613AE · Emb EMB145 · Windshield/Door Rain/Ice RemovalSDR SIMA200809301Unknown · odorON FLIGHT 4227 - DURING CRUISE, CREW REPORTED A STRONG ELECTRICAL ODOR AT FL280. THE F/A NOTED THE ODOR AS SHE APPROACHED THE COCKPIT DOOR. ODOR DISSIPATED SHORTLY BEFORE THE APPROACH TO DSM. AIRCRAFT REMOVED FROM SERVICE. PERFORMED INSPECTION OF COCKPIT AMar 31, 2008 · N613AE · Emb EMB145 · Air Distribution SystemSDR SIMA200735302Proximity Switch · malfunctionedFLT 4105 - CREW CALLED TO REPORT LANDING GEAR AIR GROUND FAIL MSG ON TAKEOFF AND GEAR WOULD NOT INITIALLY RETRACT. CREW DID GET GEAR UP. ALSO RECEIVED BLEED 2 CLOSED MESSAGE. AC LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR PROX SWITCH AND FUNCTIONAL CHECK ODec 15, 2007 · N613AE · Emb EMB145 · Landing Gear Position and WarningSDR SIMA200735102Warning Light · illuminatedCREW REPORT LANDING GEAR AIR GROUND FAIL MSG ON TAKEOFF AND GEAR WOULD NOT INITIALLY RETRACT. CREW DID GET GEAR UP. ALSO RECEIVED BLEED 2 CLOSED MESSAGE. AC LANDED WITHOUT INCIDENT.Dec 15, 2007 · N613AE · Emb EMB145 · Central WarningSDR SIMA200729912Door Frame · corrodedDURING MBV INSP, AFT LOWER SERVICE DOOR FRAME CORRODED. REPAIRED FRAME IAW EO EM-53MR-842. AIRCRAFT RETURN TO SERVICE. Oct 23, 2007 · N613AE · Emb EMB145 · Fuselage Main, StructureSDR SIMA200635213Fan Blade · out of balanceENGINE ONE VIBRATIONS. REMOVED AND REPLACED 2 BLADE SETS IAW ROLLS ROYCE MM 72-21-15. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.Dec 11, 2006 · N613AE · Emb EMB145 · Turbine Engine Combustion SectionSDR SIMA200532504Handle · crackedA CRACK WAS DISCOVERED ON THE PASSENGER DOOR INNER HANDLE BRACKET. STOP DRILLED THE CRACK ON THE PAX DOOR HANDLE BRACKET. FABRICATED A REINFORCEMENT ANGLE. REPAIR DONE IAW SRM. (K)Nov 9, 2005 · N613AE · Emb EMB145 · Passenger/Crew DoorsSDR SIMA200532502Support · damagedTHE APU COWLING RT LOWER MOUNTING SUPPORT AREA WAS FOUND DAMAGED. FABRICATED A REINFORCEMENT DOUBLER. REPAIR DONE IAW SRM. (K)Nov 8, 2005 · N613AE · Emb EMB145 · APU Cowling/ContainmentSDR SIMA200532509Floor Support · corrodedTHE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING CUTOUT. PREPARED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)Nov 7, 2005 · N613AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200532507Floor Support · corrodedTHE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)Nov 7, 2005 · N613AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200532503Sill · corrodedTHE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED LOWER SILL. INSTALLED SERVICEABLE SILL IAW SRM. (K)Nov 4, 2005 · N613AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200532508Floor Support · corrodedA PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED AHT PREVIOUS REPAIR. PREPARED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K)Nov 3, 2005 · N613AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200432703Switch · leakingCREW REPORTED AIRCRAFT HAD HYDRAULIC SYSTEM 2 FAIL IN FLIGHT. THEY FOLLOWED THE AOM AND CONTINUED AND PERFORMED AN EMERGENCY LANDING. AIRCRAFT LANDED SAFELY WITH NO OTHER INCIDENTS. FOUND NR 2 HYDRAULIC SYSTEM SWITCH LEAKING REPLACED SWITCH. FOUND NR 2 EDMNov 18, 2004 · N613AE · Emb EMB145 · Hydraulic System, MainSDR SIMA200423912Solenoid · malfunctionedDFW - FLT 3819 - CAPTAIN REPORTED NOSE GEAR DOOR FAILED TO CLOSE AFTER GEAR RETRACTION. INSTALLED NEW NOSE LANDING GEAR DOOR SOLENOID VALVE IAW EMB AMM 32-33-02. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) SIMAAug 23, 2004 · N613AE · Emb EMB145 · Landing Gear Retraction/Extension SystemSDR SIMA200311204Window Post · corrodedWHILE CHANGING THE CO-PILOTS WINDSHIELD TWO FASTENER HOLES IN THE LOWER AFT CORNER OF THE AIRFRAME OPENING WERE FOUND TO BE CORRODED. ONE OF THE FASTENER HOLES REMAINED WITHIN MANUFACTURERS LIMITS AFTER REMOVAL OF CORROSION. APPLIED ALODINE AND EPOXY PRIMER Apr 13, 2004 · N613AE · Emb EMB145 · Fuselage Main, StructureSDR SIMA200311101Acm · inoperativeORD - FLT 4246 - DURING CLIMB CREW REPORTED AN ELECTRICAL/SULPHUR ODOR IN THE COCKPIT AND THE FLIGHT ATTENDANT REPORTED A SMALL AMOUNT OF SMOKE IN THE CABIN. THE AIRCRAFT WAS RETURNED TO ORD AND THE SMOKE DISSIPATED DURING THE LANDING. MAINTENANCE REMOVED ANApr 17, 2003 · N613AE · Emb EMB145 · Cabin Cooling SystemSDR SIMA200228204Skin · puncturedDURING A PS2 INSPECTION A 1.5 INCH PUNCTURE WAS DISCOVERED BETWEEN FRAMES 65-66 AND STRINGERS 20L AND 21L. PERFORMED A CUT OUT OF THE DAMAGED AREA. PERFORMED A EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A FILLER AND REPAIR DOUBLER. Oct 6, 2002 · N613AE · Emb EMB145 · Fuselage Main, Plate/SkinSDR SIMA200212141Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING, FORWARD GIGITAL IN GALLEY HAS CORROSION. INSTALLED REPAIR DOUBLER IAW EMB GST-1140/02 AND 1169/02. (M)Apr 13, 2002 · N613AE · Emb EMB145 · Fuselage Main, Floor BeamSDR SIMA200212140Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING, RIGHT OMEGA BEAM CORRODED AT FRAME 25. BLENDED CORROSION, PERFORMED NDT INSPECTION. RESTORED SURFACE FINISH, IAW EMB GST-1140/02. (M)Apr 13, 2002 · N613AE · Emb EMB145 · Fuselage Main, Floor BeamSDR SIMA200210710Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, FOUND CORROSION IN TWO AREAS, FORWARD AND AFT, ON FORWARD DIGITAL. REMOVED CORROSION BY BLENDING AREAS. FABRICATED TWO REPAIR DOUBLERS. REPAIR DONE IAW EMB GST-1140/02, DAMAGE NR 9, GST-1169/02, ITEM 4, AND STANDARD SRM PRACApr 10, 2002 · N613AE · Emb EMB145 · Fuselage Main, Floor BeamSDR SIMA200210712Floorbeam · corrodedABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON RIGHT OMEGA BEAM BETWEEN FRAMES 23 AND 25. REMOVED CORROSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER. REPAIR DONE Apr 10, 2002 · N613AE · Emb EMB145 · Fuselage Main, Floor BeamSDR SIMA200210711Doubler · corrodedABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20. REMOVED PREVIOUS REPAIR (CORROSION LIMITED TO PREVIOUS REPAIR). FABRICATED A DOUBLER ANGLE, AND FILLER. REPAIRED IAW EMB145 SRM-145/1142, CHAPTERSApr 9, 2002 · N613AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200210713Beam · corrodedABI - DURING ABV INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY RIGHT BEAM AT FRAME 23. REMOVED CORROSION BY BLENDING. FABRICATED A U-SHAPE REPAIR. REPAIRED IAW EMB GST-1140/02, DAMAGE NR 7 AND STANDARD SRM PRACTICES. (M)Apr 9, 2002 · N613AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200210202Sill · corrodedDURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON RIGHT SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING. FABRICATED AND INSTALLED DOUBLER IAW EMB GST-1140/02 AND STANDARD SRM PRACTICES. (M)Apr 7, 2002 · N613AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200210201Frame · chafedABI - DURING INSPECTION OF AIRCRAFT, FOUND FRAME 81 CHAFED. REPLACED CHAFED FRAME IAW EMB 145 SRM 51-20-03, 51-40-03, AND STANDARD SRM PRACTICES. (M)Apr 7, 2002 · N613AE · Emb EMB145 · Fuselage Main, FrameSDR SIMA200210203Floorbeam · corrodedDURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY CENTER BEAM. REPLACED GALLEY CENTER BEAM IAW EMB 145 EMB SRM 145 51-40-02, GST-1128/02, AND STANDARD SRM PRACTICES. (M)Apr 5, 2002 · N613AE · Emb EMB145 · Fuselage Main, Floor BeamSDR SIMA200210701Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING. RIGHT OMEGA BEAM HAS CORROSION BETWEEN FRAMES 23 AND 25. FABRICATED DOUBLER IAW EMB145 SRM 51-40-02, 51-40-06, 51-20-03 AND GST-1169/02. (M)Apr 3, 2002 · N613AE · Emb EMB145 · Fuselage Main, Floor BeamSDR SIMA200210702Doubler · corrodedABI - THIS IS A LEVEL 2 FINDING. LEFT OMEGA BEAM REPAIR AT FRAME 20 HAS MINOR CORROSION. INSTALLED NEW OMEGA BEAM REPAIR AT FRAME 20 IAW EMB GST-1140-/02 AND SRM 51-40-02. (M)Apr 1, 2002 · N613AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200210704Floor Support · corrodedABI - THIS IS A LEVEL 2 FINDING. PASSENGER ENTRY FLOORBOARD SUPPORT HAS CORROSION. INSTALLED NEW FLOORBOARD SUPPORT IAW EMB 145 SRM 51-40-02, 51-40-03, 51-40-06. (M)Apr 1, 2002 · N613AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200210705Floor Support · corrodedABI - THIS IS A LEVEL 2 FINDING. RIGHT CABIN FORWARD FLOOR SUPPORT HAS CORROSION. BLENDED CORROSION, RESTORED PROTECTIVE TREATMENT, ACCEPTED AS IS IAW EMB 145 GST-1140/02. (M)Apr 1, 2002 · N613AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200210706Floorbeam · corrodedTHIS IS A LEVEL 2 FINDING. LEFT OMEGA BEAM HAS CORROSION BETWEEN FRAMES 22 AND 23. BLENDED CORROSION, PERFORMED NDT, RESTORED PROTECTIVE FINISH, ACCEPTED AS IS IAW EMB GST-1140/02. (M)Apr 1, 2002 · N613AE · Emb EMB145 · Fuselage Main, Floor BeamSDR SIMA200210707Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING. LEFT OMEGA BEAM CORRODED AT FRAME 25. BLENDED CORROSION, PERFORMED NDT, RESTORED PROTECTIVE FINISH, ACCEPTED AS IS IAW EMB 145 GST-1140/02. (M)Apr 1, 2002 · N613AE · Emb EMB145 · Fuselage Main, Floor Beam
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