# Service difficulty reports: N14514, cancelled Oct 30, 2018

A list on [N14514, cancelled Oct 30, 2018](https://openairdocs.org/deregistered/N14514-2018-10-30.md).

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

Page 1 of 2 · 65 reports

- [SDR ASOA20140701087](https://openairdocs.org/sdr/ASOA20140701087.md): Bulb · failed · Jul 1, 2014 · N14514 · Emb EMB135LR · Passenger Compartment Lighting
  > THE F/A REPORTED THE LIGHT AT SEAT 2A WAS FLICKERING AND HAD AN ELECTRICAL BURNING ODOR. MAINTENANCE R & R THE BULB, OPERATED CABIN LIGHTS WITH NO DEFECTS OR ODORS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140506067](https://openairdocs.org/sdr/ASOA20140506067.md): Skin · cracked · May 4, 2014 · N14514 · Emb EMB135LR · Fuselage Main, Plate/Skin
  > DURING 4A INSPECTION, THE LEFT AFT FUSELAGE SKIN WAS FOUND TO HAVE A 2 MM CRACK EMINATING FROM A RIVET ON FRAME 75, STRINGER 2L. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW DER APPROVED ETD2014-145-037541, AND THE ACFT WAS APPROVED FOR
- [SDR ASOA20140108006](https://openairdocs.org/sdr/ASOA20140108006.md): Inverter · inoperative · Jan 8, 2014 · N14514 · Emb EMB135LR · Emergency Lighting
  > DURING ROUTINE CHECK THE FWD EMERGENCY EXIT SIGN IN THE OVERWING AISLE CEILING PANEL WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 6 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131212282](https://openairdocs.org/sdr/ASOA20131212282.md): Light · inoperative · Dec 12, 2013 · N14514 · Emb EMB135LR · Emergency Lighting
  > AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R OVERHEAD EMERGENCY LIGHT IAW 33-50-13. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130423139](https://openairdocs.org/sdr/ASOA20130423139.md): Inverter · inoperative · Apr 20, 2013 · N14514 · Emb EMB135LR · Emergency Lighting
  > DURING ROUTINE CHECK THE GALLEY EMERGENCY LIGHTS FAILED OPS TESTING. MX R & R THE NR 3 INVERTER IAW AMM 33-50-11. THE EMERGENCY LIGHTS OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130322039H](https://openairdocs.org/sdr/ASOA20130322039H.md): Connector · disconnected · Mar 22, 2013 · N14514 · Emb EMB135LR · Light System Wiring
  > DURING MX INSPECTION, THE EMERGENCY LIGHT EXIT LOCATING SIGN IN THE GALLEY AISLE CEILING PANEL WAS FOUND TO BE INOPERATIVE. MX INSPECTED THE SIGN, RECONNECTED THE ELECTRICAL CONNECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN
- [SDR C2XA08IA185](https://openairdocs.org/sdr/C2XA08IA185.md): Sign · disconnected · Aug 2, 2008 · N14514 · Emb EMB135LR · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION LT EMERGENCY EXIT IDENTIFIER AT THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT, RESECURED THE CONNECTIONS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (
- [SDR C2XA08IA184](https://openairdocs.org/sdr/C2XA08IA184.md): Wire · broken · Aug 2, 2008 · N14514 · Emb EMB135LR · Light System Wiring
  > IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT ON THE SERVICE DOOR SWING ARM WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)
- [SDR C2XA08SH095](https://openairdocs.org/sdr/C2XA08SH095.md): Floor Support · corroded · Jul 11, 2008 · N14514 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM FR 21-23 HAS VARIOUS AREAS OF CORROSION ON LWR FLANGE WEB. MX REMOVED LT OMEGA BEAM FROM 17 SPLICE TO FR 26 AND INSTALLED WITH NEW IAW EC5320-01413 ANS CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)
- [SDR C2XA08IA135](https://openairdocs.org/sdr/C2XA08IA135.md): Ballast · inoperative · Jun 5, 2008 · N14514 · Emb EMB135LR · Emergency Lighting
  > IAH - FLIGHT 2452, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL ODOR IN THE CABIN. MAINTENANCE INSPECTED THE ACFT, AND REMOVED AND REPLACED THE LIGHT BALLAST AT ROW SIX. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETU
- [SDR C2XA08IA106](https://openairdocs.org/sdr/C2XA08IA106.md): Connector · dirty · Apr 8, 2008 · N14514 · Emb EMB135LR · Light System Wiring
  > IAH - FLIGHT 2791, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE SECOND AND THIRD SECTION OF AISLE PATH LIGHTING TO BE INOPERATIVE. MAINTENANCE CLEANED THE CONNECTOR ON THE AISLE PATH LIGHTING, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS A
- [SDR C2XA07IA227](https://openairdocs.org/sdr/C2XA07IA227.md): Light · inoperative · Oct 22, 2007 · N14514 · Emb EMB135LR · Emergency Lighting
  > DURING SCHEDULED MAINTENANCE THE EMERGENCY STRIP LIGHT AT ROW 3A TO 7A WAS FOUND TO BE INOPERATIVE. THE FLOOR STRIP WIRING WAS FOUND TO BE CHAFED. THE AFFECTED WIRE WAS REPAIRED, THE LIGHTS OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.
- [SDR C2XA07IA197](https://openairdocs.org/sdr/C2XA07IA197.md): Unknown · odor · Sep 9, 2007 · N14514 · Emb EMB135LR · Air Distribution System
  > IAH - FLIGHT 2890, DURING PRE-FLIGHT INSPECTION, THE NUMBER ONE ELECTRIC HYDRAULIC PUMP FAILED AND A SMOKE SMELL WAS REPORTED IN THE COCKPIT. MAINTENANCE OPERATIONALLY TESTED THE ELECTRIC HYDRAULIC PUMP WITH NO DEFECTS NOTED, AND COULD NOT DUPLICATE THE SMOKE
- [SDR C2XA07IA126](https://openairdocs.org/sdr/C2XA07IA126.md): Unknown · odor · May 28, 2007 · N14514 · Emb EMB135LR · Air Distribution System
  > SLP - FLIGHT 2148, THE CREW REPORTED A BURNING ODOR AT THE COFFEEMAKERS. THE AIRCRAFT RETURNED TO SLP WHERE THE COFFEEMAKERS WERE PLACED ON MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON FLIGHT 2148 WHERE MAINTENANCE I
- [SDR C2XA06IA157](https://openairdocs.org/sdr/C2XA06IA157.md): Unknown · smoke · Sep 23, 2006 · N14514 · Emb EMB135LR · Air Distribution System
  > LEX - FLIGHT 2671, THE CREW REPORTED SMOKE IN THE COCKPIT AFTER AN ACARS MESSAGE FOR PACK 2 VALVE CLOSED MESSAGE. THE AIRCRAFT DIVERTED TO LEX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND TH
- [SDR C2XA06IA111](https://openairdocs.org/sdr/C2XA06IA111.md): Controller · faulty · Jul 18, 2006 · N14514 · Emb EMB135LR · Passenger Compartment Lighting
  > DURING START, THE CREW REPORTED A BURNING SMELL IN THE COCKPIT AND CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE CABIN LIGHT CONTROLLER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06SH071](https://openairdocs.org/sdr/C2XA06SH071.md): Floor Support · corroded · Jul 1, 2006 · N14514 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LEFT OMEGA 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.
- [SDR C2XA05IA083](https://openairdocs.org/sdr/C2XA05IA083.md): Ballast · inoperative · Jun 18, 2005 · N14514 · Emb EMB135LR · Passenger Compartment Lighting
  > THE CREW REPORTED A BURNED/HOT ELECTRICAL ODOR COMING FROM THE GALLEY. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LIGHT BALLAST FOR THE GALLEY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC
- [SDR C2XA05IA054](https://openairdocs.org/sdr/C2XA05IA054.md): Relay · failed · Apr 18, 2005 · N14514 · Emb EMB135LR · Pitot/Static System
  > THE CREW REPORTED THAT THE NR 3 PITOT INOPERATIVE WHILE CLIMBING THROUGH CLOUDS, AND THE COCKPIT FILLED WITH SMOKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE CURRENT SENSING RELAY (K0057) FOR THE NUMBER THREE PITOT
- [SDR C2XA04IA126](https://openairdocs.org/sdr/C2XA04IA126.md): Light · inoperative · Oct 5, 2004 · N14514 · Emb EMB135LR · Emergency Lighting
  > IAH- FLIGHT 2621, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ON THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE
- [SDR C2XA04IA108](https://openairdocs.org/sdr/C2XA04IA108.md): Bulb · burned out · Aug 25, 2004 · N14514 · Emb EMB135LR · Emergency Lighting
  > IAH - DURING 3A INSPECTION, THE AFT OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04TY070](https://openairdocs.org/sdr/C2XA04TY070.md): Carbon Seal · leaking · Apr 15, 2004 · N14514 · Emb EMB135LR · Turbine Engine Oil System
  > AIR RETURN, FERRIED TO TYS FROM EWR, FOR LAV SMOKE ON EICAS, STRONG ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED THE ZERO CARBON SEAL ON THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKED GOOD IAW RR MM 72-25-40, 72-25-25, 72-21-05, 72-21-15, 72-50-00 AND EC
- [SDR C2XA04SH174](https://openairdocs.org/sdr/C2XA04SH174.md): Buttstrap · corroded · Mar 20, 2004 · N14514 · Emb EMB135LR · Fuselage Structure (General)
  > SHV- DURING C-CHECK THE AFT FLOORBEAM BUTTSTRAP BETWEEN FRAMES 17 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH173](https://openairdocs.org/sdr/C2XA04SH173.md): Sill · corroded · Mar 20, 2004 · N14514 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > SHV- DURING C-CHECK THE LT FLOOR SILL BETWEEN FRAMES 18 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH172](https://openairdocs.org/sdr/C2XA04SH172.md): Buttstrap · corroded · Mar 20, 2004 · N14514 · Emb EMB135LR · Fuselage Main, Floor Beam
  > SHV- DURING C-CHECK THE FORWARD FLOORBEAM BUTTSTRAP AT FRAME 14 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH167](https://openairdocs.org/sdr/C2XA04SH167.md): Floorbeam · corroded · Mar 17, 2004 · N14514 · Emb EMB135LR · Fuselage Main, Floor Beam
  > SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER SHIM REPAIR IAW EMB 135 SRM 51-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH170](https://openairdocs.org/sdr/C2XA04SH170.md): Support Bracket · corroded · Mar 17, 2004 · N14514 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE PASSENGER DOOR THRESHOLD AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH169](https://openairdocs.org/sdr/C2XA04SH169.md): Bracket · corroded · Mar 17, 2004 · N14514 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE PASSENGER DOOR THRESHOLD FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH168](https://openairdocs.org/sdr/C2XA04SH168.md): Support Beam · corroded · Mar 17, 2004 · N14514 · Emb EMB135LR · Fuselage Main, Structure
  > SHV - DURING C-CHECK THE AFT GALLEY SUPPORT BEAM BETWEEN FRAMES 22 AND 23 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.
- [SDR C2XA04SH166](https://openairdocs.org/sdr/C2XA04SH166.md): Floorbeam · cracked · Mar 17, 2004 · N14514 · Emb EMB135LR · Fuselage Main, Floor Beam
  > SHV - DURING C-CHECK, THE T-SECTION IN THE LOWER CARGO DOOR CUTOUT AT FRAME 67 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED T-SECTION IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH165](https://openairdocs.org/sdr/C2XA04SH165.md): Beam · corroded · Mar 16, 2004 · N14514 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CARGO DOOR LOWER CUT 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.
- [SDR C2XA04SH164](https://openairdocs.org/sdr/C2XA04SH164.md): Frame · cracked · Mar 16, 2004 · N14514 · Emb EMB135LR · Fuselage Main, Frame
  > SHV - DURING C-CHECK THE ATTACH ANGLE ON THE LOWER END OF THE T-SECTION AT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE CRACKED ANGLE, FABRICATED AND INSTALLED A NEW ANGLE IAW EMB 135 SRM 51-30-01 AND EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPRO
- [SDR C2XA04SH163](https://openairdocs.org/sdr/C2XA04SH163.md): Door Frame · cracked · Mar 16, 2004 · N14514 · Emb EMB135LR · Fuselage Main, Structure
  > SHV - DURING C-CHECK THE LEFT T-SECTION AT THE CARGO DOOR CUT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED SECTION IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH162](https://openairdocs.org/sdr/C2XA04SH162.md): Sill · corroded · Mar 16, 2004 · N14514 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AROUND THE NUT PLATES AT FRAME 21. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH152](https://openairdocs.org/sdr/C2XA04SH152.md): Intake · gouged · Mar 12, 2004 · N14514 · Emb EMB135LR · Engine Air Intake System
  > SHV - DURING C-CHECK, THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH151](https://openairdocs.org/sdr/C2XA04SH151.md): Intake · gouged · Mar 12, 2004 · N14514 · Emb EMB135LR · Engine Air Intake System
  > SHV - DURING C-CHECK, THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04IA004](https://openairdocs.org/sdr/C2XA04IA004.md): Bracket · distorted · Jan 8, 2004 · N14514 · Emb EMB135LR · Landing Gear Position and Warning
  > FLIGHT 3250 - PILOT REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND THE LT MAIN LANDING GEAR PROXIMITY SWITCH MOUNT BRACKET TO BE DISTORTED. THE AFFECTED BRACKE
- [SDR C2XA02CL196](https://openairdocs.org/sdr/C2XA02CL196.md): Switch · inoperative · Oct 7, 2002 · N14514 · Emb EMB135LR · Rudder Control System
  > CLT FLIGHT#3177 THE CREW REPORTED A RUDDER 1/2 FAIL MESSAGE ON CLIMBOUT.THE AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE #1 AND #2 RUDDER PRESSURE SWITCHES.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERV
- [SDR C2XA02CL133](https://openairdocs.org/sdr/C2XA02CL133.md): Autopilot Sys · malfunctioned · Jun 16, 2002 · N14514 · Emb EMB135LR · Autopilot System
  > CLE FLIGHT 4015 THE CREW REPORTED A AUTO PILOT FAIL MESSAGE AFTER FLIGHT INTO MODERATE TURBULENCE ASSOCIATED WITH BURNING SMELL IN THE COCKPIT AND CABIN. MAINTENANCE INSPECTED AND PERFORMED AUTO PILOT CHECKS AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEAS
- [SDR C2XA02CL056](https://openairdocs.org/sdr/C2XA02CL056.md): Wire · broken · Feb 20, 2002 · N14514 · Emb EMB135LR · Emergency Lighting
  > CLE FLIGHT#3133 THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT ROW 9 WAS INOPERATIVE.MAINTENANCE INSPECTED AND REPAIRED A WIRE ON THE EMERGENCY AISLE PATH LIGHTING STRIP.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR C2XA02TY003](https://openairdocs.org/sdr/C2XA02TY003.md): Proximity Switch · cracked · Jan 1, 2002 · N14514 · Emb EMB135LR · Landing Gear Position and Warning
  > TYS AT TAKEOFF THE LANDING GEAR/GROUND FAIL MESSAGE INDICATOR CAME ON. CREW RETURNED AND MAINTENANCE REMOVED AND REPLACED THE NLG WOW PROXIMITY SWITCH AND THEN ON SECOND ATTEMPT THE SWITCH HAD TO BE ADJUSTED TO THE TARGET. THE OPS CHECK WERE GOOD IAW EMB 1
- [SDR C2XA01TY226](https://openairdocs.org/sdr/C2XA01TY226.md): Proximity Switch · cracked · Jan 1, 2002 · N14514 · Emb EMB135LR · Landing Gear Position and Warning
  > TYS AT TAKEOFF THE LANDING GEAR/GROUND FAIL MESSAGE INDICATOR CAME ON. CREW RETURNED AND MAINTENANCE REMOVED AND REPLACED THE NLG WOW PROXIMITY SWITCH AND THEN ON SECOND ATTEMPT THE SWITCH HAD TO BE ADJUSTED TO THE TARGET. THE OPS CHECK WERE GOOD IAW EMB 1
- [SDR C2XA01TY223](https://openairdocs.org/sdr/C2XA01TY223.md): Floorbeam · corroded · Dec 30, 2001 · N14514 · Emb EMB135LR · Fuselage Main, Floor Beam
  > TYS, DURING A SCHEDULED 1C INSPECTION, CORROSION WAS FOUND ON SEVERAL AREAS OF THE FORWARD DIGITAL. MAINTENANCE REMOVED FORWARD DIGITAL AND CUT OUT DAMAGED AREA, FABRICATED DOUBLERS AND INSTALLED, REINSTALLED DIGITAL IAW-EC5320-01059, EMB-135/145-SRM-51-20-03
- [SDR C2XA01TY222](https://openairdocs.org/sdr/C2XA01TY222.md): Light · broken · Dec 30, 2001 · N14514 · Emb EMB135LR · Emergency Lighting
  > TYS, DURING A SCHEDULED 1C INSPECTION, THE NR 6 EMERGENCY TRACK LIGHT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE NR 6 TRACK LIGHTING IAW EMB-135-AMM-33-50-12. OPERATIONAL CHECKED GOOD. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.
- [SDR C2XA01TY221](https://openairdocs.org/sdr/C2XA01TY221.md): Switch · faulty · Dec 30, 2001 · N14514 · Emb EMB135LR · Oxygen System
  > TYS, During a scheduled 1C inspection, the oxygen deployement on step 13 of task card #35-20-00-770-001-A00 failed. Maintenance removed and replaced the altitude sensing switch. IAW-EMB-135-AMM-35-20-02, operational checked good. Aircraft will be released upon
- [SDR C2XA01TY220](https://openairdocs.org/sdr/C2XA01TY220.md): Angle · corroded · Dec 30, 2001 · N14514 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > TYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS DETECTED ON CENTER SUPPORT RAMP NEXT TO THE CARBON FIBER CROSSBEAM. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE AND REINSTALLED THE CARBON FIBER CROSSBEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACC
- [SDR C2XA01TY219](https://openairdocs.org/sdr/C2XA01TY219.md): Antenna · corroded · Dec 30, 2001 · N14514 · Emb EMB135LR · Air Collision Avoidance System
  > TYS DURING A SCHEDULED 1-C INSPECTION THE LOWER TCAS ANTENNA WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE TCAS ANTENNA IAW EMB 135 AMM34-43-03, PERFORMED OPS CHECK IAW EMB 135AMM 34-43-00. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION
- [SDR C2XA01TY218](https://openairdocs.org/sdr/C2XA01TY218.md): Bypass Jacket · corroded · Dec 30, 2001 · N14514 · Emb EMB135LR · Turbine Engine Bypass Section
  > TYS DURING A SCHEDULED 1-C INSPECTION THE NR 1 FANCASE TO BYPASS HAD CORROSION. MAINTENANCE CLEANED UP THE CORROSION. APPLIED CHEMICAL FILM COATING TO THE MAGNESIUM IAW RR AE3007A MM 70-00-00-300-818 AND APPLIED CORROSION RESISTANT PAINT IAW EC7220-01009.
- [SDR C2XA01TY217](https://openairdocs.org/sdr/C2XA01TY217.md): Rivet · corroded · Dec 30, 2001 · N14514 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > TYS DURING A SCHEDULED 1-C INSPECTION TWO RIVETS WERE FOUND CORRODED UNDERNEATH THE SERVICE DOOR THRESHOLD. MAINTENANCE REMOVED AND REPLACED THE TWO RIVETS. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF C-CHECK INSPECTION.
- [SDR C2XA01TY216](https://openairdocs.org/sdr/C2XA01TY216.md): Attach Fitting · gouged · Dec 29, 2001 · N14514 · Emb EMB135LR · Ailerons
  > TYS DURING A SCHEDULED 1-C INSPECTION, NOTED THAT THE LEFT AILERON FITTING WAS GOUGED. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF C-CHECK INSPECTION.

Next page: https://openairdocs.org/deregistered/N14514-2018-10-30/reports.md?page=2

## 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 = 'N14514' AND deregistration_id = 'N14514-2018-10-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14514-2018-10-30/reports

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