# Service difficulty reports: N14508, cancelled Sep 6, 2019

A list on [N14508, cancelled Sep 6, 2019](https://openairdocs.org/deregistered/N14508-2019-09-06.md).

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

- [SDR C2XA08CL071](https://openairdocs.org/sdr/C2XA08CL071.md): Carbon Seal · leaking · Jun 15, 2008 · N14508 · Emb EMB135ER · Turbine Engine Oil System
  > CLE FLIGHT 2290. THE CREW REPORTED ON SHORT FINAL RECEIVED AN ENG 2 LOW OIL PRESSURE WARNING MESSAGE. THE ENG WAS SHUT DOWN BY THE CREW IMMEDIATELY AFTER LANDING. MAINTENANCE INSPECTED AND FOUND MAJOR OIL LEAK AT THE REAR OF THE ENG. THE NR 2 ENG WAS REPLA
- [SDR C2XA08RI037](https://openairdocs.org/sdr/C2XA08RI037.md): Control Unit · defective · Mar 19, 2008 · N14508 · Emb EMB135LR · Master Cylinder/Brake Valve
  > FLIGHT 2424 - EWR - CREW REPORTED BRAKES INEFFECTIVE AT HIGH SPEED AFTER LANDING. BRAKE DEGRADE MESSAGE ON EICAS APPEARED MOMENTARILY, AND THEN DISAPPEARED, BUT BRAKE OPERATED NORMAL AT LOW SPEED. EWR MX REMOVED AND REPLACED BRAKE CONTROL UNIT AND PERFORMED
- [SDR C2XA07TY089](https://openairdocs.org/sdr/C2XA07TY089.md): Flashlight · inoperative · Dec 26, 2007 · N14508 · Emb EMB135ER · Emergency Equipment
  > NR 3 EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT LAMP IAW EMB 135 VCMM 25-60-02. OPS CK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA07TY085](https://openairdocs.org/sdr/C2XA07TY085.md): Battery · discharged · Dec 18, 2007 · N14508 · Emb EMB135ER · Emergency Lighting
  > FA FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY IAW EMB 135 AMM 33-50-16. OPS CK GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA07RI063](https://openairdocs.org/sdr/C2XA07RI063.md): Hydraulic Line · leaking · Jul 26, 2007 · N14508 · Emb EMB135ER · Hydraulic System, Main
  > FLT 4923 - EWR - AT MLG RETRACTION, CREW REPORTED THAT RT MLG RETRACTED FASTER THAN LF MLG CAUSING YAW MOTION TO THE RIGHT. EWR MX REMOVED AND REPLACED MLG ACTUATOR EXTENSION LINE AND BLEED THE SYSTEM. MX PERFORMED LG OPERATIONAL CHECK SUCCESSFULLY. ACFT PE
- [SDR C2XA06SH101](https://openairdocs.org/sdr/C2XA06SH101.md): Skin Panel · damaged · Oct 9, 2006 · N14508 · Emb EMB135ER · Fuselage Main, Plate/Skin
  > SHV - MAJOR - DURING C-CHECK THE FORWARD FUSELAGE II SKIN WAS FOUND TO BE CREASED FORWARD OF FR 9 AND BELOW STR 15R. AFTER INITIAL REWORK THE AREA WAS STILL CREASED, HAD MINOR OIL CANNING AND MINOR WAVINESS OUT OF SRM LIMITS. MAINTENANCE REMOVED THE DAMAGED
- [SDR C2XA06SH100](https://openairdocs.org/sdr/C2XA06SH100.md): Floor Support · corroded · Oct 7, 2006 · N14508 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10, FIG 206 DET B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06CL024](https://openairdocs.org/sdr/C2XA06CL024.md): Lamp · inoperative · Feb 14, 2006 · N14508 · Emb EMB135ER · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA05CL077](https://openairdocs.org/sdr/C2XA05CL077.md): Acm · defective · Sep 6, 2005 · N14508 · Emb EMB135ER · Cabin Cooling System
  > CLE FLIGHT NR 2268, CREW REPORTED, SAW AND SMELLED SMOKE IN THE AIRCRAFT WITH PACK NR 1 ON. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE REPORTED GOOD.
- [SDR C2XA04TY091](https://openairdocs.org/sdr/C2XA04TY091.md): Bulb · burned out · Jun 17, 2004 · N14508 · Emb EMB135ER · Emergency Lighting
  > DURING A SEVICE/ROUTINE OF A/C THE EMERGENCY LIGHT BULB WAS FOUND BLOWN OVERHEAD LEFT EMERGENCY DOOR. REPLACED BULB AND OPS CHECK WAS GOOD. A/C WAS RELEASED FOR SERVICE.
- [SDR C2XA04CL041](https://openairdocs.org/sdr/C2XA04CL041.md): Engine · failed · Apr 24, 2004 · N14508 · Emb EMB135ER · Engine (Turbine/Turboprop)
  > CLE FLIGHT NR 2162 THE CREW REPORTED NR 1 ENGINE HIGH VIBRATION ON DESCENT AND AFTER LANDING REPORTED LOW OIL PRESSURE. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA04SH113](https://openairdocs.org/sdr/C2XA04SH113.md): Control Panel · inoperative · Feb 27, 2004 · N14508 · Emb EMB135ER · Emergency Lighting
  > SHV- DURING C-CHECK THE EMERGENCY LIGHT PUSH BUTTON ON THE FLIGHT ATTENDANTS CONTROL PANEL WOULD NOT OPERATE THE EMERGENCY LIGHTING TEST. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANTS CONTROL PANEL IAW EMB 135 AMM II 25-27-09. THE AIRCRAFT WAS APPRO
- [SDR C2XA04SH108](https://openairdocs.org/sdr/C2XA04SH108.md): Support · corroded · Feb 26, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > DURING C CHECK THE MAIN DOOR THRESHOLD SILL SUPPORT WAS FOUND TO BE CORRODED AT FRAME 15 TO 18 AND STRINGER 15 LT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL SUPPORT IAW AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH107](https://openairdocs.org/sdr/C2XA04SH107.md): Stringer · corroded · Feb 26, 2004 · N14508 · Emb EMB135ER · Fuselage Main, Longeron/Stringer
  > SHV- DURING C-CHECK THE CENTER OMEGA BEAM STRINGER FROM FRAMES 22 TO 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRINGER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH106](https://openairdocs.org/sdr/C2XA04SH106.md): Buttstrap · corroded · Feb 26, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE BLENDED OUT THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH105](https://openairdocs.org/sdr/C2XA04SH105.md): Hinge Bracket · corroded · Feb 26, 2004 · N14508 · Emb EMB135ER · Vertical Stabilizer
  > SHV- DURING C-CHECK THE UPPER CENTER HINGE BRACKET ON THE VERTICAL STABILIZER TO THE RUDDER WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 AMM 20-10-01 AND EMB 135 IPC 55-31-00. THE AIRCRAFT WAS APPROVED FOR RETUR
- [SDR C2XA04SH104](https://openairdocs.org/sdr/C2XA04SH104.md): Crossbeam · corroded · Feb 26, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV- DURING C-CHECK THE CROSSBEAM AT FRAME 22 BETWEEN THE CENTER OMEGA BEAM AND THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV
- [SDR C2XA04SH103](https://openairdocs.org/sdr/C2XA04SH103.md): Skin · chafed · Feb 26, 2004 · N14508 · Emb EMB135ER · Engine Cowling System
  > SHV- DURING C-CHECK THE RIGHT HAND LOWER COWLING SKIN WAS FOUND TO BE CHAFED IN TWO AREAS BETWEEN STATIONS XN=2180.0 AND XN=2905.0. MAINTENANCE REMOVED THE DAMAGED AREAS AND PERFORMED DOUBLER REPAIRS IAW EMB 135 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RE
- [SDR C2XA04SH102](https://openairdocs.org/sdr/C2XA04SH102.md): Stiffener · chafed · Feb 26, 2004 · N14508 · Emb EMB135ER · Engine Cowling System
  > SHV- DURING C-CHECK THE RIGHT HAND LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH088](https://openairdocs.org/sdr/C2XA04SH088.md): Structure · chafed · Feb 20, 2004 · N14508 · Emb EMB135ER · Engine Cowling System
  > SHV- DURING C-CHECK THE NR 1 ENGINE UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH087](https://openairdocs.org/sdr/C2XA04SH087.md): Structure · chafed · Feb 20, 2004 · N14508 · Emb EMB135ER · Engine Cowling System
  > SHV- DURING C-CHECK THE AFT EDGE MEMBER ON THE NR 2 ENGINE UPPER COWLING WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH086](https://openairdocs.org/sdr/C2XA04SH086.md): Floorbeam · corroded · Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Main, Floor Beam
  > SHV- DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 1SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH085](https://openairdocs.org/sdr/C2XA04SH085.md): Floorbeam · corroded · Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Main, Floor Beam
  > SHV- DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH084](https://openairdocs.org/sdr/C2XA04SH084.md): Sill · corroded · Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LOWER SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH083](https://openairdocs.org/sdr/C2XA04SH083.md): Splice · gouged · Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV- DURING C-CHECK STRINGER 19 LEFT INTERNAL SPLICE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPLICE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH082](https://openairdocs.org/sdr/C2XA04SH082.md): Angle · corroded · Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH081](https://openairdocs.org/sdr/C2XA04SH081.md): Bracket · corroded · Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV- DURING C-CHECK THE PASSENGER DOOR 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 C2XA04SH080](https://openairdocs.org/sdr/C2XA04SH080.md): Sill · corroded · Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV- DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FORWARD SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH079](https://openairdocs.org/sdr/C2XA04SH079.md): Buttstrap · corroded · Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV- DURING C-CHECK THE CENTER BUTTSTRAP 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 C2XA04SH078](https://openairdocs.org/sdr/C2XA04SH078.md): Buttstrap · corroded · Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV- DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED AROUND THE SCREW HOLES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH077](https://openairdocs.org/sdr/C2XA04SH077.md): Stringer · gouged · Feb 20, 2004 · N14508 · Emb EMB135ER · Fuselage Main, Longeron/Stringer
  > SHV- DURING C-CHECK STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-24-02 AND EC 5320-01106. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH069](https://openairdocs.org/sdr/C2XA04SH069.md): Buttstrap · corroded · Feb 16, 2004 · N14508 · Emb EMB135LR · Fuselage Miscellaneous Structure
  > SHV- DURING C-CHECK THE AFT DIGITAL BUTTSTRAP AT FRAME 16 TO FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH068](https://openairdocs.org/sdr/C2XA04SH068.md): Doubler · corroded · Feb 16, 2004 · N14508 · Emb EMB135LR · Fuselage Main, Floor Beam
  > SHV- DURING C-CHECK THE RT FLOORBEAM DOUBLER CAP AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER CAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH067](https://openairdocs.org/sdr/C2XA04SH067.md): Doubler · corroded · Feb 16, 2004 · N14508 · Emb EMB135LR · Fuselage Main, Floor Beam
  > SHV- DURING C-CHECK THE RIGHT HAND FLOORBEAM DOUBLER CAP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH070](https://openairdocs.org/sdr/C2XA04SH070.md): Buttstrap · corroded · Feb 16, 2004 · N14508 · Emb EMB135ER · Fuselage Main, Floor Beam
  > SHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED IN THE LAVATORY BETWEEN FRAMES 55 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH060](https://openairdocs.org/sdr/C2XA04SH060.md): Sill · corroded · Feb 12, 2004 · N14508 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > SHV-DURING C-CHECK THE LEFT HAND 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 C2XA02CL145](https://openairdocs.org/sdr/C2XA02CL145.md): Odor · detected · Jul 5, 2002 · N14508 · Emb EMB135ER · Air Distribution System
  > CLE FLIGHT 3149 THE CREW REPORTED A BURNT RUBBER SMELL WITH THE PACK SYSTEM ON. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE PACK SYSTEM. NO DEFECTS WERE NOTED.
- [SDR C2XA02CL031](https://openairdocs.org/sdr/C2XA02CL031.md): Firewall · cracked · Feb 3, 2002 · N14508 · Emb EMB135ER · Fuselage Structure (General)
  > DURING ROUTINE MAINTENANCE THE APU FIREWALL WAS FOUND CRACKED AT UPPER RIGHT CORNER OF FIREWALL.THE FIREWALL WAS REPAIRED I/A/W EMBRAER GST-0401/02.THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR C2XA01CL232](https://openairdocs.org/sdr/C2XA01CL232.md): Smoke Warning · malfunctioned · Nov 25, 2001 · N14508 · Emb EMB135ER · Smoke Detection
  > CLE FLIGHT 3207 THE CREW REPORTED AFTER TAKEOFF RECEIVED A LAV SMOKE WARNING. THE AIRCRAFT RETURNED TO MDT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE LAV SMOKE SYSTEM. NO DEFECTS WERE FOUND. THE AIRCR
- [SDR C2XA01TY160](https://openairdocs.org/sdr/C2XA01TY160.md): Bulb · burned out · Oct 17, 2001 · N14508 · Emb EMB135ER · Emergency Lighting
  > TYS During a scheduled inspection the overhead emergency light on right side was found out. Maintenance removed and replaced the bulb, operational checks good I.A.W.-EMB-135-AMM-33-50-07, Aircraft released for service.
- [SDR C2XA01CL197](https://openairdocs.org/sdr/C2XA01CL197.md): Connector · burned · Aug 23, 2001 · N14508 · Emb EMB135ER · Buffet/Galleys
  > CLE FLIGHT 3692 THE CREW REPORTED A BURNING SMELL IN THE CABIN. MAINTENANCE INSPECTED AND FOUND THE GALLEY HOT JUG RECEPTACLE TO BE BURNT. THE RECEPTACLE CONNECTOR WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR C2XA01CL175](https://openairdocs.org/sdr/C2XA01CL175.md): Engine · failed · Jul 25, 2001 · N14508 · Emb EMB135ER · Engine (Turbine/Turboprop)
  > CLE FLIGHT 3722 THE CREW REPORTED THE NR 1 ENGINE FAILED AT 2800 FT WITH NO ABNORMAL INDICATIONS PRIOR TO FAILURE. THE AIRCRAFT DIVERTED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD. THE A
- [SDR C2XA01TY099](https://openairdocs.org/sdr/C2XA01TY099.md): Stringer · chafed · Jul 19, 2001 · N14508 · Emb EMB135ER · Fuselage Main, Longeron/Stringer
  > TYS DURING A SCHEDULED INSPECTION, STRINGER 19L BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED THE BLEND OUT REPAIR IAW EMB GST 2412/01, THE REPAIR WAS SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE.
- [SDR C2XA01TY098](https://openairdocs.org/sdr/C2XA01TY098.md): Floorbeam · corroded · Jul 19, 2001 · N14508 · Emb EMB135ER · Fuselage Main, Floor Beam
  > TYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE, LOCATED JUST AFT OF COCKPIT ENTRANCE WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE ACCOMPLISHED THE DOUBLER REPAIR IAW EMB GST 2405-01, THE REPAIR WAS SATISFACTORY. AIRCRAFT RELEASED F
- [SDR C2XA01CL089](https://openairdocs.org/sdr/C2XA01CL089.md): Receptacle · burned · Apr 24, 2001 · N14508 · Emb EMB135ER · Buffet/Galleys
  > YYZ FLIGHT 3898 THE CREW REPORTED A BURNING SMELL FROM THE LEFT COFFEE JUG. MAINTENANCE REPLACED THE LEFT COFFEE JUG RECEPTACLE CONNECTOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR C2XA01TY061](https://openairdocs.org/sdr/C2XA01TY061.md): Skin · damaged · Mar 30, 2001 · N14508 · Emb EMB135ER · Fuselage Main, Plate/Skin
  > TYS DURING A SCHEDULED INSPECTION, THE LEFT HAND AFT FUSELAGE SKIN AT FRAME 74 BETWEEN STRINGERS 15L AND 17L WAS FOUND TO BE DAMAGED. MAINTENANCE REPAIRED THE DAMAGED AREA IAW EMB SST-1031/00, REPAIR WAS SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE.

## 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 = 'N14508' AND deregistration_id = 'N14508-2019-09-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14508-2019-09-06/reports

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