# Service difficulty reports: N14952, cancelled Oct 5, 2015

A list on [N14952, cancelled Oct 5, 2015](https://openairdocs.org/deregistered/N14952-2015-10-05.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 3 · 109 reports

- [SDR ASOA20141120093](https://openairdocs.org/sdr/ASOA20141120093.md): Light · faulty · Nov 20, 2014 · N14952 · Emb EMB145LR · Emergency Lighting
  > THE CREW REPORTED THE EMERGENCY FLOOR LIGHTS WERE INOPERATIVE AT ROWS 3-18. MAINTENANCE INSPECTED AND REPLACED THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECKS WERE GOOD.
- [SDR ASOA20141117131](https://openairdocs.org/sdr/ASOA20141117131.md): Charger · inoperative · Nov 17, 2014 · N14952 · Emb EMB145LR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION THE FWD RT SIDE EMERGENCY EXIT SIGN WAS DISCOVERED INOPERATIVE. MX R & R THE EMERGENCY LIGHT SYSTEM BATTERY CHARGER WITH OPS, GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140906095](https://openairdocs.org/sdr/ASOA20140906095.md): Unknown · smoke · Sep 6, 2014 · N14952 · Emb EMB145LR · Indicating/Recording System
  > CREW REPORTED SMOKE COMING FROM LIGHT CONTROL PANEL ON F/O'S SIDE. MAINTENANCE INSPECTED BEHIND F/O'S LIGHT CONTROL PANEL AND OTHER PANELS IN THE VICINITY AND COULD NOT FIND ANY DEFECTS. CREW TAXIED AND RAN ALL SYS AND WAS UNABLE TO DUPLICATE ANY SMOKE OR O
- [SDR ASOA20140824092R](https://openairdocs.org/sdr/ASOA20140824092R.md): Battery Pack · discharged · Aug 24, 2014 · N14952 · Emb EMB145LR · Emergency Lighting
  > CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT STAY ON DURING F/A TEST. MAINTENANCE CHARGED EMERGENCY LIGHT SYSTEM BATTERIES AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130809092R](https://openairdocs.org/sdr/ASOA20130809092R.md): Unknown · odor · Aug 9, 2013 · N14952 · Emb EMB145LR · Air Distribution System
  > PILOT REPORTED A STRONG EXHAUST/FUEL ODOR IN FLIGHT DECK AND CABIN THROUGHOUT FLIGHT. MX RAN THE ENGINES AND APU WITH NO FUEL OR EXHAUST ODOR NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130420290](https://openairdocs.org/sdr/ASOA20130420290.md): Light · inoperative · Apr 20, 2013 · N14952 · Emb EMB145LR · Emergency Lighting
  > ACFT WAS IN FOR A LINE CHECK WHEN INSPECTION FOUND A FLOOR PROXIMITY LIGHT STRIP INOPERATIVE BETWEEN ROLL 2 THRU5. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECK GOOD AND WAS RELEASED.
- [SDR ASOA20121213149](https://openairdocs.org/sdr/ASOA20121213149.md): Door Frame · corroded · Dec 13, 2012 · N14952 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C-CHECK LT OVERWING EMERGENCY EXIT LOWER FRAME CORRODED UNDER TEFLON GUIDE. MAINTENANCE PERFORMED AND COMPLETED REPAIR AT LT OVERWING EMERGENCY EXIT LOWER FRAME IAW EC 5220-01043. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121213148](https://openairdocs.org/sdr/ASOA20121213148.md): Shear Tie · corroded · Dec 13, 2012 · N14952 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > DURING C-CHECK SHEAR TIE AT FRAME 68 CORRODED. MAINTENANCE PERFORMED AND COMPLETED REPAIR AT FRAME 68 BY INSTALLING DOUBLER AND FILLER IAW EC 5320-01494. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121213147](https://openairdocs.org/sdr/ASOA20121213147.md): Frame · corroded · Dec 13, 2012 · N14952 · Emb EMB145LR · Fuselage Main, Frame
  > DURING C-CHECK, FRAME 65 CORRODED, IN UPPER RADIUS AT STRINGER 17L AND AT NUT PLATES FOR GUIDE. MAINTENANCE COMPLETED REPAIR AT FRAME 65 STRINGER 17L IAW EC5330-02661. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121213146](https://openairdocs.org/sdr/ASOA20121213146.md): Stringer · corroded · Dec 13, 2012 · N14952 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STRINGER 20L CORRODED, AROUND RIVETS (2 EA) BETWEEN FRAMES 65-66. MAINTENANCE COMPLETED STRINGER REPAIR AT FRAMES 65-66 STRINGER 20L IAW SRM 53-00-03. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121213145](https://openairdocs.org/sdr/ASOA20121213145.md): Sill · corroded · Dec 13, 2012 · N14952 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, CARGO DOOR SILL CORRODED, FROM FRAME 65 TO 68. MAINTENANCE R & R CARGO DOOR SILL AT FRAMES 65-68 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121213144](https://openairdocs.org/sdr/ASOA20121213144.md): Shear Tie · corroded · Dec 13, 2012 · N14952 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > DURING C-CHECK, SHEAR TIE CORRODED, FRAME 65, STRINGER 17L. MAINTENANCE COMPLETED SHEAR TIE SPLICE REPAIR AT FRAME 65, STRINGER 17L IAW EC5320-01494, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120906074](https://openairdocs.org/sdr/ASOA20120906074.md): Wire Harness · faulty · Sep 6, 2012 · N14952 · Emb EMB145 · Light System Wiring
  > THE CREW REPORTED A STRONG ELECTRICAL ODOR IN CABIN. 17A CEILING LIGHT WAS INOPERATIVE. MX REPLACED ROW 17A CEILING LIGHT ELECTRICAL HARNESS ASSY. OPS CHECKS WERE GOOD.
- [SDR ASOA20120507044](https://openairdocs.org/sdr/ASOA20120507044.md): Charger · faulty · May 7, 2012 · N14952 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MX THE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER AND EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.
- [SDR ASOA20111215009](https://openairdocs.org/sdr/ASOA20111215009.md): Conditioner · faulty · Dec 8, 2011 · N14952 · Emb EMB145LR · Fuel Indicating System
  > AFTER TAKEOFF, IN CLIMB CREW REPORTED FUEL QTY NR1 WENT TO DASHES AND FUEL QUANITY NR 2 READ 0 LBS. CREW PERFORMED AIR RETURN WITHOUT ISSUE. MX R & R FUEL CONDITIONING UNIT IAW AMM 28-41-01 WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11IA255](https://openairdocs.org/sdr/C2XA11IA255.md): Smoke Detector · malfunctioned · Nov 8, 2011 · N14952 · Emb EMB145LR · Smoke Detection
  > MCI - THE LAV SMOKE DETECTOR WAS REPORTED AS MALFUNCTIONING. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11CL223](https://openairdocs.org/sdr/C2XA11CL223.md): Uplock · failed · Oct 4, 2011 · N14952 · Emb EMB145LR · Landing Gear Retraction/Extension System
  > THE CREW REPORTED IMMEDIATELY AFTER TAKEOFF FROM CLE A LOUD REPETITIVE THUMPING NOISE FROM UNDER THE AIRCRAFT. MOMENTARILY THE LEFT MAIN GEAR INDICATED AMBER CROSS-HATCHES WITH A MISCOMPARE INDICATION ON THE COCKPIT EICAS. CREW PERFORMED AN AIR RETURN TO CLE
- [SDR C2XA11IA201](https://openairdocs.org/sdr/C2XA11IA201.md): Window · malfunctioned · Sep 6, 2011 · N14952 · Emb EMB145LR · Flight Compartment Windows
  > IAH - FLIGHT 4586, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE CAPTAINS DV WINDOW WOULD NOT OPEN. MAINTENANCE INSPECTED THE AIRCRAFT AND VERIFIED NORMAL OPERATION OF THE CAPTAINS DV WINDOW, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11TY131](https://openairdocs.org/sdr/C2XA11TY131.md): Light · blown · Aug 20, 2011 · N14952 · Emb EMB145LR · Emergency Lighting
  > TYS - A/C WAS IN FOR A ROUTINE CHECK WHEN INSPECTION FOUND THE EMERGENCY LIGHT BLOWN ON THE RIGHT OVERHEAD WING. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD AND WAS RELEASED.
- [SDR C2XA11CL174](https://openairdocs.org/sdr/C2XA11CL174.md): Switch · faulty · Jul 25, 2011 · N14952 · Emb EMB145LR · Pneumatic Distribution System
  > CLE FLT 2431 THE CREW REPORTED A BLEED 2 VALVE CLOSED MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE BLEED 2 ON/OFF PUSH BUTTON SWITCH. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11CL167](https://openairdocs.org/sdr/C2XA11CL167.md): Duct · leaking · Jul 16, 2011 · N14952 · Emb EMB145LR · Pneumatic Distribution System
  > ORD FLT 6187 THE CREW REPORTED A BLEED 1 LEAK MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE. MAINTENANCE REPLACED THE BLEED LINE O-RINGS AT JOINT 5, 9, 11, 13, 15, 19 AND 23. ALSO REPLACED THE NR 1 BLEED VALVE Y DUCT ASSEMBLY AND AFT CLAMP. OPERATIONAL
- [SDR C2XA11CL169](https://openairdocs.org/sdr/C2XA11CL169.md): Battery · overtemp · Jul 15, 2011 · N14952 · Emb EMB145LR · Battery/Charger System
  > ORD FLT 5854 THE CREW REPORTED A BATTERY NR 1 OVERTEMP MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT FURTHER INCIDENT.
- [SDR C2XA11CL121](https://openairdocs.org/sdr/C2XA11CL121.md): Light · inoperative · May 12, 2011 · N14952 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE AISLE PATH EMERGENCY LIGHT STRIPS NR 3 AND NR 4 WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT STRIPS. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11TY042](https://openairdocs.org/sdr/C2XA11TY042.md): Battery · discharged · Apr 6, 2011 · N14952 · Emb EMB145LR · Emergency Lighting
  > FLOOR PROX LIGHTS NR 1 2 & 3 ARE INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04 OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA11IA063A](https://openairdocs.org/sdr/C2XA11IA063A.md): Acm · inoperative · Mar 26, 2011 · N14952 · Emb EMB145LR · Cabin Cooling System
  > MTY - FLIGHT 2127, THE CREW REPORTED THAT THE NUMBER ONE PACK WAS SURGING AND THE CABIN FILLS WITH SMOKE. PACK ONE WAS PLACED ON MEL, AND THE AIRCRAFT SUBSEQUENTLY LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ACM, OPERATIONALLY TESTED W
- [SDR C2XA11TY018](https://openairdocs.org/sdr/C2XA11TY018.md): Skin · dented · Feb 25, 2011 · N14952 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > TYS - A/C HAD A DENT IN A PRIEVIOUS REPAIR AND TO MAY IN 1 AREA BETWEEN FR19 AND FR 20 AND STR 15L AND WAS PLACED ON 750 FLIGHT CYLE DMI. MAINTENANCE REMOVED AND REPLACED THE CENTER FUSELAGE 1 LEFT DOOR SURROUND SKIN PANEL IAW EC5330-02372. PERFORMED A RVSM
- [SDR C2XA11IA023](https://openairdocs.org/sdr/C2XA11IA023.md): Probe · inoperative · Jan 25, 2011 · N14952 · Emb EMB145LR · Fuel Quantity Indicator
  > HOU - FLIGHT 2636 THE CREW REPORTED THAT THE NR 2 FUEL QUANTITY INDICATION DASHED OUT. THE AIRCRAFT DIVERTED TO HOU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT FOR LEAKS WITH NO DEFECTS NOTED, AND PLACED THE NR 2 FUEL QUANTITY ON MEL
- [SDR C2XA10IA311](https://openairdocs.org/sdr/C2XA10IA311.md): Wire · burned · Nov 22, 2010 · N14952 · Emb EMB145LR · Light System Wiring
  > MTY - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT SIDEWALL LIGHT AT 9A TO BE SMOKING. MAINTENANCE PLACED THE SIDEWALL LIGHT IN MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 11/25/10 IAH MAINTENANCE REPAIRED A WIRE ON THE AFFECTED SIDEWA
- [SDR C2XA10TY180](https://openairdocs.org/sdr/C2XA10TY180.md): Light · inoperative · Nov 17, 2010 · N14952 · Emb EMB145LR · Emergency Lighting
  > TYS - EMERGENCY FLOOR LIGHTS AT ROWS 6 AND 12 INOP. REMOVED AND REPLACED ROW 6 AND ROW 12 EMERGENCY LIGHT STRIPS, OPS CHECK GOOD.
- [SDR C2XA10TY177](https://openairdocs.org/sdr/C2XA10TY177.md): Skin · dented · Nov 16, 2010 · N14952 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > TYS - DENT ON PREVIOUS REPAIR BETWEEN FRAMES 19 AND 20 STRINGER 15L. REPAIRED DENTS IAW EC5330-02287.
- [SDR C2XA10TY175](https://openairdocs.org/sdr/C2XA10TY175.md): Door Frame · corroded · Nov 16, 2010 · N14952 · Emb EMB145LR · Fuselage Main, Structure
  > TYS - A/C IS CURRENTLY IN A C-CHECK STATUS WHEN THE INSPECTION DEPARTMENT FOUND CORROSION UNDER THE LOWER AFT SERVICE DOOR TEFLON GUIDE. MAINTENANCE REPAIRED THE CORROSION UNDER THE TEFLON GUIDE AT THE SERVICE DOOR IAW EC5310-01532, REFER TO M6023 (0554421 2-
- [SDR C2XA10TY174](https://openairdocs.org/sdr/C2XA10TY174.md): Fairing · damaged · Nov 16, 2010 · N14952 · Emb EMB145LR · Horizontal Stabilizer, Plate/Skin
  > TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RIGHT SIDE HORIZIONTAL STAB TIP FAIRING WITH MULTIBLE SPOTS OF DAMAGE COMPOSITE. MAINTENANCE REPAIRED THE HORIZ STAB TIP IAW EC5750-01183 REV B AND EMB 145 SRM 51-70-06 PARAGRAPH 4, STEPS A, B AND D.
- [SDR C2XA10TY173](https://openairdocs.org/sdr/C2XA10TY173.md): Bracket · worn · Nov 16, 2010 · N14952 · Emb EMB145LR · Ailerons
  > TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RIGHT AILERON PCA BRACKET OUTBOARD HAT BUSHION HOLE OUT OF LIMITS. MAINTENACE REMOVED AND REPLACED THE RIGHT AILERON PCA BRACKET IAW EC5750-01177. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE
- [SDR C2XA10TY176](https://openairdocs.org/sdr/C2XA10TY176.md): Skin · corroded · Nov 15, 2010 · N14952 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > TYS - LOWER SKIN CORRODED AT FR14 BETWEEN STR 19L AND 19R. REMOVED AND REPLACED SKIN IAW EC5330-02280.
- [SDR C2XA10TY172](https://openairdocs.org/sdr/C2XA10TY172.md): Stringer Splice · corroded · Nov 15, 2010 · N14952 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > TYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE STRINGER SPLICE CORRODED AT STRINGER 20R AND FRAMES 13-14. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW EMB 145SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END
- [SDR C2XA10RI117](https://openairdocs.org/sdr/C2XA10RI117.md): Warning System · malfunctioned · Sep 14, 2010 · N14952 · Emb EMB145LR · Landing Gear Position and Warning
  > FLIGHT 2348 - EWR - FLIGHT CREW REPORTED LANDING GEAR LEVER DISAGREE MESSAGE ON EICAS. FLIGHT CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX PERFORMED OPERATIONAL CHECK AND FOUND NO DEFECTS. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA10IA198](https://openairdocs.org/sdr/C2XA10IA198.md): Unknown · odor · Jul 8, 2010 · N14952 · Emb EMB145LR · Air Distribution System
  > IAH - FLIGHT 2973 THE CREW REPORTED A FUEL SMELL IN THE COCKPIT WHEN ANTI-ICE CAME ON AND ON DESCENT. IT WAS NOTED THAT THE SMELL DISSIPATED QUICKLY. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED ENGINE RUNS
- [SDR C2XA10RI037](https://openairdocs.org/sdr/C2XA10RI037.md): Door · lack of lube · Mar 15, 2010 · N14952 · Emb EMB145LR · Passenger/Crew Doors
  > FLIGHT 2892 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR VERY DIFFICULT TO OPEN. EWR MX LUBRICATED MAIN CABIN DOOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09CL074](https://openairdocs.org/sdr/C2XA09CL074.md): Turbine Wheel · cracked · May 26, 2009 · N14952 · Emb EMB145LR · Turbine Section
  > DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 2 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND DURING THE ULTRASOUND INSPECTION. THE NR 2 ENGINE WAS REPLACED.
- [SDR C2XA09CL041](https://openairdocs.org/sdr/C2XA09CL041.md): Tube · leaking · Apr 8, 2009 · N14952 · Emb EMB145LR · Aircraft Fuel Distribution System
  > DURING ROUTINE MAINTENANCE THE PRESSURE REFUEL/DEFUEL LINE WAS FOUND LEAKING. MAINTENANCE INSPECTED AND FOUND THE TUBE ASSEMBLY TO BE CORRODED. THE TUBE WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA08RI182](https://openairdocs.org/sdr/C2XA08RI182.md): Clamp · deformed · Dec 18, 2008 · N14952 · Emb EMB145LR · Pneumatic Distribution System
  > FLIGHT 2775 - EWR - FLIGHT CREW REPORTED ENG NR 1 BLEED LEAK INDICATION ON EICAS IN FLIGHT. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX R&R BLEED V-CLAMP AND PERFORMED OPX CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08RI180](https://openairdocs.org/sdr/C2XA08RI180.md): Switch · inoperative · Dec 15, 2008 · N14952 · Emb EMB145LR · Compressor Bleed Valve
  > FLIGHT 2306 - EWR - DURING CLIMBING FLIGHT CREW REPORTED THE FOLLOWING MSGS ON EICAS: PACK 2 CLSD AND BLD 2 CLSD. CREW RESET THE SYSTEM BUT FAILED AGAIN AND WHEN TRIED AN ANTI ICE TEST GOT BLD 2 FAIL MSG. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. MX
- [SDR C2XA08RI179](https://openairdocs.org/sdr/C2XA08RI179.md): Bleed Valve · inoperative · Dec 15, 2008 · N14952 · Emb EMB145LR · Compressor Bleed Valve
  > FLIGHT 2306 EWR DURING CLIMBING FLIGHT CREW REPORTED THE FOLLOWING MSGS ON EICAS: PACK 2 CLSD AND BLD 2 CLSD. CREW RESET THE SYSTEM BUT FAILED AGAIN AND WHEN TRIED AN ANTI ICE TEST GOT BLD 2 FAIL MSG. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX
- [SDR C2XA08SH145](https://openairdocs.org/sdr/C2XA08SH145.md): Attach Bracket · worn · Nov 11, 2008 · N14952 · Emb EMB145LR · Rudder Miscellaneous Structure
  > SHV - DURING C-CHECK THE RUDDER UPPER CENTER ATTACHMENT BRACKET WAS FOUND TO BE WORN AND THE HAT BUSHINGS MIGRATED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 55-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA08SH144](https://openairdocs.org/sdr/C2XA08SH144.md): Sill · corroded · Nov 11, 2008 · N14952 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CARGO DOOR LOWER CUTOUT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA08SH143](https://openairdocs.org/sdr/C2XA08SH143.md): Floor Support · corroded · Nov 11, 2008 · N14952 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10 FIG 202, STEP 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA08SH142](https://openairdocs.org/sdr/C2XA08SH142.md): Floor Support · corroded · Nov 11, 2008 · N14952 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 34. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10 FIG 202, STEP 3. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA08SH141](https://openairdocs.org/sdr/C2XA08SH141.md): Floor Support · corroded · Nov 11, 2008 · N14952 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10, FIG 203, STEP 4. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA08SH140](https://openairdocs.org/sdr/C2XA08SH140.md): Floor Support · corroded · Nov 8, 2008 · N14952 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CORROSION ON LT OMEGA BEAM JUST ABOVE FR 20 CARBON CROSS BEAM. MX REPAIRED LT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10 FIG 201. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.
- [SDR C2XA08SH139](https://openairdocs.org/sdr/C2XA08SH139.md): Floor Support · corroded · Nov 8, 2008 · N14952 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CORRODED NUT PLATE HOLE ON OMEGA BEAM LAV AREA BETWEEN FRAME 60 AND 61 LT SIDE. REPAIRED LT OMEGA BEAM BETWEEN FR 60-61 AT NUT PLATE ARE IAW EC 5320-01430. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Next page: https://openairdocs.org/deregistered/N14952-2015-10-05/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 = 'N14952' AND deregistration_id = 'N14952-2015-10-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14952-2015-10-05/reports

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