N24517, cancelled Sep 6, 2019

Service difficulty reports · 25

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 = 'N24517' AND deregistration_id = 'N24517-2019-09-06'
  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 C2XA08IA127Proximity Switch · faultyIAH - FLIGHT 2649, THE CREW REPORTED THAT THE NOSE LANDING GEAR DOORS OPENED IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR DOOR SEQUENCE PROXIMITY SWITCH. OPERATIONALLY CHECKED WIMay 15, 2008 · N24517 · Emb EMB135LR · Landing Gear Door Retract SectionSDR C2XA07IA149Light · inoperativeDURING SCHEDULED MAINTENANCE, THE SERVICE DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE WHEN TESTED. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONALLY TESTED THE SYSTEM AND CLEARED THE DISCREPANCY.Jun 23, 2007 · N24517 · Emb EMB135LR · Emergency LightingSDR C2XA07IA083Handle · looseFLIGHT 2102, THE CREW REPORTED THAT THE MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND IT SAFE FOR A FERRY FLIGHT WHERE IT LANDED WITHOUT INCIDENT. MFG MAINTENANCE INSPECTED THE DOOR, AND RESECURED THE INTERNAL HANApr 10, 2007 · N24517 · Emb EMB135LR · Passenger/Crew DoorsSDR C2XA06CL054Light · inoperativeDURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE SERVICE DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.May 28, 2006 · N24517 · Emb EMB135LR · Emergency LightingSDR C2XA05IA113Odor · detectedXNA - FLIGHT 3028, THE CREW REPORTED A STRONG ELECTRICAL SMELL IN THE COCKPIT ON APPROACH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT, AND MAINTENANCE INSPECTED THE AIRCRAFT, WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 13, 2005 · N24517 · Emb EMB135LR · Air Distribution SystemSDR C2XA05IA023Warning System · inoperativeIAH - FLIGHT 2373, ON DESCENT THE CREW REPORTED A GPWS WARNING AND A LANDING GEAR WARNING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE AURAL WARNING UNIT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS AFeb 9, 2005 · N24517 · Emb EMB135LR · Landing Gear Position and WarningSDR C2XA04SH477Control Module · will not testSHV - DURING C-CHECK THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE FROM THE FLIGHT ATTENDANTS CONTROL PANEL. MAINTENANCE REMOVED AND REPLACED THE LIGHTING CONTROL MODULE IAW EMB 135 AMM 33-21-01. THE ENSUING OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS APPROVAug 7, 2004 · N24517 · Emb EMB135LR · Emergency LightingSDR C2XA04SH467Beam · corrodedDURING C CHECK THE CARGO DOOR CUTOUT LOWER BEAM 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.Jul 25, 2004 · N24517 · Emb EMB135LR · Fuselage Main, StructureSDR C2XA04SH465Floorbeam · corrodedDURING (C) CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10, STEP 2 FIG. 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jul 22, 2004 · N24517 · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA04SH471Floorbeam · corrodedSHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAME 35 AND 39. MAINTENANCE REMOVED THE DAMAGED AREA AND FOUND IT TO BE GREATER THAN 30 PERCENT OF ORIGINAL MATERIAL THICKNESS, BUT WITHIN REPAIRABLE LIMITS. A DYE PENETRANT INSPECTIONJul 21, 2004 · N24517 · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA04SH464Floorbeam · corrodedDURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jul 21, 2004 · N24517 · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA04BT055Cable · bindingCREW REPORTED, FLAP FAIL INFLIGHT DURING DESCENT AT APPROXIMATELY 9000 MSL, APPROXIMATELY 240 KNOTS, SPEED BRAKE DEPLOYED OPEN. FLAP INDICATOR ON EICAS AMBER WITH DASHED LINE. QRH FLAP FAILURE CHECKLIST COMPLETED. ZERO FLAP LANDING PERFORMED. MAINTENANCE RApr 27, 2004 · N24517 · Emb EMB135LR · Trailing Edge Flap Control SystemSDR C2XA03IA077Gcu · faultyIAH - FLT NR 3325 - UPON APPROACH TO IAH THE CREW REPORTED THAT GENERATOR NUMBERS 1, 2, 3, AND APU SHOWING VOLTS BUT NO AMPS AND THAT GENERATOR 4 WENT OFF LINE AT 1500FT. THE AIRCRAFT LANDED AT IAH WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AAug 6, 2003 · N24517 · Emb EMB135LR · AC RegulatorSDR C2XA03CL001Bulb · burnedDURING 3A INSPECTION THE AFT AISLE EMERGENCY LIGHT WAS NOT ILLUMINATING IN THE TEST MODE. MAINTENANCE REPLACED THE AFT AISLE EMERGENCY LIGHT,IT THEN TESTED GOOD.Jan 3, 2003 · N24517 · Emb EMB135LR · Emergency LightingSDR C2XA02CL186Lamp · inoperativeCLE FLIGHT#3309 THE CREW REPORTED ROW 9 OVERHEAD EMERGENCY EXIT LIGHT WAS INOPERATIVE.MAINTENANCE INSPECTED AND REPLACED THE LAMPS.OPERATIONAL CHECKS WERE GOOD.Sep 22, 2002 · N24517 · Emb EMB135LR · Emergency LightingSDR C2XA02BT051Switch · faultyEWR---CO3181, CREW REPORTED, "AIR RETURN DUE TO LDG AIR GND FAILURE AND THRUST REVERSER #1&#2 DISAGREE" MESSAGES AFTER ROTATION. RUMBLING HEARD FROM NOSE ON CLIMBOUT. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT AND REMOVED AND REPLACED NOSE LANDING GEAR Sep 5, 2002 · N24517 · Emb EMB135LR · Nose/Tail Landing GearSDR C2XA02TY121Engine · corrodedTYS, During a schedule inspection corrosion was found on the left engine fancase, lower side. Maintenance removed the corrosion, applied chrome pickle solution to magnesium parts, applied corrosion resistant paint I/A/W-EC7000-01001, EC7220-01009, AE3007A-70-0Aug 7, 2002 · N24517 · Emb EMB135LR · Powerplant SystemSDR C2XA02TY120Engine · corrodedTYS, During a schedule inspection corrosion was found on the right engine fancase, lower side. Maintenance removed the corrosion, applied chrome pickle solution to magnesium parts, applied corrosion resistant paint I/A/W-EC7000-01001, Ec7220-01009, AE3007A-70-Aug 7, 2002 · N24517 · Emb EMB135LR · Powerplant SystemSDR C2XA02TY119Skin · gougedTYS - DURING A SCHEDULED 1-C INSPECTION, THE CENTER WING BOX OF THE HORIZONTAL STAB HAS SOME SCRATCHES AND GOUGES. MAINTENANCE BLENDED DAMAGE, PERFORMED DYE-PENETRANT INSPECTION. WILL BE RELEASED UPON COMPLETION OF ALL WORK.Aug 2, 2002 · N24517 · Emb EMB135LR · Horizontal Stabilizer, Plate/SkinSDR C2XA02TY118Frame · chafedTYS DURING A SCHEDULED 1-C INSPECTION, A CHAFE MARK WAS FOUND ON FRAME 70 NEXT TO THE BLEED AIR DUCT. BLENDED OUT THE AREA, PERFORM A DYE INSPECTION, ALODINED AND PAINTED. NO DEFECTS WERE FOUND AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.Aug 2, 2002 · N24517 · Emb EMB135LR · Fuselage Main, FrameSDR C2XA02TY116Gusset · corrodedTYS DURING A SCHEDULED 1-C INSPECTION THE AFT GUSSET IN THE GALLEY WAS FOUND CORRODED. MAINTENANCE R/R THE AFT GUSSET IAW 135/145 SRM 51-40-02.R/R SCREWS IAW EMB 135/14553-01-06. ALL WORK WAS ACCOMPLISH AND WILL BE REL. UPON COMPLETION OF ALL WORK.Aug 1, 2002 · N24517 · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA02TY115Floorbeam · corrodedTYS, DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL WAS FOUND CORRODED FROM FRAME 13 TO 16. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED DOUBLER, SHIM AND INSTALLED, ALODINED, PRIMED AND PAINTED IAW-EMB-135/145-SRM-53-21-10 AND 51-40-02. THE REPAIR WAS SAAug 1, 2002 · N24517 · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA02TY114Skin · dentedTYS, DURING A SCHEDULED INSPECTION THE LEFT, NR 2 LEADING EDGE WAS FOUND DENTED AROUND A SCREW HOLE ON THE LOWER CENTER SIDE. MAINTENANCE REPAIRED THE DENT IAW-EMB-GST2378/02, THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THAug 1, 2002 · N24517 · Emb EMB135LR · Leading Edge DevicesSDR C2XA02CL018Light · inoperativeCLE MAINTENANCE FOUND THE 2ND ROW OF EMERGENCY FLOOR PATH LIGHTING WAS INOPERATIVE DURING ROUTINE MAINTENANCE. MAINTENANCE REPLACED THE FLOOR LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Jan 23, 2002 · N24517 · Emb EMB135LR · Emergency LightingSDR C2XA01CL257Skin · crackedDURING OVERNIGHT MAINTENANCE A CRACK ON THE RUDDER II SKIN WAS FOUND.THE CRACK WAS ON THE RIGHT SIDE OF THE RUDDER AND CLOSE TO THE TRAILING EDGE.MAINTENANCE PERFORMED A PERMANENT REPAIR OF THE RUDDER II SKIN AS PER CONTINENTAL EXPRESS EC 5540-01015.THE AIRCRADec 24, 2001 · N24517 · Emb EMB135LR · Rudder, Plate/Skin
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