# Service difficulty reports: N14953, cancelled Feb 3, 2016

A list on [N14953, cancelled Feb 3, 2016](https://openairdocs.org/deregistered/N14953-2016-02-03.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 · 72 reports

- [SDR ASOA20140913278V](https://openairdocs.org/sdr/ASOA20140913278V.md): Skin · dented · Sep 13, 2014 · N14953 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, REAR FUSELAGE HAS DENT BETWEEN FRAME 77 AND SPLICE BETWEEN STRINGERS 18 - 19R, REPAIRED DENT IAW EC5330-02939. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140911273](https://openairdocs.org/sdr/ASOA20140911273.md): Floor Support · corroded · Sep 11, 2014 · N14953 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, CORROSION FOUND ON OMEGA BEAM NUTPLATE HOLES AT FRAME 59-61. MAINTENANCE R & R CENTER OMEGA BEAM BUTTSTRAP IAW EC5310-01473, REV D. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140909272](https://openairdocs.org/sdr/ASOA20140909272.md): Beam · corroded · Sep 9, 2014 · N14953 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C-CHECK, CARGO DOOR LOWER CUTOUT CORRODED. R & R CARGO DOOR LOWER CUTOUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140906271](https://openairdocs.org/sdr/ASOA20140906271.md): Floor Support · corroded · Sep 6, 2014 · N14953 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, RT OMEGA BEAM BETWEEN FRAMES 59-61 CORRODED. MAINTENANCE FABRICATED AND INSTALLED REPAIR PARTS ON RT OMEGA BEAM IAW EC5310-01473, REV D. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130708100](https://openairdocs.org/sdr/ASOA20130708100.md): Skin · cracked · Jul 8, 2013 · N14953 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING 4A INSPECTION THE LT FUSELAGE 1 SKIN WAS FOUND TO BE CRACKED AT FRAME 75 IN 2 PLACES BELOW STRINGER 1R. MX PERFORMED A DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130708099](https://openairdocs.org/sdr/ASOA20130708099.md): Skin · cracked · Jul 8, 2013 · N14953 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING 4A INSPECTION THE REAR FUSELAGE 1 SKIN WAS FOUND TO BE CRACKED AT FRAME 75 BETWEEN STRINGERS 1R AND 2R. MX PERFORMED A DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121018153](https://openairdocs.org/sdr/ASOA20121018153.md): Skin · cracked · Oct 17, 2012 · N14953 · Emb EMB145LR · Wing, Plate/Skin
  > LT WING UPPER SKIN T/E WAS FOUND CRACKED AT THE LT GROUND SPOILER HINGE POINT. CUTOUT THE CRACKED AREA, FABRICATED AND INSTALLED DOUBLER AND TRIPLER. ACFT STILL IN C CHECK
- [SDR ASOA20121017152](https://openairdocs.org/sdr/ASOA20121017152.md): Window Frame · corroded · Oct 17, 2012 · N14953 · Emb EMB145LR · Fuselage Main, Structure
  > LEFT & RIGHT WINDSHIELD FRAME HAS CORROSION IN SEVERAL HOLES. REMOVED CORROSION FROM BOLT HOLES AND SOME OF THE HOLES REQUIRED BUSHINGS TO BE INSTALLED IAW ETD2012-145-014418-A AND EC5310-01633. ACFT IS STILL IN C-CHECK.
- [SDR C2XA11IA185](https://openairdocs.org/sdr/C2XA11IA185.md): Uplock · inoperative · Aug 27, 2011 · N14953 · Emb EMB145LR · Landing Gear Position and Warning
  > IAH - FLIGHT 2174, THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR INDICATION WAS SHOWING DASHES OF YELLOW AND GREEN, AND ALTERNATING BACK AND FORTH. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT MLG
- [SDR C2XA11CL157](https://openairdocs.org/sdr/C2XA11CL157.md): Inverter · faulty · Jun 27, 2011 · N14953 · Emb EMB145LR · Emergency Lighting
  > GRR FLT 2904 THE CREW REPORTED THE OVERWING CEILING EXIT LIGHT DID NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11RI113](https://openairdocs.org/sdr/C2XA11RI113.md): Controller · inoperative · Jun 20, 2011 · N14953 · Emb EMB145LR · Central Display
  > FLIGHT 2287 - EWR - FLIGHT CREW REPORTED THAT, EN ROUTE FROM EWR TO CMH, FMS FAILED, BOTH PFD'S AND NAVS ALSO WENT OUT. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED CAPT DC550 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. A
- [SDR C2XA11TY028](https://openairdocs.org/sdr/C2XA11TY028.md): Shim · worn · Mar 15, 2011 · N14953 · Emb EMB145LR · Nose/Tail Landing Gear
  > TYS - A/C WAS TAXI FOR TAKEOFF AND IN CLIMBOUT, WHEN GEAR STOWED, CREW REPORTED A RATTLING NOISE WHEN GEAR STOWED. A/C WAS FERRIED TO TYS FROM BNA WHERE MAINTENANCE REMOVED THE NOSE GEAR AND FOUND THAT GEAR NEEDED TO BE SHIM. MAINTENANCE MEASURED THE BEARIN
- [SDR C2XA10SH372](https://openairdocs.org/sdr/C2XA10SH372.md): Fitting · cracked · Oct 29, 2010 · N14953 · Emb EMB145LR · Nacelle/Pylon, Attach Fittings
  > SHV - DURING C-CHECK NR 1 ENGINE FORWARD LOWER YOKE FORWARD FLANGE CRACKED. MAINTENANCE REMOVED AND REPLACED NR1 ENGINE FORWARD LOWER YOKE FITTING IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH371](https://openairdocs.org/sdr/C2XA10SH371.md): Floor Support · corroded · Oct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FRAME 38 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRAME 38 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH370](https://openairdocs.org/sdr/C2XA10SH370.md): Floor Support · corroded · Oct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 HAS CORROSION. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH369](https://openairdocs.org/sdr/C2XA10SH369.md): Floor Support · corroded · Oct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CENTER OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 HAS CORROSION. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE BETWEEN FRAME 43-44 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH368](https://openairdocs.org/sdr/C2XA10SH368.md): Floor Support · corroded · Oct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE BETWEEN FRAME 49-50 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE BETWEEN FRAME 49-50 IAW EMB-145 SRM 51-00-10 AND RESTORED TO ORIGINAL FINISH IAW EMB-145 CPM 51-21-06. THE A
- [SDR C2XA10SH367](https://openairdocs.org/sdr/C2XA10SH367.md): Floor Support · corroded · Oct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CENTER OMEGA BEAM L-FLANGE BETWEEN FRAME 49-50 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE BETWEEN FRAMES 49-50 IAW EC5310-01466 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH366](https://openairdocs.org/sdr/C2XA10SH366.md): Floor Support · corroded · Oct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FRAME 54 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRAME 54 REPAIR IAW EMB-145 SRM 51-00-10. RESTORED TO ORIGINAL FINISH IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS
- [SDR C2XA10SH365](https://openairdocs.org/sdr/C2XA10SH365.md): Frame · corroded · Oct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Main, Frame
  > SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON FRAME 65 STRINGER 16L-17L. MAINTENANCE PERFORMED REPAIR ON FRAME 65 STRINGER 16L-17L IAW EMB-145 EC5310-01529. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH364](https://openairdocs.org/sdr/C2XA10SH364.md): Fitting · corroded · Oct 29, 2010 · N14953 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON SHEAR CLIP FRAME 65 STRINGER 16L-17L. MAINTENANCE PERFORMED REPAIR ON SHEAR CLIP FRAME 65 STRINGER 16L-17L IAW EMB-145 EC5320-01494. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10CL096](https://openairdocs.org/sdr/C2XA10CL096.md): Proximity Switch · out of adjust · Jun 14, 2010 · N14953 · Emb EMB145LR · Landing Gear Position and Warning
  > CLE FLT 2632 - THE CREW REPORTED AN AIR/GROUND FAIL MESSAGE. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE BUT CHANGED THE LGEU, ADJUSTED 1 PROXIMITY SWITCH ON LEFT AND RIGHT GEAR AND ADJUSTED NOSE PROXIMITY SWITCH TARGET ON THE NOSE GEAR AND CHANGED THE NOSE
- [SDR C2XA10RI002](https://openairdocs.org/sdr/C2XA10RI002.md): Charger · defective · Jan 5, 2010 · N14953 · Emb EMB145LR · Emergency Lighting
  > FLIGHT 2531 - EWR - FLIGHT CREW REPORTED EMERGENCY LIGHT WOULD NOT TURN OFF. EWR MX REMOVED AND REPLACED NR 2 BATTERY CHARGER ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09TY265](https://openairdocs.org/sdr/C2XA09TY265.md): Battery · discharged · Oct 27, 2009 · N14953 · Emb EMB145LR · Emergency Equipment
  > TYS - A/C WAS IN FOR A SERVICE CHECK WHEN INSPECTION FOUND THE AED DEFIBRILLATOR BATTERY INOP. MAINTENANCE REMOVED AND REPLACED THE AED DEFIBRILLATOR BATTERY IAW EC 2560-01065. A/C RELEASED BACK TO SERVICE.
- [SDR C2XA09IA263](https://openairdocs.org/sdr/C2XA09IA263.md): Inverter · inoperative · Oct 14, 2009 · N14953 · Emb EMB145LR · Emergency Lighting
  > MCI - DURING MAINTENANCE INSPECTION THE NUMBER FOUR AND FIVE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETU
- [SDR C2XA09RI148](https://openairdocs.org/sdr/C2XA09RI148.md): Altimeter · malfunctioned · Aug 19, 2009 · N14953 · Emb EMB145LR · Altimeter, Barometric/Encoder
  > FLIGHT 2790 - EWR - DURING DESCENT, FLIGHT CREW REPORTED AN AMBER INDICATION FOR RADIO ALTIMETER ON PFD WITH LANDING GEAR AURAL SOUND FOR 5 SECONDS THEN CLEARED. EWR MX RESET BOTH RA C/B'S AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RE
- [SDR C2XA09TY107](https://openairdocs.org/sdr/C2XA09TY107.md): Proximity Switch · broken · Jun 16, 2009 · N14953 · Emb EMB145LR · Landing Gear Position and Warning
  > TYS - AIRCRAFT WAS EN ROUTE TO IAH FROM EWR WITH A STOP AT TYS, WHEN LEAVING TYS THE LDG WOULDN'T RETRACT SO CREW RETURN TO BASE. MAINTENANCE REMOVED AND REPLACED THE NLG PROX SWITCH IAW EMB 145 AMM 32-63-02 AND OPS CHECK GOOD. RELEASED BACK TO SERVICE.
- [SDR C2XA09TY106](https://openairdocs.org/sdr/C2XA09TY106.md): Bulb · failed · Jun 16, 2009 · N14953 · Emb EMB145LR · Emergency Lighting
  > ACFT IN OVERNIGHT FOR A 2A CHECK, WHEN INSP FOUND THE RT OVERWING EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED THE THE BULB FOR THE LIGHT IAW AMM 33-50-07, OPS CHECK GOOD AND WAS RELEASED.
- [SDR C2XA09RI043](https://openairdocs.org/sdr/C2XA09RI043.md): Power Supply · discharged · Mar 20, 2009 · N14953 · Emb EMB145LR · Emergency Lighting
  > FLIGHT 2996 - EWR - FLIGHT CREW REPORTED FORWARD EMERGENCY LIGHT INOPERATIVE ABOVE F/A SEAT. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08CL101](https://openairdocs.org/sdr/C2XA08CL101.md): Warning System · activated · Aug 27, 2008 · N14953 · Emb EMB145LR · Fuel Indicating System
  > DSM FLIGHT NR 2636 THE CREW REPORTED A FUEL 1 LOW LEVEL MSG IN FLIGHT. THE FLIGHT DIVERTED IN DSM AND LANDED WITHOUT INCIDENT. THE FUEL QUANTITY INDICATOR WAS ACCURATE. THE SYSTEM WAS PLACED ON MEL SUPPLEMENT TO FOLLOW.
- [SDR C2XA08RI084](https://openairdocs.org/sdr/C2XA08RI084.md): Handle · unsecure · Jun 13, 2008 · N14953 · Emb EMB145LR · Passenger/Crew Doors
  > FLIGHT 2807 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR WOULD NOT OPEN OR CLOSE FROM INSIDE. EWR MAINTENANCE SECURED MAIN CABIN DOOR HANDLE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)
- [SDR C2XA08IA044](https://openairdocs.org/sdr/C2XA08IA044.md): Skin · cracked · Jan 29, 2008 · N14953 · Emb EMB145LR · Wing, Plate/Skin
  > IAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH RE-INSPECTIONS TO BE MADE AT EVER 50FC, AND THE
- [SDR C2XA08IA029](https://openairdocs.org/sdr/C2XA08IA029.md): Fuse · blown · Jan 17, 2008 · N14953 · Emb EMB145LR · Emergency Lighting
  > IAH - FLIGHT 2099 DURING PREFLIGHT INSPECTION SOME EMERGENCY LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED A FUSE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA07TY065](https://openairdocs.org/sdr/C2XA07TY065.md): Handle · failed · Oct 31, 2007 · N14953 · Emb EMB145LR · Landing Gear Selector
  > LANDING GEAR FAILED TO RETRACT. REPLACED LANDING GEAR HANDLE IAW EMB 145 MM 32-32-02, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA07CL092](https://openairdocs.org/sdr/C2XA07CL092.md): Computer · shorted · Oct 30, 2007 · N14953 · Emb EMB145LR · Autopilot Computer
  > CLEVELAND MAINTENANCE REPORTED THE GUIDANCE CONTROL UNIT (GC-550) HAD SMOKE COMING FROM IT. MAINTENANCE INSPECTED AND REPLACED THE GUIDANCE CONTROL COMPUTER. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA07TY060](https://openairdocs.org/sdr/C2XA07TY060.md): Doubler · missing · Oct 15, 2007 · N14953 · Emb EMB145LR · Rudder, Plate/Skin
  > TYS - A/C WAS FOUND WITH A NUT PLATE MISSING AND THE HOLE ELONGATED ON THE RUDDER 2. MAINTENANCE FABRICATED A FILLER AND A INTERNAL DOUBLER. ALODINED AND EPOXY PRIMED THE PARTS. INSTALL FABRICATED PARTS ON THE RUDDER IAW EC 5540--01077. ALL WORK WAS ACCOMP
- [SDR C2XA07RI052](https://openairdocs.org/sdr/C2XA07RI052.md): Light · malfunctioned · Jul 3, 2007 · N14953 · Emb EMB145LR · Emergency Lighting
  > FLT 2774 - DAY - CREW REPORTED MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. DAY MX RECYCLED BATTERY SWITCHES AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA07IA047](https://openairdocs.org/sdr/C2XA07IA047.md): Light · malfunctioned · Feb 26, 2007 · N14953 · Emb EMB145LR · Emergency Lighting
  > IAH - FLT NR 3116, DURING A TEST THE EMERGENCY EXIT LIGHTING FAILED TO ILLUMINATE. MAINTENANCE RESET THE EMERGENCY LIGHTING SYSTEM AND OPERATIONALLY TESTED THE SYSTEM. THE DISCREPANCY COULD NOT BE DUPLICATED AND WAS THEN CLEARED.
- [SDR C2XA06IA141](https://openairdocs.org/sdr/C2XA06IA141.md): Wire · loose · Aug 27, 2006 · N14953 · Emb EMB145LR · Light System Wiring
  > IAH - DURING A-CHECK INSPECTION, THE EMERGENCY EXIT LIGHT ABOVE THE F/A SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED THE SIGN, RE-SECURED THE CONNECTORS, AND RE-INSTALLED THE SIGN. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED
- [SDR C2XA06IA053](https://openairdocs.org/sdr/C2XA06IA053.md): Acm · overheated · Apr 1, 2006 · N14953 · Emb EMB145LR · Cabin Cooling System
  > FLT 2862 - CREW REPORTED SMOKE IN THE CABIN AFTER REACHING 10,000 FT CLIMBOUT. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE FOUND THE NR 2 ACM TO BE OVERHEATING. THE ACM WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.
- [SDR C2XA05TY004](https://openairdocs.org/sdr/C2XA05TY004.md): Fitting · corroded · Jan 13, 2005 · N14953 · Emb EMB145LR · Vertical Stabilizer, Attach Fittings
  > TYS, DURING A SCHEDULED INSPECTION, THE VERTICAL STAB TO FUSELAGE FITTING ATTACH BRACKET WAS FOUND FRETTING ON SKIN AT FRAME 75. MAINTENANCE REMOVED THE STAB FITTING AT FRAME 75, CLEANED AND INSPECTED THE SKIN AND FITTING (NO CORROSION OR DAMAGE WAS FOUND), A
- [SDR C2XA05TY003](https://openairdocs.org/sdr/C2XA05TY003.md): Sill · corroded · Jan 13, 2005 · N14953 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > TYS, DURING A SCHEDULED INSPECTION THE SERVICE DOOR SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE DOOR SILL IAW EMB-145-AMM-21-31-00 / 135/145 SRM 51-40-00 AND 52-20-03, CABIN LEAKAGE AND FUNCTIONAL CHECKED GOOD.
- [SDR C2XA05TY002](https://openairdocs.org/sdr/C2XA05TY002.md): Hinge · worn · Jan 4, 2005 · N14953 · Emb EMB145LR · Ventral Structure
  > DURING A 4C INSPECTION THE RT AND LT VERTICAL STABLIZER SPHERICAL BEARING HOUSINGS WERE FOUND WORN. MAINTENANCE REAM AND INSTALL NEW BUSHINGS IAW EC5510-01107.
- [SDR C2XA04BT110](https://openairdocs.org/sdr/C2XA04BT110.md): Battery · inoperative · Oct 17, 2004 · N14953 · Emb EMB145LR · Emergency Lighting
  > BTV, DURING SERVICE AND ROUTINE CHECK ON RON, MAINTENANCE FOUND THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY POWER SUPPLY IAW EMB145 AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR C2XA04CL044](https://openairdocs.org/sdr/C2XA04CL044.md): Controller · failed · Apr 28, 2004 · N14953 · Emb EMB145LR · Cabin Pressure Controller
  > BTV FLIGHT NR 2441 THE CREW REPORTED SMOKE COMING FROM THE DIGITAL PRESSURE CONTROLLER. MAINTENANCE REPLACED THE DIGITAL PRESSURE CONTROLLER. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA03IA105](https://openairdocs.org/sdr/C2XA03IA105.md): Lamp · loose · Nov 20, 2003 · N14953 · Emb EMB145LR · Emergency Lighting
  > DURING SCHEDULED MAINTENANCE THE LEFT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE-SECURED THE LAMP IN THE LIGHT FIXTURE. THE LIGHT OPERATIONALLY CHECKED GOOD.
- [SDR C2XA03BT064](https://openairdocs.org/sdr/C2XA03BT064.md): Bulb · burned out · Jun 6, 2003 · N14953 · Emb EMB145LR · Emergency Lighting
  > DURING 3A INSPECTION MAINTENANCE FOUND PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED PASSENGER DOOR EMERGENCY LIGHT BULB IAW EMB145 AMM 33-50-00. OPS CHECKED GOOD.
- [SDR C2XA03SH082](https://openairdocs.org/sdr/C2XA03SH082.md): Sill · corroded · Mar 31, 2003 · N14953 · Emb EMB145LR · Fuselage Main, Structure
  > DURING C-CHECK FOWARD SILL HAS CORROSION BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED DAMAGE AND MADE A DOUBLER REPAIR ON AFFECTED SILL IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA03SH081](https://openairdocs.org/sdr/C2XA03SH081.md): Skin · gouged · Mar 31, 2003 · N14953 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > DURING C-CHECK SKIN WAS FOUND GOUGED UNDER GPU ACCESS PANEL BETWEEN FRAMES 6 AND 8. MAINTENACE REMOVED DAMAGE AND REPAIRED SKIN IAW EMB 145 SRM 53-11-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA03SH080](https://openairdocs.org/sdr/C2XA03SH080.md): Support · corroded · Mar 31, 2003 · N14953 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK THE SUPPORT PLATE BETWEEN LT OMEGA BEAM AND LT SILL WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 60 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Next page: https://openairdocs.org/deregistered/N14953-2016-02-03/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 = 'N14953' AND deregistration_id = 'N14953-2016-02-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14953-2016-02-03/reports

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