# Service difficulty reports: N29515, cancelled Oct 30, 2018 A list on [N29515, cancelled Oct 30, 2018](https://openairdocs.org/deregistered/N29515-2018-10-30.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR ASOA20141004122](https://openairdocs.org/sdr/ASOA20141004122.md): Fan · overheated · Oct 4, 2014 · N29515 · Emb EMB135LR · Air Distribution Fan > THE CREW REPORTED THAT THE NAV CIRCUIT BREAKER TRIPPED DURING CLIMBOUT, AND AN ELECTRICAL BURNING ODOR AT 17,000 FT. THE ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE CIRCUIT BREAKER, PERFORMED OPS CHECKS WITH NO DEFECTS NOTED, DETERMONED - [SDR ASOA20140915116](https://openairdocs.org/sdr/ASOA20140915116.md): Inverter · inoperative · Sep 15, 2014 · N29515 · Emb EMB135LR · Emergency Lighting > DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE NR 2 AND 3 AISLE PATH FLOOR LIGHT STRIPS WOULD NOT ILLUMINATE. MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE - [SDR ASOA20140704088](https://openairdocs.org/sdr/ASOA20140704088.md): Solenoid Valve · malfunctioned · Jul 4, 2014 · N29515 · Emb EMB135LR · Landing Gear Door Retract Section > THE CREW REPORTED THAT THE NLG DOOR OPENED UNCOMMANDED IN FLIGHT. LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE NLG DOOR SOLENOID VALVE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131215221](https://openairdocs.org/sdr/ASOA20131215221.md): Battery Pack · discharged · Dec 15, 2013 · N29515 · Emb EMB135LR · Emergency Lighting > DURING MAINTENANCE INSPECTION, FORWARD THREE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R BATTERY PACK, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE. - [SDR C2XA08IA149](https://openairdocs.org/sdr/C2XA08IA149.md): Door · out of adjust · Jul 2, 2008 · N29515 · Emb EMB135LR · Passenger/Crew Doors > IAH - FLIGHT 2975, THE CREW REPORTED THAT THE MAIN CABIN DOOR GETS HUNG UP WHEN OPENING ON THE UPPER RT. MAINTENANCE ADJUSTED THE PAX DOOR, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) - [SDR C2XA08IA141](https://openairdocs.org/sdr/C2XA08IA141.md): Unknown · odor · Jun 10, 2008 · N29515 · Emb EMB135LR · Air Distribution System > IAH - FLIGHT 2386, DURING POST FLIGHT INSPECTION THE FLIGHT ATTENDANT REPORTED A BURNING ODOR IN THE CABIN. MAINTENANCE INSPECTED THE ACFT, NR 2 PACK SYSTEM, AND CABIN LIGHTS, ALL WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) - [SDR C2XA08IA117](https://openairdocs.org/sdr/C2XA08IA117.md): Light · disconnected · Apr 21, 2008 · N29515 · Emb EMB135LR · Emergency Lighting > IAH - DURING MAINTENANCE INSPECTION A FLOOR PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE LIGHT STRIP ON MEL 33-50-00/2 CAT "C" CONTROL NUMBER 143990, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON - [SDR C2XA07IA175](https://openairdocs.org/sdr/C2XA07IA175.md): Inverter · inoperative · Jul 26, 2007 · N29515 · Emb EMB135LR · Emergency Lighting > IAH -FLIGHT 2487, DURING CREW INSPECTION THE RT EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 5 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE - [SDR C2XA07IA059](https://openairdocs.org/sdr/C2XA07IA059.md): Battery Pack · discharged · Mar 8, 2007 · N29515 · Emb EMB135LR · Emergency Lighting > IAH - DURING MAINTENANCE INSPECTION THE AFT AISLE PATH EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RE - [SDR C2XA06IA153](https://openairdocs.org/sdr/C2XA06IA153.md): Connector · loose · Sep 19, 2006 · N29515 · Emb EMB135LR · Landing Gear System Wiring > IAH - FLIGHT 2063, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL CAUTION ON CLIMB AND THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RESECURED THE CONNECTOR ON THE LT MAIN LANDING GEAR WOW PROXY SWIT - [SDR C2XA06IA130](https://openairdocs.org/sdr/C2XA06IA130.md): Landing Gear · underserviced · Aug 15, 2006 · N29515 · Emb EMB135LR · Nose/Tail Landing Gear > IAH - FLIGHT 2703, THE CREW REPORTED A AIR/GROUND FAIL MESSAGE ON GEAR RETRACTION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND SERVICED THE NOSE LANDING GEAR, OPERATIONALLY CHECKED WITH NO DEFECTS, AN - [SDR C2XA06IA042](https://openairdocs.org/sdr/C2XA06IA042.md): Connector · defective · Mar 19, 2006 · N29515 · Emb EMB135LR · Landing Gear System Wiring > IAH - FLIGHT 2164, THE CREW REPORTED A LANDING GEAR AIR/DRND FAILURE AFTER T/O, AND THAT THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WEIGHT ON WHEELS CONNECTOR ON THE NOSE LA - [SDR C2XA04TY058](https://openairdocs.org/sdr/C2XA04TY058.md): Sill · corroded · Mar 28, 2004 · N29515 · Emb EMB135LR · Fuselage Miscellaneous Structure > TYS DURING A SCHEDULED 2C INSPECTION THE LEFT FLOOR SUPPORT FRAME WAS CORRODED AT FR 20 AND FR 21. MAINT REMOVED AND REPLACED THE LEFT FORWARD SILL IN THE AFFECTED AREA IAW EMB 135/145 SRM 51-40-02; 51-40-06 AND 51-20-03. ALL WORK WAS ACCOMPLISHED AND WILL - [SDR C2XA04TY057](https://openairdocs.org/sdr/C2XA04TY057.md): Floorbeam · corroded · Mar 28, 2004 · N29515 · Emb EMB135LR · Fuselage Main, Floor Beam > TYS DURING A SCHEDULED 2C INSPECTION THE LEFT FLOORBEAM CAP HAD AREAS OF CORROSION AT FR 19-23. MAINT REMOVED AND REPLACED THE LEFT FLOORBEAM TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. - [SDR C2XA03TY102](https://openairdocs.org/sdr/C2XA03TY102.md): Engine · lack of lube · Jul 30, 2003 · N29515 · Emb EMB135LR · Engine (Turbine/Turboprop) > THE LT ENGINE IMPENDING OIL BYPASS INFLIGHT. AFTER APPROXIMATELY 2 MINUTES OIL PRESSURE DROPPED INTO THE RED, 32 PSI AND DROPPING. THE CREW PERFORMED PRECAUTIONARY ENGINE SHUTDOWN. LANDED AT MEM. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW-TASK CA - [SDR C2XA02CL146](https://openairdocs.org/sdr/C2XA02CL146.md): Wire Harness · faulty · Jul 10, 2002 · N29515 · Emb EMB135LR · Light System Wiring > CLE FLIGHT 3462 THE CREW REPORTED A ELECTRICAL SMELL COMING FROM SIDE WALL PANEL AT ROW 4A. MAINTENANCE INSPECTED AND FOUND A MELTED PLASTIC CONNECTOR FOR THE CABIN LIGHT BULB. THE AIRCRAFT WAS RELEASED FOR SERVICE. REPLACED SIDEWALL LIGHTING HARNESS ASSEMB - [SDR C2XA02BT031](https://openairdocs.org/sdr/C2XA02BT031.md): Harness · faulty · Jul 10, 2002 · N29515 · Emb EMB135LR · Passenger Compartment Lighting > DSM/EWR---CO3463, CREW REPORTED "BURNING SMELL COMING FROM SIDEWALL PANEL IN ROW 4 SEAT A....MAINTENANCE IN DSM RELEASED AIRCRAFT IAW MEL #33-20-00 CATEGORY "C" PLACARD #023338 AIRCRAFT RETURNED TO SERVICE. CO 4362, EWR MAINTENANCE CLEARED PLACARD BY REMOVIN - [SDR C2XA02CL068](https://openairdocs.org/sdr/C2XA02CL068.md): Light · inoperative · Mar 8, 2002 · N29515 · Emb EMB135LR · Emergency Lighting > CLE FLIGHT 3237 THE CREW REPORTED 1 SECTION OF EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY AISLE PATH LIGHTING SECTION. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA02TY045](https://openairdocs.org/sdr/C2XA02TY045.md): Wire · broken · Feb 22, 2002 · N29515 · Emb EMB135LR · Light System Wiring > TYS, DURING A SCHEDULED 1C INSPECTION A BROKEN WIRE WAS FOUND ON EMERGENCY LIGHT STRIP ON PANEL 251DE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW-EMB-135-AMM-33-50-12, OPERATIONAL CHECKED GOOD, AIRCRAFT RELEASED TO SERVICE. - [SDR C2XA02TY044](https://openairdocs.org/sdr/C2XA02TY044.md): Skin · dented · Feb 21, 2002 · N29515 · Emb EMB135LR · Fuselage Main, Plate/Skin > TYS, DURING A SCHEDULED 1C INSPECTION, A DENT WAS FOUND ON THE FUSELAGE SKIN AFT OF FR24, BELOW STR 10R. MAINTENANCE RE CONTOURED DENT, PERFORMED DYE-PENATRENT INSPECTION (NO CRACKS NOTED) IAW-EMB-GST-0504/2. REPAIR PROCEDURE WAS SATISFACTORY AND AIRCRAFT WI - [SDR C2XA02TY043](https://openairdocs.org/sdr/C2XA02TY043.md): Plate · corroded · Feb 21, 2002 · N29515 · Emb EMB135LR · Fuselage Miscellaneous Structure > TYS, During a scheduled 1C inspection, corrosion was found on the forward digital plate aft of cockpit door. Maintenance removed the corrosion by cutting out the center section and installed a new section, fabricated and installed doubler and shims. I/A/W-EMB- - [SDR C2XA02TY042](https://openairdocs.org/sdr/C2XA02TY042.md): Beam · corroded · Feb 21, 2002 · N29515 · Emb EMB135LR · Fuselage Main, Floor Beam > TYS, During a scheduled 1C inspection, corrosion was found on the left omega beam ar FR20 under the carbon fiber beam. Maintenance cut out the damage, fabricated an external angle, plate and filler I/A/W-EMB-135/145-SRM-53-21-10 and reinstalled the left ramp a - [SDR C2XA02TY041](https://openairdocs.org/sdr/C2XA02TY041.md): Support · corroded · Feb 21, 2002 · N29515 · Emb EMB135LR · Fuselage Miscellaneous Structure > TYS, During a scheduled 1C inspection, corrosion was found on the center omega beam ramp support between FR19-20. Maintenance removed and replaced the ramp support. I/A/W-EMB-135/145-SRM-51-40-02. Repair procedure was satisfactory and aircraft will be released - [SDR C2XA02TY040](https://openairdocs.org/sdr/C2XA02TY040.md): Angle · corroded · Feb 21, 2002 · N29515 · Emb EMB135LR · Fuselage Miscellaneous Structure > TYS, During a scheduled 1C inspection, corrosion was found on the support angle at main door entrance below the threshold strip. Maintenance removed and replaced the support angle. I/A/W-EMB-135/145-SRM-51-40-02. Repair procedure was satisfactory and aircraft - [SDR C2XA02TY039](https://openairdocs.org/sdr/C2XA02TY039.md): Floorbeam · corroded · Feb 21, 2002 · N29515 · Emb EMB135LR · Fuselage Main, Floor Beam > TYS, DURING A SCHEDULED 1C INSPECTION, CORROSION WAS FOUND ON THE FORWARD DIGITAL PLATE AFT OF COCKPIT DOOR. MAINTENANCE REMOVED CORROSION BY CUTTING OUT THE CENTER SECTION AND INSTALLING A NEW SECTION, FABRICATED AND INSTALLED DOUBLERS AND SHIMS, ALODINED AN - [SDR C2XA02TY038](https://openairdocs.org/sdr/C2XA02TY038.md): Beam · corroded · Feb 21, 2002 · N29515 · Emb EMB135LR · Fuselage Main, Floor Beam > TYS, During a scheduled 1C inspection, corrosion was found on the forward center omega beam galley area. Maintenance removed corrosion and replaced affected rivits, alodined and primed. I/A/W-EMB-135/145-CPM-51-21-05 & 06. Repair procedure was satisfactory and - [SDR C2XA02TY037](https://openairdocs.org/sdr/C2XA02TY037.md): Floorbeam · corroded · Feb 20, 2002 · N29515 · Emb EMB135LR · Fuselage Main, Floor Beam > TYS DURING A SCHEDULED 1-C INSPECTION THE FORWARD DIGITAL PLATE AFT OF THE COCKPIT DOOR WAS FOUND CORRODED. MAINTENANCE REMOVED THE CORROSION BY CUTTING OUT THE CENTER SECTION OF THE DIGITAL PLATE AND FAB. A NEW PART WITH A DOUBLER AND SHIM, ALODINE, PRIME - [SDR C2XA02TY035](https://openairdocs.org/sdr/C2XA02TY035.md): Angle · corroded · Feb 20, 2002 · N29515 · Emb EMB135LR · Fuselage Miscellaneous Structure > TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND ON THE SUPPORT ANGLE AT THE MAIN DOOR ENTRANCE BELOW THE THRESHOLD. MAINTENANCE REMOVED AND REPLACED THE SUPPORT ANGLES, ALODINE AND PAINTED IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AN - [SDR C2XA02TY034](https://openairdocs.org/sdr/C2XA02TY034.md): Lever · gouged · Feb 19, 2002 · N29515 · Emb EMB135LR · Elevator, Tab Structure > TYS DURING A SCHEDULED 1-C INSPECTION THE RT SERVO TAB DOG BONE WAS FOUND WEARING INTO THE ELEVATOR SUPPORT BRACKET WHICH REQUIRED A GST. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. - [SDR C2XA02TY033](https://openairdocs.org/sdr/C2XA02TY033.md): Lever · gouged · Feb 19, 2002 · N29515 · Emb EMB135LR · Elevator, Tab Structure > TYS DURING A SCHEDULED 1-C INSPECTION THE LT SERVO TAB DOG BONE WAS FOUND WEARING AGAINST THE ELEVATOR SUPPORT BRACKET, WHICH REQUIRED A GST. ALL WORK WAS ACCOMPLISHED IAW GST-0522/02 AND WILL BE RELEASED UPON COMPLETION OF THE INSPECTION. - [SDR C2XA02TY032](https://openairdocs.org/sdr/C2XA02TY032.md): Wire · broken · Feb 18, 2002 · N29515 · Emb EMB135LR · Light System Wiring > TYS DURING A SCHEDULED 1-C INSPECTION A BROKEN WIRE WAS FOUND ON THE PROXIMITY LIGHT STRIP ON PANEL 251DF. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP IAW EMB 135/145 AMM 33-50-12. OPS CHECK GOOD AND WILL BE RELEASED UPON COMPLETION OF INSPECTION. - [SDR C2XA02TY031](https://openairdocs.org/sdr/C2XA02TY031.md): Duct · corroded · Feb 18, 2002 · N29515 · Emb EMB135LR · Turbine Engine Bypass Section > TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND BETWEEN THE OUTER BYPASS AND THE FAN CASE ON NR 2 ENGINE. MAINTENANCE CLEANED THE AFFECTED AREA, APPLIED A CHEMICAL COATING AND APPLIED CORROSION RESISTANT PAINT IAW EC7000-01001. WORK WAS ACCOMPLISH - [SDR C2XA02TY030](https://openairdocs.org/sdr/C2XA02TY030.md): Support · corroded · Feb 18, 2002 · N29515 · Emb EMB135LR · Fuselage Miscellaneous Structure > TYS DURING A SCHEDULED 1-C INSPECTION THE RAMP SUPPORT ON THE CENTER OMEGA BEAM BETWEEN FR'S 19 AND 20 HAS A AREA OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE RAMP SUPPORT IAW EMB 135/145 SRM 51-40-02. WORK WAS SATISFACTORY AND WILL BE RELEASED UPON CO ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N29515' AND deregistration_id = 'N29515-2018-10-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N29515-2018-10-30/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.